N666US
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
Service Difficulty Reports filed with the FAA for this airframe. Filing is largely voluntary — the number of reports is not a measure of reliability. To verify a report, search its control number at the FAA SDRS site.
188 reports on file, 1995-05-10 – 2017-10-29.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 116,854 hrs · 14,407 cycles
UPPER DECK EMERGENCY LIGHTS FWD INOP. REPLACED BATTERY IN PACK M335 PER AMM 33-51-04.
Part: LENS — MISSING (CABIN) · airframe 116,546 hrs · 14,379 cycles
2R LAV RED LENS AND EMERGENCY LIGHT ASSY MISSING ON FLOOR. REPLACED RED LENS ASSEMBLY AS REQUIRED AT DOOR 2R LAV. OPS CHECK GOOD.
Part: GIRT BAR — UNSECURE (L2 DOOR) · airframe 116,484 hrs · 14,374 cycles
UNABLE TO FULLY OPEN THE L2 DOOR. SECURED GIRT BAR IAW AMDS 2560-9901-26. OPS CHECKED GOOD AND PINS REMOVED. OK FOR SERVICE.
Part: SEAL — MISSING (LIFE VEST) · airframe 116,030 hrs · 14,330 cycles
COVER FOR LIFE VEST MISSING THE PIN, CANNOT ATTACH. SECURED COVER AND INSTALLED THE SEAL. CHECKED OK FOR SERVICE.
Part: SWITCH — FAILED (R5 DOOR) · airframe 115,853 hrs · 14,314 cycles
EICAS MSG, DOOR R5 ON SHORT FINAL. INTERMITTENT. HAD PLF MSG 52109 DOOR ENTRY R5 SWITCH FAIL. PER FIM 52-71-00-812-820. REPLACED R5 ENTRY DOOR SWITCH S38 IAW AMM 52-71-01. OP CK GOOD.
Part: PROXIMITY SWITCH — DAMAGED (R5 DOOR) · airframe 115,853 hrs · 14,314 cycles
DOOR 5R ILLUMINATED AFTER TO FOR 15 SECONDS AGAIN ON LANDING FOR A BRIEF MOMENT ACARS TIMES WERE LOST EACH TIME. FOUND SWITCH DAMAGED S1975. REPLACED PROX SWITCH PER WDM 52-73-13 . OPS CKS GOOD.
Part: POWER SUPPLY — INOPERATIVE (CABIN) · airframe 115,581 hrs · 14,289 cycles
EXTERNAL EMERGENCY LIGHT AT LT BODY INOP. REPLACED POWER SUPPLY M7919 IAW AMM 33-51 & OK.
Part: ESCAPE HATCH — UNSECURE (COCKPIT) · airframe 115,473 hrs · 14,278 cycles
SHORTLY AFTER TAKE-OFF, THE COCKPIT ESCAPE HATCH OPENED AND WILL NOT STAY SHUT CAUSING PRESSURIZATION ISSUES AS WELL. DUMPED FUEL, DECLARED AN EMERGENCY AND RETURNED TO DEPARTURE. MAINTENANCE CHECKED THE LATCH IAW AMM 52-21. LATCH OPERATES SMOOTH, CLOSED LATCH, AIRCRAFT OK FOR SERVICE.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 114,886 hrs · 14,228 cycles
RIGHT UPPER DECK EXIT LIGHT AT DOOR IS INOPERATIVE. REPLACED THE BATTERY PACK IAW AMM 33-51.
Part: BATTERY PACK — DISCONNECTED (EMERGENCY LIGHTS) · airframe 114,302 hrs · 14,176 cycles
EMERGENCY LIGHTS INOPERATIVE FROM SEAT 35 TO THE R3 DOOR 3. CONNECTED THE BATTERY PACK AND OPS CHECKED NORMAL.
Part: CLAMP — BROKEN (CARGO BAY) · airframe 114,522 hrs · 14,196 cycles
RAMP REPORTED SPARKS COMING FROM FWD CARGO BENEATH FLOOR. REPAIRED WIRES THAT WERE DAMAGED DUE TO BROKEN CLAMP AND CHAFFING AT STA 560 WL 105 RBL10. REPAIRED WIRES AS PER SWPM 20-10-13 FOR WIRE HARNESS NEEDS TO BE SECURED. WIRES THAT WERE DAMAGED WERE IDENTIFIED FOR FORWARD CARGO LOADING SYSTEM. OPS CHECK OF SYSTEM AND ALL PDUS WORKED EXCEPT FOR BAY 3 RIGHT PDU. OPEN CIRCUIT FROM CONNECTOR M502 PIN 3 OF 3R PDU TO PIN 27 OF CONNECTOR D43446P COMPLETED SECURING HARNESS OK TO DEFER TO MEL 25-53-01. REPAIRED WIRING AT PIN 3 OF CONNECTOR DM502 PER WDM 25-53-24 & SPWM 20-10 CHECKS GOOD PER AMM 25-53 REMOVED PLACARD CLEARED MEL.
Part: SOCKET — DAMAGED (EMERGENCY LIGHT) · airframe 113,939 hrs · 14,136 cycles
LEFT OVERWING EMERGENCY LIGHT INOPERATIVE. REMOVED SHORTED BULB AND REPAIRED THE SOCKET TERMINAL IAW CMM 33-50-18.
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 113,649 hrs · 14,107 cycles
LT WING OTBD T/E FLAP AFT FLAP LOWER SKIN FOUND THREE DELAMINATION. ONE DELAMINATION APPROX 1.5X1.5 INCH FROM T/E 2 INCH AND FROM INBD 132 INCH. ONE DELAMINATION APPROX 1X1 INCH FROM T/E 5 INCH AND FROM INBD 73 INCH. THE OTHER DELAMINATION APPROX 1X1 INCH FROM T/E 2 INCH AND FROM INBD 17 INCH. REPAIRED THE DELAMINATION AREA ON THE AFT FLAP LWR SKIN OF LT WING O/B T/E FLAP. LOCATION: ONE IS FROM T/E 2 INCH AND INBD 132 INCH. ONE IS FROM T/E 5 INCH AND FROM INBD 73 INCH. ONE IS FROM T/E 2 INCH AND FROM INBD 17 INCH IAW B747-400 SRM 51-70-07 PARA. 5. A(1) FIG. 5 REV. 98. JOB COMPLETED. (2875135)
Part: STRUCTURE — CRACKED (BS 1480 BULKHEAD) · airframe 113,649 hrs · 14,107 cycles
CRACK AT BS 1480 BULKHEAD STRINGER 34R. REPAIR IAW ERA 550542-14, REV. 0 .
Part: BEAM — CRACKED (VERTICAL STAB) · airframe 113,649 hrs · 14,107 cycles
CRACK IN RT T/E BEAM OF VERTICAL STAB VSS 182.7. REPAIRED IAW SRM 55-30-13, REPAIR 2, REV 98.
Part: SKIN — DELAMINATED (LT AILERON) · airframe 113,649 hrs · 14,107 cycles
LEFT WING INBD AILERON TOP SKIN FOUND TWO DELAMINATION. ONE DELAMINATION APPROX 2X9 INCH FROM T/E 12 INCH AND FROM OTBD 30 INCH. THE OTHER DELAMINATION APPROX 2X3 INCH FROM L/E 13 INCH AND FROM INBD 23 INCH. REPAIRED THE DELAMINATION AREA ON THE TOP SKIN OF LT WING I/B AILERON. LOCATION: ONE IS FROM T/E 12 INCH AND FROM OTBD 30 INCH. THE OTHER IS FROM L/E 13 INCH AND FROM INBD 23 INCH IAW B747-400 SRM 51-70-07 PARA. 5. A(1) FIG. 5 REV. 98. JOB COMPLETED. (2875149)
Part: BEAM — CRACKED (VERTICAL STAB) · airframe 113,649 hrs · 14,107 cycles
CRACK AT RT T/E BEAM OF THE VERTICAL STAB VSS 182.7. REPAIRED IAW SRM 55-30-13, REPAIR 2, REV. 98.
Part: BEAM — CRACKED (VERTICAL STAB) · airframe 113,649 hrs · 14,107 cycles
CRACK AT THE RT T/E BEAM OF VERTICAL STAB VSS 157.7. REPAIRED IAW SRM 55-30-13, REPAIR 2, REV 98.
Part: SKIN — DELAMINATED (LT AILERON) · airframe 113,662 hrs · 14,108 cycles
LEFT WING INBD AILERON TOP SKIN FOUND TWO DELAMINATION APPROX 3X3 INCH. ONE IS FROM L/E 5 INCH AND FROM OTBD 4 INCH THE OTHER IS FROM T/E 6 INCH AND FROM INBD 16 INCH. REPAIRED IAW SRM 51-70-06 PARA. 5. A. (1) FIG. 5 REV. 98.
