N757AT

Part: ANGLE — DAMAGED (FUSELAGE) · airframe 90,541 hrs · 38,168 cycles

DAMAGE WAS FOUND ON THE LOWER SURFACE OF THE INNER ANGLE COMMON TO THE C2 DOOR. IAW ER/A 519692-14, REV A.

Part: SKIN — CRACKED (WING) · airframe 90,183 hrs · 38,086 cycles

WING SKIN PANEL HAS A CRACK. FABRICATED REPAIR DOUBLER IAW ERA 529907-14.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 86,676 hrs · 37,166 cycles

EMERGENCY LIGHTS INOPERATIVE. REPAIRED WIRE IAW WDM 33-51.

Part: LIGHT — INOPERATIVE (SEAT 43 DEF) · airframe 85,625 hrs · 36,884 cycles

FOUND SEAT 43DEF EMERGENCY LIGHT INOPERATIVE. R & R WHITE EMERGENCY LIGHT ASSY IAW AMM 33-51. OPS CHECKED GOOD.

Part: UNKNOWN — ODOR (CABIN) · airframe 84,522 hrs · 36,594 cycles

DIVERTED DUE TO REPORT OF "LIGHT" SMOKE/MIST IN CABIN AND SULFUR/MATCH/BURNING ODOR NEAR SEATS 24-26 & 36-38. MIST/ ODOR DISIPATED BEFORE LANDING. NO MASKS DONNED OR DEPLOYED. NO EMERGENCY DECLARED. INSPECTED SEAT AREAS, CEILING PANELS, LAVS, AND RAN IFE EQUIPMENT, ENGINES AND PACKS. NO ODOR DETECTED. TEST FLIGHT ACCOMPLISHED AND ALL SYS CHECKS OK.

Part: CONNECTOR — DAMAGED (LT OVRWG SLIDE) · airframe 83,337 hrs · 36,292 cycles

FOUND OVERWING SLIDE LT SIDE PRESSURE SWITCH CONNECTOR TO BOTTLE BROKEN WIRES. REPLACED CONNECTOR IAW BSWPM 21-61 OVERWING ESCAPE SQUIB TEST SYS LT AND RT TEST 2 NOW TESTS NORMAL.

Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 83,055 hrs · 36,225 cycles

AFT EMEGENCY LIGHTS WERE INOPERATIVE. MX RESEATED AFT LIGHTS. OPERATION OF LIGHT NOW CHECK OK.

Part: FUSE — BLOWN (EMERGENCY LIGHTS) · airframe 81,391 hrs · 35,806 cycles

DURING LAYOVER MAINTENANCE FOUND EMERGENCY LIGHTS FROM ROW 36 AND AFT INOPERATIVE. MAINTENANCE REPLACED FUSES ON BATTERY PACK M9012. OPS CHECKED OK.

Part: SLIDE — FAILED (CABIN) · airframe 79,810 hrs · 35,421 cycles

LINE MAINTENANCE FOUND RIGHT OVERWING EMERGENCY SLIDE FAILS TEST NUMBER 2. REMOVED AND REPLACED SLIDE.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 79,178 hrs · 35,273 cycles

LINE MAINTENANCE FOUND INOPERATIVE EMERGENCY LIGHT AT SEAT ROW 43. REPLACED LIGHT ASSEMBLY. LIGHT OPERATION NORMAL.

Part: DOOR FRAME — CRACKED (FUSELAGE)

DUE OPN 5032 AD NR 1 CARGO DOOR OPENING FWD FRAME STA 560 WEB CRACKED BETWEEN 24R-26R. REF NR 148. INSTALLED PERMANENT REPAIR PER SRM 53-00-07 FIG 201 REPAIR NR 2. REQUIRES REPETITIVE INSPECTION PER SRM 53-00-07 FIG 201 TABLE 3. HFEC AND LFEC REF NDT PART 6 51-00-01 EVERY 3000 FLIGHT CYCLES.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 78,390 hrs · 35,070 cycles

DURING OPN 50321 INSPECTION DISCOVERED THE FWD CARGO DOOR OPENG, FWD FRAME WEB CRACKED FRAME STATION 560 BETWEEN STRINGER 24R, 25R AND 26R. INSTALLED PERMANENT REPAIR PER SRM 53-00-07 REPAIR 2 FIG 201. THIS IS A CATEGORY B REPAIR AND REQUIRES FOLLOW UP INSPECTIONS EVERY 3000 FLIGHT CYCLES PER SRM 53-00-07 FIG 201 TABLE III.

