N39356
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.
114 reports on file, 1995-04-17 – 2016-06-24.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 114,713 hrs · 18,659 cycles
AIRCRAFT WAS NOT GROUNDED. SEAT MOUNTED EMERGENCY LIGHT AT SEAT 37H IS INOPERATIVE. R & R SEAT LIGHT ASSY IAW AMM 33-60-98. OPS CHECK NORMAL.
Part: WIRE — BROKEN (ZONE 400) · airframe 114,692 hrs · 18,655 cycles
AIRCRAFT WAS GROUNDED. AIR INTERRUPT, EMERGENCY DECLARED, LANDING UNEVENTFUL. ACFT OVERWEIGHT. DURING CLIMB, RECEIVED NR 2 ENGINE PRV EICAS MESSAGE. ALSO, RECEIVED NR 1 ENGINE HPSOV EICAS MESSAGE ACCOMPANIED BY BLEED LIGHT. MAINTENANCE REPAIRED A BROKEN WIRE TERMINAL ON THE NR 2 ENGINE PRV TERMINAL BLOCK IAW SWPM 20-30-11 AND AMM 36-11-18. NR 1 ENGINE HPSOV DEFERRED. ALSO, AALA20160624006.
Part: WIRE — BROKEN (NR 2 ENGINE) · airframe 114,692 hrs · 18,655 cycles
DURING CLIMB, RECEIVED NR 2 ENGINE PRV EICAS MESSAGE ALSO RECEIVED NR 1 ENGINE HPSOV EICAS MESSAGE ACCOMPANIED BY BLEED LIGHT. MAINTENANCE REPAIRED A BROKEN WIRE TERMINAL ON THE NR 2 ENGINE PRV TERMINAL BLOCK IAW SWPM 20-30-11 AND AMM 36-11-18. EMERGENCY DECLARED, LANDING UNEVENTFUL. AIRCRAFT WAS GROUNDED. ACCOMPLISHED PNEUMATIC SYSTEM HEALTH CHECK ON LEFT ENGINE IAW AMM 36-11-21. OPS CHECKED GOOD.
Earlier reports · 1995–2015 · 111 reports
2015
Part: PROXIMITY SENSOR — FAULTY (RT MLG DOOR) · airframe 111,373 hrs · 17,976 cycles
DURING APPROACH RECEIVED LANDING GEAR MONITOR MSG & LG DOOR LIGHT ILLUMINATED. EMERGENCY DECLARED & LANDING UNEVENTFUL. R & R RT MLG DOOR PROXIMITY SENSOR S264 IAW AMM 32-61-02. ACCOMPLISHED MAIN GEAR EXTENSION & RETRACTION SYS TEST IAW AMM 32-32-00-501 & MCM 32-95-31. SYS CHECKED NORMAL.
Part: CONNECTOR — FAULTY (MLG DOOR) · airframe 111,373 hrs · 17,976 cycles
EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. CREW REPORTS DURING APPROACH RECEIVED LG MONITOR MESSAGE & MLG DOOR LIGHT ILLUMINATED. ACCOMPLISHED MEASUREMENT & ADJUSTMENT IAW AMM 32-61-02. PERFORMED PSEU BITE NEAR & FAR TARGETS. FOUND CONNECTOR D1942P PIN 2 INOPERATIVE. R & R CONNECTOR IAW WDM 32-61-12. ACCOMPLISHED MAIN GEAR EXTENSION & RETRACTION SYS TEST IAW AMM 32-32-00-501 & MCM 32-95-31. SYS CHECKED NORMAL.
Part: PROXIMITY SENSOR — FAULTY (RT MLG) · airframe 111,373 hrs · 17,976 cycles
EMERGENCY DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH RECEIVED LG MONITOR MSG & LG DOOR LIGHT ILLUMINATED. R & R RT MLG DOOR PROXIMITY SENSOR S242 IAW AMM 32-61-02. ACCOMPLISHED MAIN GEAR EXTENSION & RETRACTION SYS TEST IAW AMM 32-32-00-501 & MCM 32-95-31. SYS CHECKED NORMAL. SEE ALSO AALA20150417006 & AALAAALA20150420005.