Part: SKIN — DENTED (L5 DOOR) · airframe 113,649 hrs · 14,107 cycles
DENT ON EXTERIOR SKIN OF THE L5 ENTRY DOOR,
Part: SKIN — DENTED (L5 DOOR) · airframe 113,649 hrs · 14,107 cycles
DENT ON EXTERIOR SKIN AT THE L5 ENTRY DOOR LOWER. CUT OUT THE DAMAGE AREA IAW SRM 52-00-01, REPAIR 8.P PERFORMED HFEC INSPECTION. FABRICATED A REPAIR IAW SRM 52-00-01, REPAIR 8. INSTALLED THE REPAIR IAW SRM 51-20-05 REV 98.
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 113,649 hrs · 14,107 cycles
LT WING OTBD T/E FLAP AFT FLAP TOP SKIN FOUND THREE DELAMINATION ONE DELAMINATION APPROX 3.5X2 INCH FROM T/E 2 INCH AND FROM INBD 176 INCH ONE DELAMINATION APPROX 5X2 INCH FROM T/E 2 INCH AND FROM OTBD 37 INCH THE OTHER DELAMINATION APPROX 2X2 INCH FROM T/E 1 INCH AND FROM OTBD 91 INCH. REPAIRED THE AFT FLAP TOP SKIN DELAMINATION AREA OF LT WING O/B T/E FLAP LOCATION: ONE IS FROM T/E 2 INCH AND FROM I/B 176 INCH ONE IS FROM T/E 2 INCH AND FROM O/B 37 INCH ONE IS FROM T/E 1 INCH AND FROM O/B 91 INCH IAW B747-400 SRM 51-70-07 PARA. 5. A(1) FIG. 5 REV. 98 JOB COMPLETED. (2874905)
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 113,649 hrs · 14,107 cycles
RIGHT WING INBD T/E FLAP AFT FLAP TOP SKIN FOUND TWO DELAMINATION ONE IS FROM T/E 15 INCH AND FROM INBD 98 INCH APPROX 11X10 INCH THE OTHER IS FROM T/E 4.5 INCH AND FROM INBD 180 INCH APPROX 1X1 INCH. REPAIRED IAW SRM 51-70-07 PARA. 5. A(1) FIG 5 REV 98.
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 113,649 hrs · 14,107 cycles
LEFT WING INBD T/E FLAP AFT FLAP TOP SKIN FOUND TWO AREAS DELAMINATION ONE DELAMINATION APPROX 1.5X1 INCH FROM T/E 5.5 INCH AND FROM INBD 151 INCH THE OTHER APPROX 3.5X2 INCH FROM T/E 2 INCH AND FROM INBD 176 INCH. REPAIRED IAW SRM 51-70-07 PARA. 5. A(1) FIG. 5 REV. 98.
Part: SKIN — NICKED (BS 480-500) · airframe 113,649 hrs · 14,107 cycles
NICK ON EXTERIOR SKIN BS 480 - 500, S45R. CUT OUT THE DAMAGE AREA IAW SRM 53-00-01, REPAIR 1. INSTALL THE REPAIR IAW SRM 51-20-05.
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 113,649 hrs · 14,107 cycles
LEFT WING INBD T/E FLAP AFT FLAP TOP SKIN FOUND TWO AREAS DELAMINATION APPROX 1X1 INCH. ONE IS FROM T/E 1.5 INCH AND FROM INBD 128 INCH THE OTHER IS FROM T/E 5 INCH AND FROM OTBD 111 INCH. REPAIRED THE IAW SRM 51-70-07 PARA. 5. A(1) FIG. 5 REV. 98.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 113,649 hrs · 14,107 cycles
RIGHT WING OTBD T/E FLAP MID FLAP TOP SKIN FOUND TWO DELAMINATION APPROX 1.5X1.5 ONE IS FROM T/E 9 INCH AND FROM OTBD 123 INCH THE OTHER IS FROM T/E 11 INCH AND FROM INBD 143 INCH. REPAIRED THE DELAMINATION AREA ON THE MID FLAP OF RH WING O/B T/E FLAP LOCATION: ONE IS FROM T/E 9 INCH AND FROM OTBD 123 INCH THE OTHER IS FROM T/E 11 INCH AND FROM INBD 143 INCH, IAW B747-400 SRM 51-70-07 PARA. 5. A (1) FIG 5 REV 98. JOB COMPLETED. (2874987)
Part: SKIN — DELAMINATED (RT AILERON) · airframe 113,649 hrs · 14,107 cycles
RIGHT WING INBD AILERON TOP SKIN FOUND ONE DELAMINATION APPROX 5X8 INCH FROM T/E 4 INCH AND FROM INBD 13 INCH. REPAIRED THE DELAMINATION AREA ON THE INBD AILERON OF RH WING, LOCATION: FROM T/E 4 INCH AND FROM INBD 13 INCH, IAW B747-400 SRM 51-70-07 PARA. 5. A(1) FIG5 REV 98. JOB COMPLETED. (2874975)
Part: SKIN — DELAMINATED (LT AILERON) · airframe 113,649 hrs · 14,107 cycles
LEFT WING OTBD AILERON FOUND SOME DELAMINATION. REPAIRED THE DAMAGED AREA OF LT WING OTBD AILENRON IAW B747-400 SRM 51-70-07 PARA. 5. 5A. 1 FIG 5 REV. 98.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 113,649 hrs · 14,107 cycles
RIGHT WING OTBD T/E FLAP AFT FLAP TOP SKIN FOUND TWO AREAS OF DELAMINATION APPROX 2X2 INCH ONE IS FROM T/E 5 INCH AND FROM INBD 151 INCH THE OTHER IS FROM T/E 1 INCH AND FROM OTBD 134 INCH. REPAIRED IAW SRM 51-70-07 PARA. 5. A(1) FIG 5 REV 98.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 113,649 hrs · 14,107 cycles
RIGHT WING OTBD T/E FLAP MID FLAP TOP SKIN FOUND THREE DELAMINATION ONE IS FROM T/E 8 INCH AND FROM OTBD 31 INCH APPROX 1X1 INCH ONE IS FROM T/E 6 INCH AND FROM INBD 131 INCH APPROX 7X3 INCH THE OTHER IS FROM T/E 8 INCH AND FROM INBD 17 INCH APPROX 4X1.5 INCH. REPAIRED THE DELAMINATION AREA ON THE MID FLAP OF RH WING O/B T/E FLAP, LOCATION: ONE IS FROM T/E 8 INCH AND FROM OTBD 31 INCH APPROX 1X1 INCH ONE IS FROM T/E 6 INCH AND FROM INBD 131 INCH THE OTHER IS FROM T/E 8 INCH AND FROM INBD 17 INCH, IAW B747-400 SRM 51-70-07 PARA. 5. A (1) FIG5 REV 98. JOB COMPLETED. (2874981)
Part: SKIN — DELAMINATED (RT AILERON) · airframe 113,649 hrs · 14,107 cycles
RT WING OTBD AILERION TOP SKIN FOUND SOME DELAMINATION. REPAIRED THE DAMAGED AREA ON THE TOP SKIN OF RT WING OTBD AILENRON IAW SRM 51-70-07 PARA. 5. A. 1 FIG 5 REV. 98.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 113,649 hrs · 14,107 cycles
RIGHT WING T/E FLAP MID FLAP TOP SKIN FOUND TWO DELAMINATION ONE IS FROM T/E 6 INCH AND FROM OTBD 103 INCH APPROX 5 X 1.5 INCH THE OTHER IS FROM T/E 13 INCH AND FROM OTBD 118 INCH APPROX 1X1 INCH. REPAIRED IAW SRM 51-70-06 PARA. 5. A (1) FIG. 5 REV. 98.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 113,649 hrs · 14,107 cycles
RIGHT WING OTBD T/E FLAP AFT FLAP TOP SKIN FOUND ONE AREA DELAMINATION APPROX 5X6 INCH FROM T/E 3 INCH AND FROM INBD 104 INCH. REPAIRED IAW SRM 51-70-07 PARA. 5. A (1) FIG 5 REV 98.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 113,649 hrs · 14,107 cycles
RIGHT WING INBD T/E FLAP AFT FLAP LOWER SKIN FOUND THREE DELAMINATION ONE IS FROM T/E 9 INCH AND FROM OTBD 152 INCH APPROX 4.5X2 INCH ONE IS FROM T/E 4 INCH AND FROM INBD 152 INCH APPROX 10X2.5 INCH THE OTHER IS FROM T/E 3 INCH AND FROM INBD 138 INCH APPROX 2X3 INCH. REPAIRED IAW SRM 51-70-07 PARA. 5. A(1) FIG 5 REV 98.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 113,649 hrs · 14,107 cycles
RIGHT WING OTBD T/E FLAP AFT FLAP TOP SKIN FOUND TWO AREAS OF DELAMINATION, APPROX 1X1 INCH ONE IS FROM T/E 3 INCH AND FROM OTBD 64 INCH THE OTHER IS FROM T/E 3 INCH AND FROM OTBD 118 INCH. REPAIRED THE RT WING O/B T/E FLAP IAW SRM 51-70-07, PARA 5. A(1), FIG 5, REV 98.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 113,649 hrs · 14,107 cycles
RIGHT WING OTBD T/E FLAP AFT FLAP TOP SKIN FOUND TWO AREAS DELAMINATION. ONE IS FROM T/E 1 INCH AND FROM INBD 3.5 INCH APPROX 1X1 INCH THE OTHER IS FROM T/E 2 INCH AND FROM OTBD 56 INCH APPROX 1X1 INCH. REPAIRED THE RT WING T/E FLAP IAW SRM 51-70-07, PARA 5, A (1), FIG. 5, REV 98.