Part: CONNECTOR — LOOSE (CABIN) · airframe 78,330 hrs · 35,055 cycles

DURING EA 06-495873-03 MAINTENANCE FOUND EMERGENCY PATH LIGHT AT SEAT 43 DEF INOP. MAINTENANCE RE-CONNECTED LOOSE LIGHT CONNECTOR. OPERATION OF LIGHT NOW CHECKS OK.

Part: CLAMP — FAILED (MLG TRUCK SHEILD)

FLT 1196AT APPROXIMATELY 2105P MLG TRUCK SHEILD DEPARTED THE ACFT ON APPROACH AND IMPACTED A PERSONAL VEHICLE. THE FAILURE OF THE THREE BAND CLAMPS THAT ATTACH THE SHIELD TO THE MAIN LANDING GEAR TRUCK CAUSED THE PART TO DEPART THE ACFT ON APPROACH WITH LANDING GEAR EXTENDED.

Part: CONNECTOR — OUT OF ADJUST (CABIN) · airframe 76,758 hrs · 34,676 cycles

EMERGENCY PATH LIGHT AT 25D WAS FOUND TO BE INOPERATIVE. MAINTENANCE ADJUSTED THE CONTACTS AT THE CONNECTOR. OPERATIONAL CHECK WAS NORMAL.

Part: WIRE HARNESS — DISCONNECTED (CABIN) · airframe 76,131 hrs · 34,524 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTS AT SEAT 43D INOPERATIVE. MAINTENANCE RECONNECTED THE HARNESS. OPERATIONAL CHECK WAS GOOD.

Part: LIGHT — MISSING (SEAT 23D) · airframe 75,106 hrs · 34,279 cycles

DURING A LAYOVER CHECK, MX FOUND THE EMERGENCY PATHLIGHTS AT 23D MISSING. MX REPLACED THE LIGHT ASSY AT SEAT 23D. OPS CHECK WAS GOOD.

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 74,875 hrs · 34,219 cycles

THE VERTICLE STAB SKIN WAS DELAMINATED. THE PANNEL WAS REMOVED AND ROUTED TO SHOP 382. THE PANEL WAS REPAIRED IAW ERA 488591-14 REV B ON 01/12/11. THE PANEL WAS COMPLETED.

Part: SKIN — DELAMINATED (VERTICAL STAB) · airframe 74,872 hrs · 34,218 cycles

DELAMINATION FOUND ON LT SIDE OF VERTICAL STABILIZER TIME LIMITED REPAIR DONE IAW ERA 488591-14, REV 0. A PERMANENT REPAIR DONE BY COMPOSITE SHOP ON NR 001 IAW ERA 488591-14, REV B.

Part: CONNECTOR — UNSECURE (EMERGENCY LIGHTS) · airframe 74,651 hrs · 34,156 cycles

DURING LAYOVER CHECK, MX FOUND SEATS 43DEF EMERGENCY PATH LIGHT INOPERATIVE. MX SECURED CONNECTOR UNDER SEAT. OPS CHECK WAS GOOD.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 74,398 hrs · 34,080 cycles

DURING LAYOVER CHECK MAINTENANCE FOUND EMERGENCY TRACK LIGHTING OPERATIVE AT 30DEF. REPLACED EMERGENCY PATH LIGHT ASSEMBLY AT 30DEF. OPERATIONAL CHECK IS GOOD. (2010-D1368) (DL75E103194)

Part: WIRE — DAMAGED (CABIN) · airframe 73,219 hrs · 33,747 cycles

DURING LAYOVER CHECK, MAINTENANCE FOUND EMERGENCY PATH LIGHTS AFT OF DOOR 2 RIGHT INOPERATIVE. MAINTENANCE REPAIRED WIRE AND REPLACED POWER SUPPLY FUSE. OPERATIONAL CHECK WAS GOOD (DL75E101771).

Part: FLOORBEAM — CORRODED (BS 1681) · airframe 72,721 hrs · 33,613 cycles

EXTRUDED FLOORBEAM AT STA 1681 AND DECK PLATE CORRODED BETWEEN AT RBL 4 AND RBL 12. COMPLIED WITH ER/A 481843-14 REV REF NON ROUTINE 154817.