Part: DOOR SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 111,184 hrs · 17,945 cycles
FORWARD CARGO DOOR LOWER SILL LOWER CHORD LOWER FLANGE IS CORRODED AT FS 590 & RBL 44.4. REMOVED CORROSION, INSPECTED AREA & RESTORED FINISH IAW EA B767-53-039089 DATED 3 20 2015.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 111,184 hrs · 17,945 cycles
CORROSION FOUND COMMON TO THE FUSELAGE SKIN & STRINGER AT STATION 500 & STRINGER 39 RT. REPAIRED STRINGER IAW SRM 53-00-03-2R REPAIR 2 & EA B767-53-039088.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 111,184 hrs · 17,945 cycles
CORROSION FOUND COMMON TO THE FUSELAGE SKIN & STRINGER AT STATION 500 & 39 RT. REPAIRED SKIN IAW SRM 53-00-01-2R REPAIR 29 & EA 53-039088.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 111,184 hrs · 17,945 cycles
CORROSION BETWEEN FUSELAGE SKIN & STRINGER 39 RT AT STATION 654+70. ACCOMPLISHED SKIN REPAIR IAW SRM 53-00-01.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 111,184 hrs · 17,945 cycles
CORROSION BETWEEN FUSELAGE SKIN & STRINGER 39 RT AT STATION 654+70. ACCOMPLISHED STRINGER SPLICE REPAIR IAW SRM 53-00-03.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 111,184 hrs · 17,945 cycles
EMERGENCY LIGHT INOPERATIVE ON EXTERIOR JUST FWD OF AFT RT CARGO DOOR L644. REPLACED EXTERIOR EMER LIGHT FWD OF AFT RT CARGO DOOR. SYS CHECKED NORMAL.
2014
Part: PRESSURE SWITCH — INOPERATIVE (LT ENG FUEL) · airframe 110,659 hrs · 17,835 cycles
LEFT ENGINE FUEL FILTER BYPASS LIGHT ILLUMINATED. RETURNED TO DEPARTURE, EMERGENCY DECLARED AND LANDED UNEVENTFULLY. REPLACED THE PRESSURE SWITCH.
Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 109,981 hrs · 17,717 cycles
LEFT ENG FUEL FILTER CLOG LIGHT ILLUMINATED. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED LT FUEL FILTER DIFFERENTIAL PRESS SWITCH. SYS GND CHECKED NORMAL, OPERATION CLOSED.
Part: BYPASS SWITCH — INOPERATIVE (FUEL SYSTEM) · airframe 109,982 hrs · 17,718 cycles
DURING CLIMB THE LT ENG FUEL FILTER BYPASS INDICATION CAME ON. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. R & R LT ENG FUEL FILTER & FUEL FILTER BYPASS SWITCH. SYS GND CHECKED NORMAL OPERATION CLOSED.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 109,055 hrs · 17,583 cycles
SEAT MOUNTED EMER LIGHTS FROM 32H TO 41H INOPERATIVE. REPLACED BATTERY & CHARGER. OPERATIONS CHECKED NORMAL.
Part: LENS — MISSING (CABIN) · airframe 109,055 hrs · 17,583 cycles
SEAT 21H EMER LIGHT MISSING LENS. REPLACED LENS. OPERATIONS CHECKED NORMAL.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 108,427 hrs · 17,479 cycles
CORROSION ON FUSELAGE SKIN AT STATION 1197. INSTALLED EXTERNAL DOUBLER REPAIR IAW SRM 53-00-01-2 REPAIR 12 DETAIL III.