Part: SKIN — DELAMINATED (LT WING TE FLAP) · airframe 113,649 hrs · 14,107 cycles
LEFT WING INBD T/E FLAP AFT FLAP TOP SKIN FOUND TWO DELAMINATION APPROX 2X2 INCH ONE IS FROM T/E 3 INCH AND FROM INBD 104 INCH THE OTHER IS FROM T/E 9 INCH AND FRM INBD 109 INCH. REPAIRED IAW SRM 51-70-07 PARA. 5. A (1) FIG. 5 REV. 98.
Earlier reports · 1995–2016 · 150 reports
2016
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 113,329 hrs · 14,076 cycles
DURING SERVICE CHECK, FOUND EMERGENCY LIGHTS OUT FWD OF THE R2 DOOR AND ALL EXIT MARKERS AS WELL. REPLACED THE BATTERY BACK IAW AMM 33-51.
Part: STRUCTURE — CRACKED (NR 4 NACELLE) · airframe 113,182 hrs · 14,064 cycles
FOUND NR 4 ENGINE NACELLE FLANGE CRACKED AND MISSING RIVETS AT NR 2 FORWARD FAIRING ATTACH POINT. C/W ERA 552527-14 REV O FOR REPAIR TO NR 4 ENGINE NACELLE DAMAGE.
Part: ACCESS DOOR — CORRODED (RT WING) · airframe 113,182 hrs · 14,064 cycles
CORROSION REPAIR ACCESS DOOR 653EB LOWER SKIN RT WING. PERFORM DETAILED VISUAL INSPECTION OF CORROSION REPAIR AT 653EB FUEL TANK ACCESS DOOR CUTOUT PER SRM 57-20-01, REPAIR 4, PAGE 206 & 207.
Part: ACCESS DOOR — CORRODED (LT WING) · airframe 113,182 hrs · 14,064 cycles
CORROSION REPAIR ACCESS DOOR 545CB LOWER SKIN LT WING. PERFORM DETAILED VISUAL INSPECTION OF CORROSION REPAIR AT 545CB FUEL TANK ACCESS DOOR CUTOUT PER SRM 57-20-01, REPAIR 4, PAGE 206 & 207.
Part: ACCESS DOOR — CORRODED (RT WING) · airframe 113,182 hrs · 14,064 cycles
CORROSION REPAIR ACCESS DOOR 652BB LOWER SKIN RT WING. PERFORM DETAILED VISUAL INSPECTION OF CORROSION REPAIR AT 652BB FUEL TANK ACCESS DOOR CUTOUT PER SRM 57-20-01, REPAIR 4, PAGE 206 & 207.
Part: ACCESS DOOR — CORRODED (RT WING) · airframe 113,182 hrs · 14,064 cycles
CORROSION REPAIR ACCESS DOOR 652AB LOWER SKIN RT WING. PERFORM DETAILED VISUAL INSPECTION OF CORROSION REPAIR AT 652AB FUEL TANK ACCESS DOOR CUTOUT PER SRM 57-20-01, REPAIR 4, PAGE 206 & 207.
Part: ACCESS DOOR — CORRODED (RT WING) · airframe 113,182 hrs · 14,064 cycles
CORROSION REPAIR ACCESS DOOR 646AB LOWER SKIN RT WING. PERFORM DETAILED VISUAL INSPECTION OF CORROSION REPAIR AT 646AB FUEL TANK ACCESS DOOR CUTOUT PER SRM 57-20-01, REPAIR 4, PAGE 206 & 207.
Part: ACCESS DOOR — CORRODED (RT WING) · airframe 113,182 hrs · 14,064 cycles
CORROSION REPAIR ACCESS DOOR 653AB LOWER SKIN RT WING. PERFORM DETAILED VISUAL INSPECTION OF CORROSION REPAIR AT 653AB FUEL TANK ACCESS DOOR CUTOUT PER SRM 57-20-01, REPAIR 4, PAGE 206 & 207.
Part: ACCESS DOOR — CORRODED (RT WING) · airframe 113,182 hrs · 14,064 cycles
CORROSION REPAIR ACCESS DOOR 652CB LOWER SKIN RT WING. PERFORM DETAILED VISUAL INSPECTION OF CORROSION REPAIR AT 652CB FUEL TANK ACCESS DOOR CUTOUT PER SRM 57-20-01, REPAIR 4, PAGE 206 & 207.
Part: ACCESS DOOR — CORRODED (RT WING) · airframe 113,182 hrs · 14,064 cycles
CORROSION REPAIR ACCESS DOOR 652DB LOWER SKIN RT WING. PERFORM DETAILED VISUAL INSPECTION OF CORROSION REPAIR AT 652DB FUEL TANK ACCESS DOOR CUTOUT PER SRM 57-20-01, REPAIR 4, PAGE 206 & 207.
Part: ACCESS DOOR — CORRODED (RT WING) · airframe 113,182 hrs · 14,064 cycles
CORROSION REPAIR ACCESS DOOR 645BB LOWER SKIN RT WING. PERFORM DETAILED VISUAL INSPECTION OF CORROSION REPAIR AT 645BB FUEL TANK ACCESS DOOR CUTOUT PER SRM 57-20-01, REPAIR 4, PAGE 206 & 207.
Part: FUSE — MISSING (POWER SUPPLY) · airframe 110,058 hrs · 13,704 cycles
EMERGENCY LIGHTS AT ROW 77-79 ARE INOPERATIVE. INSTALLED FUSES THAT WERE MISSING FROM R & R POWER SUPPLY. OPS CHECK EMERGENCY LIGHTS GOOD.
2015
Part: ENGINE — FLAMED OUT (NR 3) · airframe 107,923 hrs · 13,439 cycles
DURING CLIMB FROM FL380 TO FL390 ENGINE NR 3 FLAMED OUT. GOT CLEARANCE TO FL300 AND ATTEMPTED RESTART AT FL300, UNSUCCESSFUL. COMPLETED QRH PROCEDURE ENGINE FLAME OUT AT APPROXIMATELY 1740Z. NR 3 ENGINE OIL PRESSURE STAYED AT 12-14 REST OF FLT NR 3 ENGINE CHANGE WAS SCHEDULED AND R & R NR 3 ENGINE IAW LOG 1991625.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 107,344 hrs · 13,369 cycles
FWD HALF OF SEAT MOUNTED AISLE EMERGENCY LIGHT IN U/D INOPERATIVE. REPLACED POWER SUPPLY AT ROW 73 LT OVHD. REF AMM 33-50.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 106,712 hrs · 13,296 cycles
UPPER DECK 1ST SECTION EMERGENCY LIGHTS ON FOR 5 SECONDS THEN OUT. REPLACED BATTERY PACK.
Part: SKIN — DEFORMED (CARGO DOOR) · airframe 106,538 hrs · 13,275 cycles
SKIN FWD LOWER CORNER AFT CARGO DOOR DEFORMED. INSTALLED REPAIR DOUBLER AND SEAL RETAINER IAW SRM 52.
Part: BULKHEAD — CRACKED · airframe 106,538 hrs · 13,275 cycles
CRACK ABOUT 1 INCH, OCCURED AT AFT INNER SURFACE 8 O'CLOCK LT SIDE BULKHEAD. INNER CHORD CRACKED AREA AT 8 O'CLOCK LT SIDE BULKHEAD 2598 CUT AND REMOVED, REPAIR PARTS INSTALLED IAW SRM.
2014
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 106,067 hrs · 13,211 cycles
ISLE EMERGENCY LIGHTS ARE OUT ROW 77-79 UPPER DECK. R & R BATTERY PACK.
Part: ENGINE — FAILED (NR 3) · airframe 104,763 hrs · 13,067 cycles
SHORTLY AFTER TAKEOFF, NR 3 ENGINE SHUTDOWN DUE TO EGT REDLINE. ACFT RETURNED TO DEPARTURE. AFTER LANDING, MAINTENANCE FOUND METAL IN TAIL PIPE. ENGINE CHANGED.