Part: FLOORBEAM — CORRODED (BS 365) · airframe 72,721 hrs · 33,613 cycles

CORROSION ON FLOORBEAM UPPER CHORD TOP SURFACE AT STA 365, RBL 24 TO RBL 48. COMPLIED WITH ER/A 481845-14, REF NON ROUTINE CARD 168871.

Part: SEAT TRACK — CORRODED (BS 420-424) · airframe 72,721 hrs · 33,613 cycles

CORROSION ON MAIN CABIN SEAT TRACK BOTTOM AREA STA 420 TO STA 424, RBL 24. REPLACED DAMAGED SEAT TRACK, REF NON ROUTINE 168917.

Part: INTERCOSTAL — CORRODED (BS 1300-1320) · airframe 72,721 hrs · 33,613 cycles

AFT CARGO INTERCOSTAL CORRODED ON LOWER LEG STA 1300-1320 OTBD OF STR 28L. REPLACED INTERCOSTAL, REF NON ROUTINE 168945.

Part: SHEAR TIE — CORRODED (BS 1320 S27-28R) · airframe 72,721 hrs · 33,613 cycles

AFT CARGO SHEAR TIE CORRODED STA 1320 BETWEEN STR 27 AND 28 RT. REPLACED SHEAR TIE REF NON ROUTINE 168938.

Part: STRINGER SPLICE — CORRODED (BS 1466 S28R) · airframe 72,721 hrs · 33,613 cycles

AFT CARGO DOOR OEM STRINGER SPLICE CORRODED STA 1466 STA 28R. REPLACED STRINGER SPLICE AT ST AEROSPACE SAT REF NON ROUTINE 168856.

Part: STRINGER — CORRODED (BS 1420 S29R) · airframe 72,721 hrs · 33,613 cycles

AFT CARGO STR 29R CORRODED FWD OF STA 1420. REMOVED DAMAGED STRINGER AND REPAIRED REF NON ROUTINE 168817.

Part: DOUBLER — CORRODED (BS 1715 LBL 10) · airframe 72,721 hrs · 33,613 cycles

MAIN CABIN DECK PLATE DOUBLER STA 1715, LBL 10 CORRODED. REPLACED DOUBLER REF NON ROUTINE CARD 168806.

Part: STRINGER — CORRODED (BS 1460 S28L) · airframe 72,721 hrs · 33,613 cycles

AFT CARGO STR 28L CORRODED STA 1460-1485. REMOVED DAMAGED SECTION OF STRINGER AND REPAIRED REF NON ROUTINE 154908.

Part: CUSP WEB — CORRODED (BS 1620-1640) · airframe 72,721 hrs · 33,613 cycles

MAIN CABIN CUSP WEB S-17R HAS CORROSION ON LOWER SURFACE (PREVIOUSLY BLENDED) STA 1620 TO 1640. REPLACED CUSP WEB, REF NON ROUTINE CARD 154873.

Part: SHEAR TIE — CORRODED (BS 1560 S26-27R) · airframe 72,721 hrs · 33,613 cycles

AFT CARGO SHEAR TIE CORRODED STA 1560 STR 26-27 RT. REPLACED SHEAR TIE REF NON ROUTINE 153626.

Part: DOUBLER — CORRODED (BS 1681) · airframe 72,721 hrs · 33,613 cycles

MAIN CABIN DOUBLER CORRODED STA 1681 RBL 30 TO RBL 48 / DECK PLATE. REPAIR ACCOMPLISHED ON N/R 15817, REF NON ROUTINE 154864.

Part: DOUBLER — CORRODED (BS 1681) · airframe 72,721 hrs · 33,613 cycles

MAIN CAIN DECK PLATE DOUBLER REPAIR STA 1681 CORRODED BL0 TO LBL 60. REPAIR ACCOMPLISHED ON NON ROUTINE 154817, REF NON ROUTINE 154865.

Part: INTERCOSTAL — CORRODED (BS 1460-1480) · airframe 72,721 hrs · 33,613 cycles

AFT CARGO INTERCOSTAL CORODED STA 1460-1480 INBD OF STR 28R. REPLACED INTERCOSTAL, REF NON ROUTINE 154851.

Part: INTERCOSTAL — CORRODED (BS 1480-1500) · airframe 72,721 hrs · 33,613 cycles

AFT CARGO INTERCOSTAL CORRODED STA 1480-1500 O/B STR 27L. REPLACED INTERCOSTAL, REF NON ROUTINE 154902.