Part: PIN — BACKED OUT (CABIN) · airframe 108,215 hrs · 17,443 cycles
SEAT 4HJ ESCAPE PATH LIGHT INOPERATIVE. FOUND PIN PUSH BACKED AT SEAT 4HJ ESCAPE PATH LIGHT CONNECTOR, REINSERTED PIN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,114 hrs · 17,424 cycles
RIGHT NR 1 DOORWAY EMERGENCY LIGHT, L288, INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOORWAY EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,114 hrs · 17,424 cycles
EMERGENCY LIGHT AT SEAT 31H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 31H, OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 108,114 hrs · 17,424 cycles
LEFT NR 4 DOORWAY EMERGENCY LIGHT, L334, INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOORWAY EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.
Part: WIRE HARNESS — NOT SEATED (CABIN) · airframe 108,114 hrs · 17,424 cycles
EMERGENCY LIGHT AT SEAT 27B INOPERATIVE. RESEATED HARNESS FOR EMERGENCY LIGHT ASSEMBLY AT SEAT 27B, OPERATIONS CHECKED NORMAL.
Part: LATCH — OUT OF ADJUST (EXIT SIGN) · airframe 108,114 hrs · 17,424 cycles
RIGHT NR 4 INTERIOR EMERGENCY EXIT SIGN ABOVE DOOR HANDLE, TOP FWD LATCH DOES NOT LOCK. ADJUSTED LATCH ON LENS ASSEMBLY, OPERATIONS CHECKED NORMAL.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 107,692 hrs · 17,355 cycles
RIGHT LOWER FUSELAGE EMERGENCY LIGHTS INOPERATIVE. REPLACED M00733 BATTERY CHARGER. OPERATIONS CHECKED NORMAL.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 107,692 hrs · 17,355 cycles
RIGHT LOWER FUSELAGE EMERGENCY LIGHTS INOPERATIVE. REPLACED M00733 BATTERY CHARGER. OPERATIONS CHECKED NORMAL.
Part: CONNECTOR — NOT SEATED (CABIN) · airframe 107,236 hrs · 17,287 cycles
ROW 4H EMERGENCY SIDEWALL LIGHT INOPERATIVE. RESEATED THE CONNECTOR FOR ROW 4H EMERGENCY SIDEWALL LIGHT. OPERATIONS CHECKED NORMAL.
2013
Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 106,246 hrs · 17,138 cycles
CORROSION AT STATION 785 & BL 0. ACCOMPLISHED CORROSION REMOVAL & REPAIR IAW EA B767-53-031979.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,228 hrs · 17,135 cycles
CEILING LIGHT ABOVE ROW 5AB INOPERATIVE. REPLACED LAMP FOR CEILING EMERGENCY LIGHT ABOVE 5AB. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 106,088 hrs · 17,109 cycles
CABIN EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR CABIN EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 103,494 hrs · 16,707 cycles
RIGHT NUMBER 1 DOOR EMERGENCY EXIT SIGN THRESHOLD LIGHTS ARE INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EMERGENCY EXIT SIGN THRESHOLD LIGHTS. OPS CHECK NORMAL.
Part: FRAME — CRACKED (FUSELAGE) · airframe 103,494 hrs · 16,707 cycles
STATIONS 883.5 RIGHT TO 905.5 LEFT, OVERWING FRAME CRACKED. INSTALLED REPAIR ANGLE PER EA B767-53-028138.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 102,623 hrs · 16,569 cycles
RIGHT OVERWING AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT OVERWING AFT EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 101,058 hrs · 16,335 cycles
EMERGENCY LIGHT AT SEAT 24G INOPERATIVE. REPLACED LAMP FOR SEAT 24G EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: FLAP — DENTED (LT WING) · airframe 100,042 hrs · 16,173 cycles
DENT IN LEFT OUTBOARD FLAP UNDERSIDE TRAILING EDGE. ACCOMPLISHED HOT BOND REPAIR PER SRM 57-53-01.
Part: SKIN — DEBONDED (LE SLAT) · airframe 100,042 hrs · 16,173 cycles
SMALL DISBOND ON NUMBER 2 SLAT OUTBOARD UPPER CORNER UPPER AND LOWER SURFACES. INSTALLED FILLER AND DOUBLER PER SRM 51-70-10-2R.