Part: LIGHT — MALFUNCTIONED (L4 DOOR SLIDE) · airframe 104,711 hrs · 13,060 cycles
L4 DOOR EMERGENCY SLIDE LIGHT ILLUMINATED ONCE ACFT POWER OFF WITH EMERGENCY LIGHT SWITCHED OFF. REPLACED EMERGENCY LIGHT ASSY.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 103,336 hrs · 12,903 cycles
DURING A NON-ROUTINE CHECK, RED EMERGENCY PATHWAY LIGHTS AT R2 DOOR FWD AND SEAT 35H INOPERATIVE. FOUND CONNECTOR DISCONNECTED, CONNECTED. OPS CHECKED NORMAL.
2013
Part: LIGHT — MALFUNCTIONED · airframe 100,736 hrs · 12,598 cycles
R5 DOOR EMERGENCY LIGHT WILL NOT TURN OFF. REPLACED EMERGENCY LIGHT IAW AMM 33-51. OPS CHECKED GOOD.
Part: DOUBLER — CRACKED · airframe 99,433 hrs · 12,430 cycles
1.4 INCH CRACK FOUND ON THE RADIUS OF THE RT SIDE UPPER LOBE DOUBLER.
Part: SUPPORT BRACKET — CRACKED (LT WING) · airframe 99,433 hrs · 12,430 cycles
LT WING REFUEL PANEL WS 807 -FLAP CAVITY CUTOUT SUPPORT BRACKET FOUND CRACKED. LT WING REFUEL PANEL WS 807 -CRACKED SUPPORT BRACKET AT FLAP CAVITY CUTOUT REPAIRED IAW SRM 57-41-13, REPAIR 3.
Part: WEB — CRACKED (BS 2238) · airframe 99,433 hrs · 12,430 cycles
R-5 DOOR FWD CUTOUT AREA CRACKED FRAME WEB AT BS 2238 S25R. R & R IAW SRM 51-40-02, PAGE 1 TO 6 AND DWG 65B05000.
Part: STRUCTURE — CRACKED (HORIZONTAL STAB) · airframe 99,433 hrs · 12,430 cycles
CRACK FOUND AT FASTENER HOLE A2 IN THE VICINITY OF RBL 43S. FASTENER HOLE A2 AT HORIZ STABILIZER CENTER SECTION, RBL 40 WAS REPAIRED IAW ERA 512576-14 AD REV ORIGINAL .
Part: SKIN — DAMAGED (RT WING TE FLAP) · airframe 99,431 hrs · 12,429 cycles
RT WING L/E -BETWEEN NR 14 KRUEGER FLAP & WING FASTENER HOLES FOUND ELONGATED. REPAIRED THE SKIN IAW TO SRM 57-41-01.
Part: CARGO TRACK — CORRODED (BS 1860) · airframe 99,431 hrs · 12,429 cycles
CORROSION ON CARGO TRACK BS 1860 RBL 58. CARGO TRACK R & R IAW SRM 51-40-02, PAGE 1 TO 6 AND DWG 65B06061.
Part: FRAME — CRACKED (BS 320) · airframe 99,431 hrs · 12,429 cycles
THE RT HALF OF LOWER CHORD (PN 65B073033-33) WAS FOUND A 0.22" LONG CRACK AT STA 320, RBL 30, THE 4 TH FASTENER HOLE STA 320, RBL 30-CRACK AT 4TH FASTENER HOLE FROM THE RT SIDE MOST END OF RT HALF LOWER CHORD (PN 65B076303-33) WAS REPAIRED IAW ERA 512575-14AD, REV ORIGINAL ASSOCIATED ER/A 14-512575 E FROM THE RT SIDE MOST ENG.
2012
Part: SKIN — CRACKED (FUSELAGE) · airframe 97,559 hrs · 12,177 cycles
FOUND ON ARRIVAL .5" CRACK ON ACFT LT AFT FUSELAGE, VENT WASTE SYS, OVERBOARD AREA. REPAIRED IAW ERA 508004-14. DAMAGE CUT OUT INTERNAL DOUBLER MADE. COMPLETED REPAIR IAW ERA 508004-14 AS PERMANENT REPAIR IAW PS 900-5-1 739058.
Part: SPLICE — CORRODED (BS 960-980) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION, FOUND CORROSION ON DRAG SPLICE FITTINGS AT BS 960-990, S38L. MAINTENANCE REMOVED CORRODED DRAG SPLICE FITTING. INSTALLED NEW FITTING PER PRI 502620-14AD REV 4.
Part: SKIN — DAMAGED (BS 990) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION FOUND ONE HOLE DAMAGED AT BS 990 STRINGER 39L END FITTING. MAINTENANCE REPAIRED.
Part: SKIN — DAMAGED (BS 996) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION FOUND DOUBLE HOLE (01EA) ON LOWER SKIN AT BS 996 STR-39L. MAINTENANCE REPAIRED.
Part: SKIN — CRACKED (BS 980) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION, A CRACK WAS FOUND ON BS 980 SKIN. MAINTENANCE REPAIRED PER ERA 502620-14AD.
Part: FRAME — CRACKED (BS 800) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION, FOUND CRACKS ON FRAME AT BS 800. MAINTENANCE REPAIRED PER ERA 502637-14AD.
Part: SKIN — CRACKED (BS 2285) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION, FOUND A CRACK AT THE NR 5 RIGHT MED CUTOUT, UPPER AFT CORNER, BS 2285. ER/A 502022-14 SECTION I WAS ACCOMPLISHED.
Part: WEB — CRACKED (BS 1265) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION, A CRACK WAS FOUND ON THE WEB. MAINTENANCE ACCOMPLISHED ERA 502611-14 SECTION 1 REPAIR.
Part: FLOOR SUPPORT — CORRODED (BS860 RBL116) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION, FOUND CORRISION ON MAIN DECK FLOOR STRUCTURE AT APPROX. BS 860 RBL 116. MAINTENANCE REMOVED CORRODED FLOOR SUPPORT AND INSTALLED NEW EWM FLOOR SUPPORT.
Part: FRAME — CRACKED (BS 140 BULKHEAD) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION, FOUND A CRACK ON BS 140 BULKHEAD OUTER RING CHORD. ER/A 503069-14 SECTION I WAS ACCOMPLISHED.
Part: SKIN — CRACKED (FUSELAGE) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION, A CRACK WAS FOUND ON THE NR 3 CABIN WINDOW CUTOUT, LOWER AFT CORNER. A REPAIR WAS INSTALLED PER ER/A 502618-14 SECTION I.
Part: DOUBLER — CRACKED (BS 1200 FRAME) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION FOUND CABIN ZONE C LT STA 1200 TENSION TIE FRAME DOUBLER FOUND CRACKED. MAINTENANCE REMOVED DOUBLER AND INSTALLED NEW FRAME DOUBLER AS PER B747-400 SRM 51-40-02.
Part: WEB — CRACKED (BS 1240-1260) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION FOUND CRACK AT THE WEB BETWEEN BS 1240 AND 1260 STR 6 TO 7R. MAINTENANCE REMOVED AREA PER SRM 51-40-02. NEW WEB FABRICATED AS PER DWG 69B04913 REV E. NEW WEB AT MAIN DECK CABIN BETWEEN BS 1240 AND 1260 STR 6 TO 7R AREA INSTALLED AS PER SRM 51-40-02.
Part: DOUBLER — CRACKED (BS 1200 FRAME) · airframe 65,648 hrs · 11,953 cycles
DURING INSPECTION FOUND CRACK AT THE TENSION TIE STATION STA1200 RT FRAME DOUBLER. MAINTENANCE REMOVED DOUBLER AND INSTALLED WITH NEW FRAME DOUBLER AS PER B747-400 SRM 51-40-02.
Part: SHEAR TIE — CRACKED (BS 1180) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION FOUND CABIN ZONE C BS 1180 TENSION TIE FRAME SHEAR TIE CRACKED. MAINTENANCE REMOVED AREA PER SRM 51-40-02. NEW SHEAR TIE CLIP FABRICATED AS PER BOEING DWG 65B01752 REV A. NEW SHEAR TIE CLIP INSTALLED AT CABIN ZONE C STA 1180 TENSION TIE FRAME AREA AS PER SRM 51-40-02.
Part: FRAME — CRACKED (BS 1220) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION FOUND CRACK AT THE TENSION TIE BS 1220 RIGHT FRAME DOUBLER. MAINTENANCE REMOVED CRACKED DOUBLER AND INSTALLED WITH NEW FRAME DOUBLER AS PER B747-400 SRM 51-40-02.