Part: SHEAR TIE — CORRODED (BS 1600 S28-29L) · airframe 72,721 hrs · 33,613 cycles

AFT CARGO SHEAR TIE CORRODED STA 1600 STR28-29L. R & R SHEAR TIE, REF NON ROUTINE 153611.

Part: FRAME — CORRODED (BS 1520 S26L/R) · airframe 72,721 hrs · 33,613 cycles

AFT CARGO FRAME CORRODED ON ALL SURFACED STA 1520, STR 26L TO 26R. COMPLIED WITH ER/A 482134-14, REF NON ROUTINE 153632.

Part: FLOORBEAM — CORRODED (BS 1640) · airframe 72,721 hrs · 33,613 cycles

MAIN CABIN FLOORBEAM PREVIOUS REPAIR CORRODED STA 1640, LBL 62 TO RBL 62. R & R PREVIOUS REPAIR, REF NON ROUTINE CARD 154872.

Part: PLATE — CORRODED (BS 1681-1720) · airframe 72,721 hrs · 33,613 cycles

MAIN CABIN DECK PLATE HAS CORROSION ON MULTIPLE AREAS STA 1681 TO 1720, BL0 TO RBL 60. REMOVED DAMAGE AND REPAIRED, REF NON ROUTINE 154862.

Part: DOUBLER — CORRODED (BS 1715 RBL 20) · airframe 72,721 hrs · 33,613 cycles

MAIN CABIN DECK PLATE DOUBLER CORRODED STA 1715, RBL 20. REPLACED DOUBLER, REF NON ROUTINE CARD 154863.

Part: FRAME — CORRODED (BS 1600 S24-26R) · airframe 72,721 hrs · 33,613 cycles

AFT CARGO FRAME REPAIR CAP CORRODED STA 1600, STR 26R-24R. REPLACED FRAME REPAIR, REF NON ROUTINE 153612.

Part: DOOR FRAME — GOUGED (OVERWING) · airframe 72,721 hrs · 33,613 cycles

RT AFT OVERWING DOOR TOP FRAME INTERIOR SIDE GOUGED AFT SIDE OF DOOR OTBD OF INTERCOSTAL. REMOVED DAMAGED AND REPAIRED, REF NON ROUTINE 154840.

Part: STRUCTURE — CORRODED (FS 1060) · airframe 72,721 hrs · 33,613 cycles

CORROSION ON CHORD LOWER SURFACE AT FS 1060 RBL8 TO LBL8. REMOVED DAMAGED CHORD AND REPAIRED REF NON ROUTINE 160818.

Part: SKIN — CRACKED (FUSELAGE) · airframe 72,721 hrs · 33,613 cycles

REPAIR DOUBLER IS CRACKED AT R-4 DOOR CUTOUT FWD SIDE, AT ENGAGE/DISENGAGE HANDLE CUTOUT. R & R REPAIR DOUBLER AT ST AEROSPACE SAT REF NON ROUTINE 160747.

Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 72,231 hrs · 33,503 cycles

FOUND EMERGENCY LIGHT AT 34 INOP. REPAIRED WIRING UNDER SEAT LIGHT. OPS CK GOOD.

Part: PUMP — FAULTY (RT ENGINE) · airframe 70,134 hrs · 32,995 cycles

RIGHT ENG START AFTER START VALVE CLOSED N1 AND N2 FAILED TO ACCELERATE TO GROUND IDLE. STAGNATED AT 18 PERCENT N1 AND 55 PERCENT N2 EGT VERY SLOWLY CONTINUE TO CLIMB TO 509. REMOVED RT ENG FUEL CONTROL IAW AMM 73-21-01-024-010. REMOVED AND REPLACED FUEL PUMP PER AMM 73-11-01, REINSTALLED FUEL CONTROL PER 73-21-01. LEAK CHECK GOOD. FUEL PUMP TEST GOOD PER AMM 71-00-00/501, FUEL CONTROL TEST GOOD PER AMM 71-00-00 TEST NR 15.

Part: EEC — FAILED (NR 1 ENGINE) · airframe 70,085 hrs · 32,982 cycles

ON LT ENGINE START, NO LIGHT OFF, NO FUEL FLOW STATUS MSG. L ENG PRI CONT, L ENG SEC CONT, L ENG OIL PRESS STATUS MSGS. REMOVED AND REPLACED LEFT EEC PER M/M, CKS GOOD. RAN ENGINE, NO MSG FAULTS.