Part: SLAT — DELAMINATED (RT WING) · airframe 100,042 hrs · 16,173 cycles
NUMBER 8 SLAT HAS DELAMINATION OUTBOARD AFT CORNER. INSTALLED FILLER AND DOUBLER PER SRM 51-70-10-2R.
Part: SKIN — DEBONDED (LE SLAT) · airframe 100,042 hrs · 16,173 cycles
RIGHT WING LEADING EDGE SLAT NUMBER 9 INBOARD END TRAILING EDGE WEDGE ON LOWER SURFACE SHOWS DISBOND INDICATION. INSTALLED FILLER AND DOUBLER PER SRM 51-70-10-2R.
Part: SLAT — DEBONDED (RT WING) · airframe 100,042 hrs · 16,173 cycles
DISBOND ON INBOARD AFT CORNER NUMBER 5 SLAT. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10.
Part: STIFFENER — CRACKED (RT PYLON) · airframe 100,042 hrs · 16,173 cycles
RIGHT PYLON HORIZONTAL STIFFENER CRACKED JUST OUTBOARD OF FRAME CHORD AT STATION 285. REPLACED STIFFENER PER SRM 51-40-02.
Part: WIRE — DAMAGED (CABIN) · airframe 100,042 hrs · 16,173 cycles
ESCAPE PATH LIGHTS AT SEAT 34HJ WAS NOT ILLUMINATED. REPLACED WIRING LOCATED UNDER MUX BOX COVER AT 34HJ FOR ESCAPE PATH LIGHTING. OPS CHECK NORMAL.
Part: WIRE — BROKEN (CABIN) · airframe 99,464 hrs · 16,077 cycles
SEAT 35AB EMERGENCY LIGHT INOPERATIVE. REPAIRED BROKEN WIRE ON HARNESS ASSEMBLY FOR SEAT 35AB EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,464 hrs · 16,077 cycles
AFT RIGHT NUMBER 2 ENTRY DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 ENTRY DOOR EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 99,464 hrs · 16,077 cycles
SEAT 38AB EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 38AB. OPS CHECK NORMAL.
2011
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 97,050 hrs · 15,701 cycles
LEFT NUMBER 4 DOOR EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK M1210 AT AFT EXIT SIGN LEFT NUMBER 4 DOOR. OPS CHECK NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 97,050 hrs · 15,701 cycles
LEFT SIDE MOUNTED EMERGENCY LIGHT ON SEATS 23AB TO 28 AB VERY DIM. REPLACED BATTERY PACK AT M00735. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 97,050 hrs · 15,701 cycles
LEFT NUMBER 1 DOOR EMERGENCY LIGHT SIGN INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR EMERGENCY EXIT SIGN. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 96,525 hrs · 15,621 cycles
EMERGENCY LIGHT AFT OF CARGO DOOR LEFT SIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AFT OF CARGO DOOR LEFT SIDE. OPS CHECK NORMAL.
Part: WEDGE — DAMAGED (TE FLAP) · airframe 96,373 hrs · 15,595 cycles
FOUND DAMAGE ON TRAILING EDGE WEDGE. PREVIOUSLY MARKED. REMOVED DAMAGED CORE AND INSTALLED NEW CORE WITH AN EXTERNAL DOUBLER PER SRM 51-70-10 2R.