Part: CHANNEL — CRACKED (BS 1200) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION FOUND CRACK 01 ON TENSION TIE FORWARD CHANNEL AT BS 1200 LT. MAINTENANCE REPLACED AREA AS PER SRM 53-40-30 REPAIR 1 F.
Part: FLOOR SUPPORT — CRACKED (BS 500-520) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION FOUND CRACK AT THE FLOOR SUPPORT WEB UPPER CHORD AT STA 500 TO STATION 520, RBL7.0 AREA REMOVED AS PER SRM 51-40-02. NEW UPPER CHORD ANGLE FABRICATED AS PER DWG 69B1965. INSTALLED NEW UPPER CHORD ANGLE AT CABIN STA 500 TO STA 520 RBL 7.0 AREA PER SRM 51-40-02.
Part: FLOORBEAM — CRACKED (BS 1720) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION FOUND CRACK AT THE FLOORBEAM WEB UPPER CHORD AT STA 1720, LBL 67.0. MAINTENANCE REMOVED CRACKED ANGLE AT FLOORBEAM WEB UPPER AT STA 1700 TO 1720 LBL 67.0 PER B747-400 SRM 51-40-02. NEW UPPER CHORD ANGLE FABRICATED AS PER BOEING DWG 65B08914. INSTALLED NEW UPPER CHORD ANGLE AT STATION 1700 TO 1720 LBL 67.0 FLOORBEAM WEB AREA PER B747-400 SRM 51-40-02.
Part: FLOOR SUPPORT — CRACKED (BS 500-520) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION CRACK FOUND AT THE FLOOR SUPPORT WEB UPPER CHORD AT BS 500 TO 520 LBL 67.0 ON FLOOR SUPPORT WEB AREA, REMOVED AS PER SRM 51-40-02. NEW UPPER CHORD ANGLE FABRICATED AS PER DWG 69B19165. NEW UPPER CHORD INSTALLED AS PER SRM 51-40-02.
Part: FLOOR SUPPORT — CRACKED (BS 1700-1720) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION FOUND CRACK AT THE FLOOR SUPPORT WEB UPPER CHORD AT BS 1700 TO 1720, RBL 67.0. MAINTENANCE REMOVED FLOOR SUPPORT WEB AREA PER SRM 51-40-02. NEW UPPER CHORD FABRICATED AS PER BOEING DWG 65B08914 REV Y. NEW UPPER CHORD ANGLE AT CABIN BS 1700 TO 1720 RBL 67.0 FLOORBEAM WEB AREA INSTALLED AS PER SRM 51-40-02.
Part: CHANNEL — CRACKED (BS 1220) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION FOUND ONE CRACK ON TENSION TIES FORWARD 'C' CHANNEL AT BS 1220. REPAIRED AS PER SRM 53-40-30, REPAIR 1, FIGURE 201.
Part: FRAME — CRACKED (BS 800 S17) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION, FOUND CRACK AT RIGHT BS 800 FRAME AT STRINGER 17. REPAIRED PER ERA 502637-14AD.
Part: FRAME — CRACKED (BS 800 S17) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION, FOUND CRACK AT RIGHT BS 800 FRAME AT STRINGER 17. REPAIRED PER ERA 502637-14AD.
Part: CHANNEL — CRACKED (BS 1160) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION FOUND CRACK 01EA ON TENSION TIES FORWARD 'C' CHANNEL AT BS 1160. REPAIRED TENSION TIES CRACKS PER SRM 53-40-30 REPAIR 1, FIG 201.
Part: CHANNEL — CRACKED (BS 1200) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION FOUND ONE CRACK ON TENSION TIES FORWARD 'C' CHANNEL AT BS 1200. REPAIRED AS PER SRM 53-40-30 REPAIR 1 FIG 201.
Part: FRAME — CRACKED (BS 1265) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION, FOUND CRACK INDICATION ON BS 1265 FRAME AT STRINGER 26R. MAINTENANCE REPAIRED AREA PER PRI 502611-14AD REV 0 AND REV 1. COMPARED TO ER/A 502611-14AD REV.0 FOUND COMPLIANT.
Part: SKIN — CRACKED (PAX DOOR) · airframe 95,648 hrs · 11,953 cycles
DURING INSPECTION, MAINTENANCE FOUND NR 5R MAIN ENTRY DOOR AFT UPPER CORNER CUTOUT CRACKED. CRACK REPAIRED PER ERA 505022-14.
Part: WINDOW FRAME — CRACKED (COCKPIT) · airframe 95,648 hrs · 11,953 cycles
NR 3 WINDOW FRAME CRACKED. REPAIRED PER PRI 502618-14E REV 0 AND REV. 1.
Part: SKIN — CRACKED (BS 982 S38L) · airframe 95,648 hrs · 11,953 cycles
DURING UT INSPECTION, FOUND HOLE CRACK 01 EA ON SKIN AT STA 982 STR-38L UNDER LWR DRAG SPLICE FTG (NR 6 HOLE FROM STA 990. CRACK REPAIRED PER ERA 502620-14AD.
Part: SKIN — CRACKED (BS 395 S7R) · airframe 95,648 hrs · 11,953 cycles
DURING HFEC SURFACE INSPECTION, FOUND CRACK APPROX 1/2 INCH AT RT FUSELAGE SKIN BS 395 STR-7R. CRACK REPAIRED PER SRM 53-00-01 REPAIR 1, FIGURE 201.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 95,418 hrs · 11,919 cycles
DURING A MAINTENANCE VISIT, THE EMERGENCY DOOR EXIT LIGHT AT DOOR 4R WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE LIGHT ASSEMBLY TO BE DEFECTIVE AND REPLACED IT. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHT ASSEMBLY WAS REPLACED.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 94,786 hrs · 11,844 cycles
DURING A MAINTENANCE VISIT, THE EMERGENCY DOOR EXIT LIGHT AT DOOR 4R WAS FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE LIGHT ASSEMBLY TO BE DEFECTIVE AND REPLACED IT. SYSTEM OPERATION WAS NORMAL AFTER THE LIGHT ASSEMBLY WAS REPLACED.
2011
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 93,330 hrs · 11,677 cycles
DURING A MAINTENANCE VISIT, THE EMERGENCY LIGHT AFT OF DOOR 1L LAVATORY THROUGH DOOR 2L WILL NOT ILLUMINATE. MAINTENANCE RECONNECTED THE WIRING CONNECTOR AT 10AB. SYSTEM OPERATION WAS NORMAL AFTER THE CONNECTOR WAS RECONNECTED.
Part: CONNECTOR — DAMAGED (CABIN) · airframe 92,086 hrs · 11,524 cycles
DURING A LINE CHECK, MAINTENANCE FOUND THE LEFT, ROW 10-12 EMERGENCY PATH FLOOR LIGHTS INOPERATIVE. MAINTENANCE REPAIRED A CONNECTION. OPERATIONAL CHECK WAS GOOD.
Part: CONNECTOR — UNSECURE (CABIN) · airframe 92,086 hrs · 11,524 cycles
DURING A LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTS AT THE F/A SEAT AT DOOR 4R INOPERATIVE. MAINTENANCE SECURED A CONNECTOR. OPERATIONAL CHECK WAS GOOD.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT) · airframe 4,473 hrs · 553 cycles
DURING A MX VISIT, THE EMERGENCY LIGHT AT ZONE B, LT SIDE, WERE FOUND TO BE INOPERATIVE. MX FOUND THE CABLE PLUG AT THE FLOOR LOOSE AND INSTALLED THE PLUG. SYSTEM OPS WAS NORMAL AFTER THE PLUG WAS INSTALLED.
Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 91,653 hrs · 11,471 cycles
DURING A LINE CHECK, MX FOUND AN EMERGENCY PATH LIGHT AT DOOR 4 RT INOPERATIVE. MX RECONNECTED AWIRE. OPS CHECK WAS GOOD.
Part: WIRE — DISCONNECTED (EMERGENCY LIGHT) · airframe 91,653 hrs · 11,471 cycles
DURING A LINE CHECK, MX FOUND THE EMERGENCY PATH LIGHTS AT SEATS 51C AND 52C INOPERATIVE. MX RECONNECTED A WIRE. OPS CHECK WAS GOOD.
Part: WIRE — DISCONNECTED (CABIN) · airframe 91,426 hrs · 11,443 cycles
DURING A MAINTENANCE VISIT, THE EMERGENCY ESCAPE PATH FLOOR TRACK LIGHTING AT SEATS 51 AND 52 WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE WIRE DISCONNECTED AT SEAT 52C AND RECONNECTED IT. SYSTEM OPERATION WAS NORMAL AFTER THE WIRE WAS RECONNECTED.