Part: CIRCUIT BREAKER — FAILED (FUEL CONTROL) · airframe 69,690 hrs · 32,879 cycles

ABORTED ENG START DUE TO NO FUEL FLOW. LT ENG VALVE LIGHT REMAINS ILLUMINATED. CA-C/B FOR LEFT FUEL CONTROL POPPED. CHECKED WIRES FROM C/B C1P6-1 P-36 PANEL AND M10506. FUEL CONTROL UNIT C/B POPS WITH UNITS DISCONNECTED RAN CHECKS THRU FUEL CONTROL MODULE. REPLACED FUEL CONTROL CONDITIONING C/B PER AMM. RAN ENGINE AT GATE ENGINE RAN NORMAL BOTH PRIMARY AND SECONDARY CONTROL. WDM 76-11-11 PG7.1 AND WDM 74-31-11 USED. ETOPS CATEGORY 'E': PROBLEMS WITH SYSTEMS CRITICAL TO ETOPS.

Part: WIRE — BROKEN (P36 PANEL) · airframe 67,895 hrs · 32,400 cycles

ON TAXI OUT CREW REPORTED A PTU XFER STATUS MSG. A/C RTB. T/S SYSTEM FOUND WIRE W1260-0407-22 BROKEN ON THE X1 LEG OF RELAY K10337. MSG ONLY SHOWS WITH BOTH ENGINES RUNNING. PERFORMED CHECK OF PTU PER MM TEST OK. REPLACED LT AND RT RELAYS K10398 LEF K10444 RIGHT, NO HELP. CONTINUITY CHECK AT LEFT EDP PRESSURE SWITCH IS GOOD. REPLACED K103338, K10399 AND K10051 NO HELP. FOUND WIRE W1260-0407-22 BROKEN AT X1 OF K10337. REPAIRED SA PTU CHECKS NORMAL.

Part: TRANSFER VALVE — LEAKING (HYD SYSTEM) · airframe 59,560 hrs · 29,278 cycles

DURING CRUISE FLT L HYD QTY EICAS MESSAGE AND L HYD RSVR LIGHT ILLUMINATED. OBSERVED L HYD QTY SLOWLY DECREASE FROM .48 TO .41. TURNED OFF L ENGINE AND L ELEC HYD PUMPS HYD QTY STABILIZED AT .40. T/S FOUND RUDDER HYD TRANSFER VALVE AND LINE LEAKING. REPLACED RUDDER HYD TRANSFER VALVE INSTALLED TEMP LINE.

Part: CONTROLLER — FAILED (CABIN PRESSURE) · airframe 58,429 hrs · 28,883 cycles

BOTH AUTOPRESSURIZATION CONTROLLERS FAILED AT THE SAME TIME AT FL350 WAS ABLE TO CONTROL OUTFLOW VALVE IN MANUAL. DESCENDED TO 10,000 AND DIVERTED TO MCO. REPLACED NR 2 AUTO CONTROLLER DUE TO A LOSS OF AC POWER LAST FLT FAULT ON BITE. BITE AND VERIFICATION OF NR 1 AND NR 2 AUTO CONTROLLERS CHECK OK. MANUAL OPERATION NORMAL.

Part: BATTERY PACK — NOT SEATED (CABIN) · airframe 55,823 hrs · 27,960 cycles

ON TAKEOFF EMERGENCY LIGHTS ON RIGHT SIDE OF CABIN ILLUM. ON PREFLIGHT THIS MORNING FOUND RIGHT EMERGENCY CHARGER C/B POPPED. RESET AFTER TAKEOFF, DISCOVERED RIGHT EMERGENCY CHARGER C/B POPPED AGAIN, LEFT OUT. INSPECTED CHARGER AND CANNON PLUG. RESET BATTERY PACK IN CRADLE. C/B NOW SECURE AND ALL LIGHT OPERATE CORRECTLY.

Part: BEAR STRAP — CRACKED (L1 DOOR CUTOUT) · airframe 54,935 hrs · 27,662 cycles

FUSELAGE BEAR STRAP CRACKED AT THE UPPER FORWARD CORNER OF THE L1 DOOR. REPAIRED IAW ERA 093001-14AD.