2010
Part: START VALVE — MALFUNCTIONED (LT ENGINE) · airframe 95,612 hrs · 15,459 cycles
MIA - CREW REPORTED AFTER ONE HOUR OF FLIGHT LEFT ENGINE START VALVE LIGHT ILLUMINATED WITH A "L ENG STARTER CUT OUT " EICAS MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE START VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: BEAM — DAMAGED (SPOILER) · airframe 95,150 hrs · 15,371 cycles
MAINTENANCE INADVERTENTLY DAMAGED THE LEFT WING SPOILER BEAM AND HINGE ASSEMBLY COMMON TO NUMBER 6 SPOILER ACTUATOR INTERFACE. CUT DAMAGE OFF AND PERFORMED HIGH FREQUENCY EDDY CURRENT. INSTALLED DOUBLER REPAIR PER EA B767-57-013537.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 95,150 hrs · 15,371 cycles
FOUND EXTENSIVE DAMAGE TO STATION 500 FUSELAGE CIRCUMFERENTIAL FRAME INNER CHORD BETWEEN STRINGER 28 TO 31 LEFT DUE IMPACT DAMAGE FROM CARGO PALLETS. PERFORMED HIGH FREQUENCY EDDY CURRENT SURFACE SCAN TRIMMED EDGES OF REMAINING CHORD, REMOVED ALL NICKS, SCRATCHES, GOUGES, BURRS AND SHARP EDGES. ACCOMPLISHED SPLICE REPAIR PER EA B767-53-013524.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 3 · airframe 95,149 hrs · 15,370 cycles
SURFACE CORROSION FOUND AT FORWARD CARGO DOOR LOWER SILL OUTER CHORD. REMOVED CORROSION AND INSTALLED TWO SEPARATE FREEZE PLUGS ON THE WEB AND OUTER CHORD PER EA B767-53-013356
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 3 · airframe 95,150 hrs · 15,372 cycles
SLIGHT BULGE TO EXTERIOR FUSELAGE SKIN JUST AFT OF STATION 654 AND CENTERED AT STRINGER 34 LEFT. AFTER INTERNAL ACCESS WAS GAINED THE SKIN INNER SURFACE WAS FOUND CORRODED UNDERNEATH 3 INCHES OF STRINGER 34 LEFT AFT OF STATION 654. TRIMMED NO MORE THAN 3 INCHES OF THE STRINGER 34 LEFT AFT OF STATION 654 TO FACILITATE SKIN REPAIR WITHIN THIS AREA. FABRICATED AND INSTALLED STRINGER SLICES, TREATED ALL PARTS AS REQUIRED. REFERENCE EA B767-53-013548.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 95,150 hrs · 15,372 cycles
DAMAGE WAS FOUND TO FUSELAGE SKIN AFT OF AFT CARGO DOOR STATION 1373 BETWEEN STRINGER 27 RIGHT AND STRINGER 28 RIGHT. DAMAGE CONSISTED OF DEEP DENT IN FUSELAGE SKIN WHICH ALSO DAMAGED THE UNDERLYING INTERCOSTAL. TRIMMED DAMAGE AND PERFORMED SURFACE HIGH FREQUENCY EDDY CURRENT INSPECTION. FABRICATED REPAIR PARTS AND TREATED ALL ASSEMBLIES. REFERENCE EA B767-53-013335.
Part: SPAR — CRACKED (LT PYLON) · airframe 95,150 hrs · 15,372 cycles
CRACK WAS FOUND ON LEFT PYLON FORWARD UPPPER SPAR WEB COMMON TO THE INTEGRATED DRIVE GENERATOR POWER FEEDER CABLES PASS THROUGH, THIS AREA IS PRONE TO CRACKING. EXTENDED THE UPPER WEB TRIM LINE, FABRICATED FILLERS, DOUBLERS AND HEAT TREATED ALSO TREATED ALL ASSEMBLY PARTS. REFERENCE EA B767-54-013543.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 95,148 hrs · 15,369 cycles
EMERGENCY LIGHTS FAILED TO ACTIVATE ON LEFT NUMBER 2 DOOR EMERGENCY SLIDE. REPLACED BATTERY PACK. OPS CHECK NORMAL.
2009
Part: SHROUD — DAMAGED (CABIN) · airframe 92,175 hrs · 14,866 cycles
EMERGENCY PATH SHROUD AT SEAT 39B DAMAGED. REPLACED SHROUD AT SEAT 39B.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 91,733 hrs · 14,783 cycles
FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED BATTERY.