Part: CONNECTOR — BROKEN (EMERGENCY LIGHTS) · airframe 91,177 hrs · 11,418 cycles
DURING A MAINTENANCE VISIT, THE FLOOR PROXIMITY EMERGENCY LIGHTS AT A-ZONE LEFT SIDE WERE FOUND TO BE INOPERATIVE. MAINTENANCE FOUND THE ELECTRICAL CONNECTOR BROKEN NEAR SEAT 4B. MAINTENANCE REPAIRED THE WIRE AT 4B EMERGENCY PROXIMITY LIGHT ASSEMBLY. SYSTEM OPERATION TESTED NORMAL AFTER THE WIRE WAS REPAIRED. AIRCRAFT IS GOOD FOR SERVICE.
2010
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 2,680 hrs · 343 cycles
DURING A LINE CHECK, MX FOUND THE DOOR MOUNTED EMERGENCY LIGHTS AT 1L AND 4R INOPERATIVE. MX RELAMPED 4R AND REPLACED THE LIGHT ASSY AT 1L. OPS CHECKS WERE GOOD.
Part: SKIN — CRACKED (LT WING) · airframe 90,124 hrs · 11,291 cycles
DURING LINE CHECK FOUND LT WING L/E SKIN HAS CRACK OTBD OF LANDING LIGHT LENS. REPLACED ILES 330.00 POSITION L/E SURFACE SKIN ( LT OTBD LANDING LIGHT OTBD SIDE ) IAW SRM57-41-01, REP-5, DETAIL-2.
Part: PLATE — DAMAGED (WING) · airframe 90,124 hrs · 11,291 cycles
DURING LINE CHECK FOUND SPLICE PLATE HAS 6 EA OF ELOGATED RIVET HOLES ILES 330.00 POS FWD AND LOWER RIB HAS 1.5 INCH CRACK. REPAIRED ILES 330.00 POS FWD RIB LOWER RIB AND SPLICE PLATE IAW SRM 51-10-02.
Part: WIRE — DAMAGED (CABIN) · airframe 89,837 hrs · 11,253 cycles
DURING A LINE CHECK, MAINTENANCE FOUND THE DOOR 2R EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPAIRED THE LIGHT WIRING. OPERATIONAL CHECK WAS GOOD. (2010-00835)
Part: SOCKET — BROKEN (CABIN) · airframe 89,720 hrs · 11,239 cycles
DURING LAYOVER CHECK MAINTENANCE FOUND AFT GALLEY EMERGENCY LIGHT IN THE CART PARTITION BROKEN. REPLACED SOCKET. (2010-00812)
Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,439 hrs · 11,206 cycles
DURING A LINE CHECK, MX FOUND THE DOOR 2R EMERGENCY SLIDE LIGHT INOPERATIVE. MX REPLACED THE LIGHT ASSY. OPS CHECK WAS GOOD.
Part: LIGHT — BROKEN (CABIN) · airframe 89,439 hrs · 11,206 cycles
DURING A LINE CHECK, MX FOUND THE EMERGENCY PATH LIGHT AT GU3A (MID) BROKEN. MX REPLACED THE LIGHT ASSY. OPS CHECK WAS GOOD.
Part: CONNECTOR — LOOSE (CABIN) · airframe 88,619 hrs · 11,098 cycles
EMERGENCY EGRESS AISLE LIGHTS INOP ROWS 35-41 LEFT. SECURED WIRE CONNECTOR, CHECKS OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,540 hrs · 11,084 cycles
DURING LINE CHECK, MAINTENANCE FOUND THE EMERGENCY PATH LIGHTS AT GALLEY 3A INOPERATIVE. MAINTENANCE REPLACED THE PATH LIGHT MODULE. OPERATIONAL CHECK WAS GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 88,109 hrs · 11,032 cycles
OUTBOUND FLIGHT CREW FOUND THE LT ZONE B EMERGENCY PATH LIGHTS INOPERATIVE. MX REPAIRED THE FLOOR LIGHTS. OPS CHECK WAS GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,516 hrs · 10,956 cycles
DURING LAYOVER CHECK, MX FOUND DOOR 2R EMERGENCY SLIDE LIGHT INOPERATIVE. MX REPLACED THE SLIDE LIGHT ASSY. OPS CHECK WAS GOOD.
Part: SKIN — DELAMINATED (RT WING TE FLAP) · airframe 87,450 hrs · 10,947 cycles
DURING "L" CHECK, FOUND RT WING AFT FLAP LOWER SURFACE WAS DELAMINATED IN 2 LOCATIONS. REPAIRED IAW SRM 51-70-07-5A.
Part: STIFFENER — MISREPAIRED (FUSELAGE) · airframe 87,450 hrs · 10,947 cycles
DURING L-CHECK AND DOOR NR 5 CREW REST SHEAR BEAM MODIFICATION FOUND SHORT EDGE MARGIN ON SHEAR WEB AND STIFFENER. REPAIRED IAW ERA 480413-14AD.
Part: STIFFENER — CRACKED (BS 260-280) · airframe 87,450 hrs · 10,947 cycles
DURING L-CHECK FOUND CRACK IN LT NOSE WHEEL WELL BOX STIFFENER FASTENER HOLE AT BS260 TO BS280, WL170. REPAIRED IAW SRM 51-10-02, 51-40-02.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,331 hrs · 10,933 cycles
DURING LAYOVER CHECK, MAINTENANCE FOUND THE DOOR 2R EMERGENCY LIGHT INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY. OPERATIONAL CHECK WAS GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,943 hrs · 10,886 cycles
DURING LAYOVER CHECK, MX FOUND DR2L EMERGENCY LIGHT INOPERATIVE. MX REPLACED THE LIGHT ASSY. OPS CHECK WAS GOOD.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS) · airframe 86,740 hrs · 10,864 cycles
DURING LINE CHECK FOUND EMERGENCY PATH LIGHTS AT ZONE C SEATS 31C TO 43C LT WOULD NOT ILLUMINATE WHEN TESTED. REPLACED POWER SUPPLY.
2009
Part: WIRE — DAMAGED (EMERGENCY LIGHT) · airframe 85,957 hrs · 10,776 cycles
MAINTENANCE DISCOVERED EMERGENCY ESCAPE PATH LIGHTS 'B' ZONE INOPERATIVE. MAINTENANCE REPAIRED WIRE AT SEAT 10 A/B JUST FORWARD OF LENS. EMERGENCY ESCAPE PATH LIGHTS CHECKED NORMAL.
2008
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 79,087 hrs · 9,923 cycles
DURING OVERNIGHT CHECK, FOUND ZONE B LEFT SIDE EMERGENCY LIGHTS WON'T ILLUMINATE. MAINTENANCE RECONNECTED ELECTRICAL CONNECTORS. OPERATIONAL CHECKED GOOD AND AIRCRAFT WAS RETURNED TO SERVICE.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,221 hrs · 9,813 cycles
DURING LINE CHECK, FOUND LT UPPER DECK EMERGENCY DOOR BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK PER AMM 52-23-14.
2007
Part: BATTERY PACK — INOPERATIVE (EMERGENCY EXIT) · airframe 77,146 hrs · 9,668 cycles
DURING LINE CHECK, FOUND UPPER DECK LT EMERGENCY DOOR PACK INOPERATIVE. REPLACED BATTERY PACK PER AMM 52-23-14.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS) · airframe 77,097 hrs · 9,662 cycles
DURING LINE CHECK, FOUND UPPER DECK LT EMERGENCY DOOR BATTERY PACK INOPERATIVE. REPLACED BATTERY PACK PER AMM 52-23-14.
Part: INTERCOSTAL — CRACKED (BS 340) · airframe 74,899 hrs · 9,354 cycles
DURING "M" CHECK, FOUND CRACKS IN UPPER CROWN INTERCOSTAL AT BS 340 BL 0. REPAIRED PER EA 63-208913.
Part: FRAME — CRACKED (BS 1265 S26L) · airframe 74,899 hrs · 9,354 cycles
DURING "M" CHECK, FOUND CRACK IN FRAME WEB HOLE AT BS 1265 S26L. ACCOMPLISHED INTERIM REPAIR PER EA 63-208916 SECTION I. REPETITIVE INSPECTIONS TO BE ACCOMPLISHED PER SECT II EVERY 2000 CYCLES. SECTION III PERMANENT REPAIR TO BE ACCOMPLISHED BASED ON SECTION II INSPECTION FINDINGS.
Part: SHEAR TIE — CRACKED (BS 1120) · airframe 74,899 hrs · 9,354 cycles
DURING "M" CHECK, FOUND CRACK IN TENSION TIE CHANNEL AT BS 1120 RBL 71. REPAIRED PER EA 63-209225.
Part: INTERCOSTAL — CORRODED (BS 1920-1960) · corrosion level 2 · airframe 74,899 hrs · 9,354 cycles
DURING "M" CHECK, FOUND CORROSION ON BULK CARGO FLOOR PANEL SUPPORT INTERCOSTAL BS 1920-1960 LBL 55. REPAIRED PER EA 63-209224.