Part: SKIN — CORRODED (FUSELAGE) · airframe 54,935 hrs · 27,662 cycles

FUSELAGE SKIN AT STATION 1510 BETWEEN STR 28L - 29L CORRODED. REPAIRED IAW ERA 092820-14.

Part: SWITCH — INCORRECT (EMERGENCY EXIT) · airframe 54,935 hrs · 27,662 cycles

GAP INCORRECT. GAP BETWEEN AUTOFIRE SWITCH ROLLER AND CAM INCORRECT IN RIGHT AFT OVERWING EXIT CUTOUT. REPLACED ADJUSTED GAP BETWEEN AUTO FIRE SWITCH ROLLER AND CAM IN RIGHT AFT OVERWING EXIT PER AMM 25-26-11-404-010. TEST NOW CORRECT PER AMM.

Part: BRACKET — DAMAGED (L-1 DOORWAY) · airframe 54,935 hrs · 27,662 cycles

STA 333.45 STR 7L PULLEY EMERGENCY POWER ASSIST PASSENGER DOOR L-1. PULLEY BRACKET DAMAGED. REMOVED DAMAGED PULLEY BRACKET. REMOVED FASTENER, DRILLED MOUNT HOLES. REPLACED PULLEY BRACKET PER BAC 141N6322. EMERGENCY POWER ASSIST SYSTEM RIGGED ON OPN 7899.

Part: CAM — CORRODED (RT FWD OVERWING) · airframe 54,935 hrs · 27,662 cycles

CAM CORRODED RIGHT OVERWING EXIT HATCH CUTOUT AUTO FIRE SWITCH CAM FWD POSITION. CLEANED CAM AND HAND BURNISHED PAINT AND DIRT RESIDUE. NO CORROSION FOUND PER SRM 51-10-02. CW VISUAL PER SRM 51-10-02, NO CORROSION FOUND. OK TO TREAT AND PAINT. RESTORED FINISH PER SRM 51-10-02.

Part: SWITCH — CORRODED (AFT RH OVERWING) · airframe 54,935 hrs · 27,662 cycles

RIGHT AFT OVERWING EXIT CUTOUT AUTOFIRE SWITCH CAM CORRODED. REMOVED CORROSION PER SRM 53-00-00D FIG 1. OK TO CHECK LIMITS. RIGGED SWITCH PER AMM. FOUND CAM OUT OF LIMITS PER BAC DWG 284N1508 AND REPLACED SWITCH ASSY.

Part: CONTROLLER — INOPERATIVE (CABIN PRESSURE) · airframe 54,202 hrs · 27,412 cycles

AT 37,000 FT CABIN ALTITUDE HORN CAME ON. SWITCHED TO AUTO 2 WITH NO IMMEDIATE ALT MOVEMENT, SO SWITCHED TO MANUAL. REPLACED NR 1 AUTO PRESSURE CONTROLLER.

Part: BOTTLE — DEFECTIVE (CARGO BAY) · airframe 52,953 hrs · 26,968 cycles

NOTICED AFTER COCKPIT INDICATOR LIGHTS TEST, CARGO BOTTLE 1 DISCHARGE LIGHT REMAINED ILLUMINATED WITH ASSOCIATED MESSAGE ON EICAS. REPLACED BOTTLE.

Part: WIRE — BROKEN (SEAT ROW 40DEF) · airframe 51,751 hrs · 26,516 cycles

EMERGENCY PATH LIGHT INOP AT ROW 40DEF. REPAIRED BROKEN WIRE UNDER SEAT TRACK, OPS NORMAL.

Part: LIGHT — INOPERATIVE (40DEF) · airframe 51,285 hrs · 26,338 cycles

EMERGENCY LIGHT AT SEAT 40 DEF INOP. RELAMPED SAME.

Part: ODOR — DETECTED (CABIN) · airframe 49,646 hrs · 25,644 cycles

ON CRUISE F/A SMELT ODOR SIMILAR TO BURNT POPCORN NEAR ROW 33. ENG A/I WAS ON. SMELL DISSIPATED AFTER A/I AND LIGHTS WERE TURNED OFF. OPERATED PACKS BOTH INDEPENDENTLY AND TOGETHER IN FULL HOT POSITION. ALSO RAN BOTH ENG USING INDIVIDUAL ENGS ANTI ICE NO BURNT ODOR SCENTED.