Part: TAB — BROKEN (FLASHLIGHT) · airframe 91,733 hrs · 14,783 cycles
EMERGENCY FLASHLIGHT AT RIGHT SIDE BUSINESS CLASS FLIGHT ATTENDANT STATION HAS TAMPER TAB BROKEN. REPLACED TAMPER TAB.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,733 hrs · 14,783 cycles
EMERGENCY LIGHT AT SEAT 2B INOPERATIVE. REPLACED LAMP AT SEAT 2B.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,733 hrs · 14,783 cycles
EMERGENCY LIGHT AT SEAT 22H INOPERATIVE. REPLACED LAMP AT SEAT 22H.
Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 91,238 hrs · 14,702 cycles
EMERGENCY EGRESS LIGHT AT SEAT 25B INOPERATIVE. REPLACED HARNESS AT SEAT 25B. OPS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,982 hrs · 14,665 cycles
RIGHT AISLE ROW 28H CEILING EMERGENCY LIGHT INOPERATIVE. RELAMPED LIGHT AT SEAT 28H. OPS CHECK OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,982 hrs · 14,665 cycles
EMERGENCY EGRESS LIGHT AT SEAT 34B INOPERATIVE. RELAMPED LIGHT AT SEAT 34B. OPS CHECK OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,982 hrs · 14,665 cycles
EMERGENCY EGRESS LIGHT AT SEAT 40H INOPERATIVE. RELAMPED LIGHT AT SEAT 40H. OPS CHECK OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,982 hrs · 14,665 cycles
EMERGENCY EGRESS LIGHT AT SEAT 11B INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 11B. OPS CHECK OK.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 90,982 hrs · 14,665 cycles
EMERGENCY EGRESS LIGHT AT SEAT 24B INOPERATIVE. RELAMPED LIGHT AT SEAT 24B. OPS CHECK OK.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 90,842 hrs · 14,638 cycles
FOUND SKIN CORRODED UNDER STRINGER 33 LEFT FROM STATION 434 TO 460. INSTALLED SKIN DOUBLER AT STATION 450 UNDER SRM 53-00-01.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 3 · airframe 90,842 hrs · 14,638 cycles
CORROSION AT STATION 510 STRINGER. REPAIRED STRINGER UNDER SRM 53-00-01.
Part: LIGHT — INOPERATIVE (EXTERIOR)
MIA RIGHT AFT EXTERIOR EXIT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT AFT EXTERIOR EXIT EMERGENCY LIGHT.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,280 hrs
MIA RIGHT HAND AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT HAND AFT.
2008
Part: WIRE — BROKEN (CABIN) · 86,549 cycles
DFW EMERGENCY LIGHT AT SEAT 6B INOPERATIVE. REPAIRED BROKEN WIRE TO LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT SEAT 6B. SYSTEM GROUND CHECKED NORMAL OPS.
Part: LIGHT — MISSING (FUSELAGE) · airframe 86,361 hrs
ORD EMERGENCY LIGHT SIGN AT LT NR 1 DOOR MISSING LIGHT. REPLACED SIGN LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT NR 1 DOOR. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 86,361 hrs
ORD EMERGENCY LIGHT AT SEAT 10B OVERHEAD INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT SEAT 10B OVERHEAD. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)
Part: WIRE — SEVERED (EMERGENCY LIGHT) · airframe 86,361 hrs
ORD EMERGENCY LIGHT AT SEAT 4B FORWARD INOPERATIVE. FOUND SEVERED WIRES. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT SEAT 4B FORWARD. SYSTEM GROUND CHECKED NORMAL OPS. (CLOSED)
Part: LENS — MISSING (CABIN)
DFW - EMERGENCY LIGHT AT LT NR FOUR DOOR AT LAVATORY AREA MISSING LENS. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT LT NR FOUR DOOR AT LAVATORY AREA. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: PIN — LOOSE (CABIN)
DFW - EMERGENCY LIGHTS AT SEAT ROW 4AB DIM. SECURED LOOSE PIN FOR EMERGENCY LIGHTS AT SEAT ROW 4AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 84,412 hrs
JFK - EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EXTERIOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: LIGHT — DIRTY (CABIN)