Part: FRAME — CRACKED (BS 500 S10R) · airframe 74,899 hrs · 9,354 cycles
DURING "M" CHECK, FOUND CRACK IN FORWARD FASTENER HOLE AT FRAME TO STRINGER CONNECTION BS 500 S10R. REPAIRED PER EA 63-209223.
Part: FRAME — CRACKED (BS 1140) · airframe 74,899 hrs · 9,354 cycles
DURING "M" CHECK, FOUND CRACK ON FRAME WEB AND FRAME DOUBLER TENSION TIE AT BS 1140 RBL 70. REPAIRED PER EA 63-209214.
Part: FRAME — CRACKED (BS 480 S10L) · airframe 74,899 hrs · 9,354 cycles
DURING "M" CHECK, FOUND CRACK IN FRAME TO STRINGER CONNECTION FASTENER HOLE AT BS 480 S10L. REPAIRED PER EA 63-209229.
Part: FRAME — CRACKED (BS 500 S10L) · airframe 74,899 hrs · 9,354 cycles
DURING "M" CHECK, FOUND CRACK IN FRAME FASTENER HOLE AT BS 500 S10L. REPAIRED PER EA 63-209228.
Part: SHEAR TIE — DAMAGED (BS 1160) · airframe 74,899 hrs · 9,354 cycles
DURING "M" CHECK, FOUND TENSION TIE WITH ELONGATED FASTENER HOLE AT BS 1160 LBL 59. REPAIRED PER EA 63-209221.
Part: SHEAR TIE — CRACKED (BS 1160) · airframe 74,899 hrs · 9,354 cycles
DURING "M" CHECK, FOUND CRACK IN FASTENER HOLE OF TENSION TIE FRAME AT BS 1160 RBL 63. REPAIRED PER EA 63-209219.
Part: SHEAR TIE — CRACKED (BS 1180) · airframe 74,899 hrs · 9,354 cycles
DURING "M" CHECK, FOUND CRACK ON UPPER LOBE TENSION TIE FORWARD CHANNEL AT BS 1180 RT. REPAIRED PER EA 63-209217.
Part: SHEAR TIE — CRACKED (1180) · airframe 74,899 hrs · 9,354 cycles
DURING "M" CHECK, FOUND CRACKS ON UPPER LOBE TENSION TIE FRAME WEB FASTENER HOLES AT BS 1180 LT. REPAIRED PER EA 63-209218.
Part: SUPPORT BRACKET — CRACKED (BS 1120 S13R) · airframe 74,899 hrs · 9,354 cycles
DURING "M" CHECK WHILE PERFORMING SB 747-53A-2507 STAGE 2 INSPECTION, FOUND CRACKS IN SUPPORT BRACKET AND WEB FOR SLOPING PANEL AT BS 1120 S13R. REPAIRED PER EA 63-208915.
2006
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 72,082 hrs · 8,982 cycles
FOUND CEILING MOUNTED EMERGENCY LIGHTS IN ZONE A LEFT FORWARD AND ZONE B RIGHT, LIGHTS INOP. MAINTENANCE REPLACED POWER SUPPLY. OPERATIONAL CHECKED GOOD, AND AIRCRAFT RETURNED TO SERVICE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 72,082 hrs · 8,982 cycles
FLOOR MOUNTED EMERGENCY LIGHTS ZONE E LEFT SIDE INOP. MAINTENANCE REPLACED LIGHT ASSEMBLY.
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 71,212 hrs · 8,866 cycles
DURING LINE CHECK, FOUND A/C RIGHT SIDE FORWARD OF DOOR 3, AFT WING FAIRING EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. A/C RETURNED TO SERVICE.
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 71,212 hrs · 8,866 cycles
DURING LINE CHECK, FOUND A/C RIGHT SIDE UNDER DOOR 3, AFT WING FAIRING EMERGENCY LIGHT INOP. REPLACED POWER SUPPLY. OPERATIONAL CHECK GOOD. A/C RETURNED TO SERVICE.
Part: BATTERY — INOPERATIVE (EMERGENCY LIGHT) · airframe 71,038 hrs · 8,843 cycles
DURING LINE CHECK, FOUND 2 AFT EMERGENCY LIGHT ASSEMBLIES INOP ON RIGHT WING TO FUSELAGE FAIRING. REPLACED POWER SUPPLY AND BATTERIES. OPERATIONAL CHECK GOOD. A/C RETURNED TO SERVICE.
2004
Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,758 hrs · 7,790 cycles
DURING LINE CHECK, FOUND ZONE-D LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RESEATED CONNECTOR. OPERATIONAL CHECK GOOD.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT) · airframe 62,255 hrs · 7,728 cycles
DURING LINE CHECK, FOUND THE RIGHT SIDE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21-41. REPLACED BULBS. OPERATIONAL CHECK GOOD.
2003
Part: OVEN — BURNED (G1B GALLEY) · airframe 17,699 hrs · 2,172 cycles
DURING FLIGHT, A STRONG BURNING FUME EMITTED FROM THE G1B GALLEY RIGHT OVEN. AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. REPLACED THE OVEN. OPERATIONAL CHECK GOOD.
Part: CONNECTOR — INOPERATIVE (BATTERY PACK) · airframe 58,853 hrs · 7,318 cycles
DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21-35 HJK AND FROM DOOR 1L TO LAV DOOR 1L. RESEATED CONNECTOR PLUG AT BATTERY PACK AND RESPLICED WIRE. OPERATIONAL CHECK GOOD.
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 58,761 hrs · 7,306 cycles
DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOP FROM ROWS 72-80 IN THE UPPER DECK. REPLACED THE POWER SUPPLY. OPERATIONAL CHECK GOOD. REFERENCE LOG PAGE 2001935.
Part: WIRE — DAMAGED (PATH LIGHTS) · airframe 57,597 hrs · 7,156 cycles
DURING LINE CHECK FOUND UPPER DECK FLOOR PATH EMERGENCY LIGHTS INOP. REPAIRED WIRE AND OPERATIONAL CHECK GOOD.
Part: WIRE — BROKEN (GALLEY) · airframe 57,481 hrs · 7,139 cycles
DURING FLIGHT, FIRE FLASHED AT GALLEY 2C AFT COFFEEMAKER WHEN HOT PLATE WAS PULLED OUT. TURNED POWER OFF AND AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. MAINTENANCE FOUND HOT PLATE WIRE BROKEN, REPLACED HOTPLATE. OPERATIONAL CHECK GOOD.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHT) · airframe 57,283 hrs · 7,113 cycles
DURING LINE CHECK FOUND LEFT (B) ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. RECONNECTED FLOOR EMERGENCY LIGHT CONNECTOR. OPERATIONAL CHECK GOOD.
Part: CONNECTOR — DISCONNECTED (LIGHT) · airframe 56,828 hrs · 7,053 cycles
DURING LINE CHECK FOUND UPPER DECK STAIR AND ZONE C, RT AISLE EMERGENCY LIGHTS INOPERATIVE. RECONNECTED CONNECTOR PLUG TO POWER SUPPLY OVER DOOR 2L. OPERATIONAL CHECK GOOD.
2002
Part: WIRE — DAMAGED (CABIN) · airframe 56,270 hrs · 6,981 cycles
DURING LINE CHECK, FOUND RIGHT (D) ZONE FLOOR EMERGENCY PATH LIGHTS INOPERATIVE. REPAIRED WIRING AND OPERATIONALLY CHECK GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 53,717 hrs · 6,644 cycles
DURING LINE CHECK, FOUND ZONE 'C' LEFT FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPLACED LIGHT AND RECONNECTED WIRES. OPERATIONAL CHECK GOOD.
Part: ODOR — DETECTED (CABIN) · airframe 53,584 hrs · 6,627 cycles
DURING CRUISE, AN INTENSE BURNING SMELL EMITTED IN THE AREA OF DOOR 5L. TURNED OFF RECIRCULATION FANS AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. VISUALLY INSPECTED AREA WITH NO DEFECTS NOTED.
Part: ODOR — DETECTED (CABIN) · airframe 53,584 hrs · 6,627 cycles
DURING CRUISE, AN INTENSE BURNING SMELL EMITTED IN THE AREA OF DOOR 5L. TURNED OFF RECIRCULATION FANS AND THE AIRCRAFT CONTINUED TO DESTINATION AND LANDED WITHOUT INCIDENT. VISUALLY INSPECTED AREA WITH NO DEFECTS NOTED.
Part: SOCKET — DAMAGED (CABIN) · airframe 52,458 hrs · 6,496 cycles
DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS ON THE RIGHT SIDE OF ZONE 'D' INOPERATIVE. REPAIRED SOCKET ASSEMBLY. OPERATIONAL CHECK GOOD.