Part: BEAR STRAP — CORRODED (FS 1440, S-25R) · airframe 47,205 hrs · 24,554 cycles

FUSELAGE / SKIN / C2 DOOR CUTOUT / FS 1440 / STRG. 25R-26R: CORROSION BLEND REPAIR THE INTERNAL BEAR STRAP AROUND THE C2 DOOR CUTOUT WAS FOUND WITH AN AREA OF CORROSION NEAR THE AFT EDGE OF THE DOOR AT FS 1440 BETWEEN STRINGERS 25R & 26R. THE CORROSION WAS MACHINED AWAY AND THE AREA REPAIRED WITH AN EXTERNAL ALUMINUM DOUBLER. THE REPAIR WAS ACCOMPLISHED PER ER/A 382009-14, REV A.

Part: SILL — CORRODED (FUSELAGE) · airframe 47,204 hrs · 24,553 cycles

THE LOWER DOOR SILL OF THE C2 DOOR OPENING WAS BADLY CORRODED AND NEEDED TO BE REPLACED.

Part: SPAR — GOUGED (NR 2 PYLON) · airframe 47,204 hrs · 24,553 cycles

THE FWD UPPER SPAR WEB OF THE NR 2 PYLON WAS FOUND WITH A DEEP GOUGE AT NAC STA 128 AT RBL 2. THE WEB WAS CUT FWD AND AFT OF THE DAMAGE AND THE DAMAGED SECTION OF WEB WAS REMOVED. A NEW SECTION OF WEB WAS SPLICED IN WITH ALUMINUM DOUBLERS PER ER/A 381993-14, REV A.

Part: JACKSCREW — DAMAGED (TE FLAP) · airframe 42,042 hrs · 22,579 cycles

ON FINAL FLAPS STUCK AT 17 DEGREES. TRAILING EDGE LIGHT ON. VISUAL INSPECTION SHOWS RIGHT INBOARD T/E FLAPS NOT EXTENDED WITH DAMAGE ON INBOARD SIDE. REPLACED RT I/B FLAP CARRAIGE ROLLER BEARING. REPLACED RIGHT I/B FLAP CARRIAGE JACKSCREW AND GIMBAL ASSY PER M/M. DL (P/N 276701217).

Part: ENGINE — SURGED (NR 2)

DURING CLIMBOUT, RIGHT ENGINE SURGED. FLIGHT CREW ELECTED TO RETARD ENGINE TO IDLE AND RETURN TO LIMA. FERRIED A/C TO ATL FOR ENGINE CHANGE.

Part: MECHANISM — OUT OF ADJUST (PAX DOOR)

RIGHT FWD ENTRY DOOR HANDLE UNLOCKED AFTER T/O AND COULD NOT BE LOCKED. EICAS MSG R FWD ENT DOOR AND ENTRY DOOR LIGHT ON OVERHEAD PANEL CAME ON. ADJUSTED LOWER GATE AND STOP PINS PER MM.

Part: FAIRING — DETACHED (NR 2 ENGINE)

NR 2 ENG FWD PYLON FAIRING DEPARTED AIRCRAFT DURING T/O. RETURNED TO DFW. REPLACED FAIRING.

Part: FM COMPUTER — FAILED (RT SYSTEM)

EICAS MSG - RIGHT FMC FAIL DISPLAYED. DEFERRED PER MEL 34-61-1. S/D REMOVED AND REPLACED RT FMC. OPS CHECK NORMAL.

Part: ENGINE — OVERTEMP (NR 2)

SNN- NR 2 ENGINE EXCEEDED EGT LIMIT 652 DEGREES CELSIUS FOR 20 SECONDS. AREA 'A' ON OVERHEAT CHART. DID NOT OCCUR DURING SURGE. REMOVED AND REPLACED NR 2 ENGINE IAW M57-71-01.

Part: ENGINE — FLAMEOUT (LT ENGINE)

MDW - WHILE ON MAINTENANCE REPOSITIONING THE LEFT ENGINE FLAMED OUT. (MAINTENANCE TAXIING AIRCRAFT TO OTHER GATE). AFTER TROUBLESHOOTING PER THE F/M, THE LEFT ENGINE FUEL FILTER WAS REMOVED AND REPLACED PER MM. PERFORMED RUN UP PER 71-05-00 IN F/M. OPS CHECK GOOD. TORQUED EEC CONNECTORS PER 73-21-04 IN MM. NO EPCS/EICAS SYSTEM LATCH.