MIA EMERGENCY LIGHT AT OVERHEAD SEAT 31J INOPERATIVE. CLEANED LIGHT ASSEMBLY FOR EMERGENCY LIGHT AT OVERHEAD SEAT 31J. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT AT OVERHEAD AISLE AT SEAT 17F INOPERATIVE. RELAMPED EMERGENCY LIGHT AT OVERHEAD AISLE AT SEAT 17F. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR OUTSIDE INOPERATIVE. RELAMPED OUTSIDE EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHTS)
SFO - FOUND EMERGENCY SEAT MOUNTED LIGHTS AT SEATS 4AB INOPERATIVE. RELAMPED EMERGENCY SEAT MOUNTED LIGHTS AT SEATS 4AB. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: WIRE — DISCONNECTED (CONNECTOR)
DFW - EMERGENCY LIGHT AT SEAT 38H INOPERATIVE. RECONNECTED WIRING AT LOWER CONNECTION ON SEAT 38H. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SEAL — LEAKING (FUEL CAP)
ORD - INFLIGHT FUEL SPRAY REPORTED COMING FROM LEFT OVERWING CAP. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED LEFT WING O-RING SEAL IN OVERWING FUEL CAP. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SEAL — LEAKING (ZONE 500)
ORD - INFLIGHT FUEL SPRAY REPORTED COMING FROM LEFT OVERWING CAP. RETURNED TO ORD AND LANDED WITHOUT INCIDENT. REPLACED LEFT WING O-RING SEAL IN OVERWING FUEL CAP. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: CONNECTOR — BROKEN (EMERGENCY LIGHT)
DFW - EMERGENCY ESCAPE LIGHTING CONNECTOR BROKEN AT SEAT 35AB. REPLACED EMERGENCY ESCAPE PATH LIGHTING CONNECTOR AT SEAT 25AB. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
LAX - EMERGENCY LIGHT AT SEAT 29H INOPERATIVE. SECURED EMERGENCY LIGHT SIDEWALL CONNECTOR AT SEAT 29H AND J. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHT)
DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT LIGHT AT SEAT 32H INOPERATIVE. RECONNECTED SEAT MOUNTED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 40C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, FIRST CLASS EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT IN FIRST CLASS GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (COCKPIT)
LEFT EGT INDICATOR EICAS AND STANDBY INDICATOR SLOWLY DROPPED TO 0 6:30 HRS INTO FLIGHT BEGAN WORKING AGAIN 8:00 HRS INTO FLIGHT. CHECKED AND FOUND CP LOOSE. RUN UP NO ANOMALIES NOTED. SYSTEM OK TO CONTINUE. (M)
2002
Part: BATTERY PACK — DISCHARGED (CABIN)
DURING OVERNIGHT MAINTENANCE EMERGENCY ESCAPE PATH LIGHTS AT 2H, 3H, 7H, AND 8H INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTS BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (K)
2001
Part: BATTERY PACK — INOPERATIVE (TAIL CONE)
ORD - DURING OVERNIGHT MAINTENANCE, TAILCONE ACCESS WALKWAY EMEREGNCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, CREW EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: SLIDE — CRACKED (LT OVERWING)
SFO - DURING OVERNIGHT MAINTENANCE, LEFT OVERWING SLIDE GIRT BAR LOOSE FROM ATTACH CLAMPS. REPLACED SLIDE ASSEMBLY. SYSTEM, GROUND CHECKED NORMAL OPERATION. (M)
Part: OVEN — MALFUNCTIONED (GALLEY)
LHR - FLT 100 - FIRST CLASS GALLEY NR 1 SMOKES WHEN HEATED TO 375 DEGREES. REPLACED FIRST CLASS GALLEY OVEN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1999
Part: WIRE — SHORTED (CABIN)
LAX - DURING OVERNIGHT CHECK, EMERGENCY EXIT SEAT LIGHTS AT 32AB THROUGH 41AB INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT LIGHT WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — DEFECTIVE (L2 DOOR)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT L2 DOOR INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT L2 DOOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: LIGHT — DEFECTIVE (ROW 41B)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT 41B INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT ASSEMBLY AT SEAT 41B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: OVEN — DIRTY (GALLEY)