2001
Part: LIGHT — INOPERATIVE (CABIN) · airframe 51,292 hrs · 6,363 cycles
DURING LINE CHECK, FOUND ZONE-D RIGHT SIDE AND ZONE-B LEFT SIDE EMERGENCY FLOOR PATH LIGHTS INOPERATIVE. REPAIRED FLOOR PATH LIGHTING. OPERATIONAL CHECK OK.
Part: WIRE — DISCONNECTED (CABIN) · airframe 50,429 hrs · 6,261 cycles
DURING LINE CHECK, FOUND EMERGENCY ESCAPE PATH LIGHTING INOPERATIVE AT PASSENGER DOOR 1L. RECONNECTED WIRING, OPERATIONAL CHECK NORMAL.
Part: HYDRAULIC LINE — RUPTURED (CASE DRAIN MOD) · airframe 50,075 hrs · 6,219 cycles
DURING CLIMB, THE AIRCRAFT LOST THE NBR 4 HYDRAULIC SYSTEM FLUID QUANTITY AND PRESSURE. CREW DECLARED AN EMERGENCY AND RETURNED TO MNL AND LANDED WITHOUT INCIDENT. REPLACED THE HYDRAULIC RETURN LINE BETWEEN THE CASE DRAIN MODULE AND HEAT EXCHANGER, CASE DRAIN MODULE, ENGINE DRIVEN HYDRAULIC PUMP, AND AIR DRIVEN HYDRAULIC PUMP. OPERATIONAL CHECK GOOD.
Part: HYDRAULIC LINE — RUPTURED (CASE DRAIN MOD) · airframe 50,075 hrs · 6,219 cycles
DURING CLIMB, THE AIRCRAFT LOST THE NBR 4 HYDRAULIC SYSTEM FLUID QUANTITY AND PRESSURE. CREW DECLARED AN EMERGENCY AND RETURNED TO MNL AND LANDED WITHOUT INCIDENT. REPLACED THE HYDRAULIC RETURN LINE BETWEEN THE CASE DRAIN MODULE AND HEAT EXCHANGER, CASE DRAIN MODULE, ENGINE DRIVEN HYDRAULIC PUMP, AND AIR DRIVEN HYDRAULIC PUMP. OPERATIONAL CHECK GOOD.
airframe 50,033 hrs · 6,214 cycles
DURING FLIGHT, RECEIVED "HYD PRES ENG 4" AND "HYD QTY LOW" MESSAGES. THE HYDRAULIC FLUID QUANTITY IN THE NBR 4 SYSTEM INDICATED ZERO. TURNED OFF THE HYDRAULIC PUMPS FOR THE NBR 4 SYSTEM AND THE CREW DECLARED AN EMERGENCY. ALTERNATE EXTENDED THE LANDING GEAR AND THE AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED THE ENGINE DRIVEN HYDRAULIC PUMP. OPERATIONAL CHECK GOOD.
Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 49,867 hrs · 6,191 cycles
In H check, found corrosion on seat track. Repaired per EA63-184052.
Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · corrosion level 2 · airframe 49,867 hrs · 6,191 cycles
IN H CHECK, FOUND CORROSION ON FLOOR SUPPORT. REPAIRED PER EA63-183406.
Part: SEAT TRACK — CORRODED · corrosion level 2 · airframe 49,867 hrs · 6,191 cycles
In H check, found corrosion on seat track. Repaired per EA63-182725.
1999
Part: CONNECTOR — BROKEN (ROW 27)
DURING LINE CHECK, FOUND C ZONE FLOOR PATH EMERGENCY LIGHT INOPERATIVE. REPAIRED LIGHT ASSEMBLY CONNECTOR AT ROW 27, OPERATIONAL CHECK GOOD.
1998
Part: WIRE — BROKEN (CABIN)
DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 35 TO 39 AND AT DOOR 3L. REPAIRED WIRES, OPERATIONAL CHECK GOOD.
Part: CONNECTOR — LOOSE (CABIN)
DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 51HJK TO 66HJK. RECONNECTED ELECTRICAL PIN, OPERATIONAL CHECK GOOD.
1997
Part: PUMP — FAILED (NR 1 ENGINE)
DURING CRUISE, THE NR 1 ENGINE DRIVEN HYDRAULIC PUMP AND THE AIR DRIVEN HYDRAULIC PUMP FAILED. AIRCRAFT DIVERTED TO ANC AND LANDED WITHOUT INCIDENT. REPLACED THE NR 1 ENGINE DRIVEN AND AIR DRIVEN HYDRAULIC PUMPS. OPERATIONAL CHECK GOOD.
Part: CONNECTOR — LOOSE (CABIN)
DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 35BC TO 39ABC. RECONNECTED CONNECTOR PIN, OPERATIONAL CHECK GOOD.
Part: CONNECTOR — LOOSE (CABIN)
DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 35BC - 45ABC. RECONNECTED CONNECTOR PIN. OPERATIONAL CHECK GOOD.
Part: WIRE — LOOSE (CABIN)
DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE AT 9J AND FROM 35C TO 40C. REPLACED LIGHT AT 9J AND RECONNECTED WIRES AT 35C, OPERATIONAL CHECK GOOD.
Part: WIRE — LOOSE (CABIN)
DURING LINE CHECK, FOUND THE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 21ABC - 24ABC. RECONNECTED WIRE. OPERATIONAL CHECK OK.
Part: OXY PRESS LIGHT — ILLUMINATED (COCKPIT)
DURING CRUISE, THE CREW OXYGEN PRESSURE LIGHT ILLUMINATED. AIRCRAFT DIVERTED TO ANC AND LANDED WITHOUT INCIDENT. FOUND OXYGEN BOTTLE PRESSURE TO BE NORMAL BUT REPLACED THE OXYGEN CYLINDER AS A PRECAUTION.
Part: CONNECTOR — LOOSE (CABIN)
DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE FROM ROWS 35 BC TO 39 ABC. RECONNECTED CONNECTOR PIN, OPERATIONAL CHECK GOOD.
Part: CONNECTOR — FAILED (CABIN)
DURING LINE CHECK, FOUND D-ZONE FLOOR PATH EMERGENCY LIGHTS INOPERATIVE. REPAIRED ELECTRICAL CONNECTOR, OPERATIONAL CHECK GOOD.
Part: WIRE — LOOSE (CABIN)
DURING LINE CHECK, FOUND FLOOR PATH EMERGENCY LIGHTS INOPERATIVE AT DOOR 2L FROM DOORS 3L-4L AND AT ROW 9K. RECONNECTED WIRES AND REPLACED LIGHT ASSEMBLY AT DOOR 2L. OPERATIONAL CHECK GOOD.
Part: CONNECTORS — LOOSE (CABIN)
DURING LINE CHECK, FOUND NINE EMERGENCY PATH LIGHTS INOPERATIVE FROM ROWS 21 TO 30. REPLACED BULBS AND RECONNECTED EMERGENCY LIGHTS CONNECTORS, OPERATIONAL CHECK GOOD.
1995
Part: EEL WIRE — LOOSE (CABIN)
TPE - DURING LINE CHECK, THE EMERGENCY PATH FLOOR LIGHTS BETWEEN SEAT ROWS 35L TO 42L WERE FOUND INOPERATIVE. RECONNECTED LOOSE WIRE PIN AT SEAT 42, OPERATIONAL CHECK OK.
Part: RESERVOIR — LOW PRESSURE (R1 DOOR)
DURING LINE CHECK (SEL), THE DOOR R1 EMERGENCY POWER RESERVOIR PRESSURE WAS FOUND BELOW LIMITS. REPLACED THE EMERGENCY POWER RESERVOIR. INSPECTED AND CHECKED OK.
Part: VIDEO CONSOLE — FAILED (CABIN)
DURING FLIGHT, A PASSENGER SPILLED A LARGE AMOUNT OF WATER ON THE ARMREST OF SEAT 10JK. THEN, DURING THE DEPLANING OF PASSENGERS, THE ARMREST STARTED EMITTING A SMALL AMOUNT OF WHITE SMOKE. FLIGHT ATTENDANT USED HALON FIRE EXTINGUISHER ON ARMREST AND SMOKING CEASED. MAINTENANCE REPLACED VIDEO CONSOLE, THE SEAT ELECTRICAL BOX AND THE UNDERSEAT ELECTRICAL BOX. OPERATIONAL CHECK OK.
Part: FLOORBEAM — CORRODED (FS 1720)
DURING PERIODIC CHECK, FOUND CORROSION ON THE UPPER FLOORBEAM CHORD FS 1720, LBL 76 TO 99. REPAIRED PER EA 63-98269.
Part: BEAM — CORRODED (FS 1630-1670)
DURING PERIODIC CHECK, FOUND CORROSION ON FLOOR SUPPORT BEAM FS 1630 TO 1670 AT LBL 42. REPAIRED PER EA 63-98066.