LHR - FLT 0136 - EN ROUTE LAX/LHR, SMOKE EMITTING FROM FIRST CLASS GALLEY OVENS. LANDED LHR WITHOUT INCIDENT. CLEANED BOTH FIRST CLASS OVENS. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: WIRE — LOOSE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY OVERHEAD LIGHT AT COCKPIT DOOR DOSE NOT WORK WITH SWITCH. SECURED LOOSE GROUND WIRE ON EMERGENCY OVERHEAD LIGHT AT COCKPIT DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — FAILED (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT AT SEAT ROW 38J INOPERATIVE. REPLACED EMERGENCY EXIT PATH LIGHT CONNECTOR AT SEAT ROW 38J. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: IDG — FAILED (LT GENERATOR)
GRU - DEFERRED LEFT IDG INOP AS PER MEL REF SERVICED BOTH IDGS AND APU OIL AS PER MEL REQUIRED. MIC SHEET ENTERED AND PLACARDED. REMOVED AND REPLACED LEFT ENGINE IDG PER MM EMP NR 486574. OPS CHECK GOOD. LEAK CHECK GOOD. CLEARED MEL 24-01. AUTH 5-320DC-B. CLEARED MIC SHEET. (M)
Part: TRANSCEIVER — FAILED (LT HF)
JFK - FLT 0068 - BOTH HF RADIOS INOP IN-FLIGHT SUSPECT ANTENNA COUPLER. TROUBLESHOT SYSTEM. REPLACED DEFECTIVE LT HF TRANSCEIVER AND RT HF COUPLER. BOTH SYSTEMS CHKS NORMAL. (X)
Part: WIRE — BROKEN (CABIN)
SFO - DURING MAINTENANCE, DISCOVERED EMERGENCY EXIT LIGHT AT PASSENGER SEAT 30B INOPERATIVE. REPAIRED BROKEN WIRE AT EMERGENCY EXIT LIGHT CONNECTOR, PASSENGER SEAT 30B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1997
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 29H INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: CONNECTOR — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 21A/B INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AND CONTACTS AT PAX SEAT 21 A/B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FLOOR BEAM — CORRODED (BS 867-921)
AFW - FOUND CORROSION ON FLOOR BEAM AFTER BLENDING TO BE BEYOND SRM LIMITS. FOUND AND BLENDED OUT CORROSION. ATTACHED A FABRICATED STRAP OF .050 301 1/2 HARD STAINLESS. ALODINED, PRIMED AND PAINTED PER ENGINEERING MRB NR 767-1237. (M)
Part: MOUNT — CORRODED (GALLEY)
AFW - FOUND G6 GALLEY MOUNT HAS CORROSION ON INBOARD VERTICAL AND HORIZONTAL SURFACE BEYOND SRM LIMITS. REMOVE EXISTING CORROSION, FABRICATE REPAIR FITTING PER ENGINEERING MRB 767-1230.
1995
Part: EEL CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 9H FOUND INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT CONNECTOR AS PASSENGER SEAT 9H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: FLOOR BEAM — CORRODED (BS 834)
AFW - TOP SIDE OF FLOOR BEAM CORRODED BEYOND SRM LIMITS. SPLICED IN NEW SECTION OF FLOOR BEAM PER MRB 767-1017. (M)
Part: EEL INVERTER — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTING IN MID-GALLEY FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHTING INVERTER. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: EEL WIRE — BROKEN (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT RT AISLE IN FIRST CLASS INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT FORWARD AREA OF RIGHT AISLE IN FIRST CLASS CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: EEL CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHT AT PAX SEAT 30AB INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT CONNECTOR AT PAX SEAT 30 AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (W)