N377AN
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.
138 reports on file, 1995-05-08 – 2018-07-02.
Part: SKIN — CRACKED (BS 1923) · airframe 101,227 hrs · 16,248 cycles
FOUND A CRACK ON THE EXTERNAL FUSELAGE SKIN, BS 1923, 10 INCHES BELOW STRINGER 25R
Part: SKIN — DENTED (BS 1562-1582) · airframe 101,227 hrs · 16,248 cycles
DEEP DENT FOUND ON THE EXTERNAL FUSELAGE SKIN BETWEEN BS 1562 - 1582, STRINGERS 24L - 26L
Part: SKIN — CRACKED (BS 1271) · airframe 101,227 hrs · 16,248 cycles
FOUND A CRACK ON AN EXISTING BLENDOUT, EXTERNAL FUSELAGE SKIN, AFT OF THE CARGO DOOR CUTOUT, BS 1271, BETWEEN STRINGERS 29R AND 30R.
Part: FRAME — CRACKED (BS 903) · airframe 101,227 hrs · 16,248 cycles
DURING PERFORMANCE OF AD 2012-22-17 AND SB 53A0209, FOUND A CRACK, 0.708 INCH IN LENGTH AT FRAME INNER CHORD TRANSITION RADIUS BS 903.5, RBL 89.
Part: FLOORBEAM — CORRODED (BS 246) · corrosion level 2 · airframe 101,227 hrs · 16,248 cycles
FOUND CORROSION ON THE FLOORBEAM BS 246, RBL 11
Part: FLOOR PANEL — CORRODED (CARGO BAY) · corrosion level 3 · airframe 101,227 hrs · 16,248 cycles
FOUND CORROSION ON THE CARGO FLOOR PANEL NEXT TO LOWER DOOR SILL BETWEEN BS 544 TO 566, RBL 25 TO 36.
Earlier reports · 1995–2017 · 132 reports
2017
Part: CONTROLLER — FAULTY (RT ENGINE) · airframe 101,159 hrs · 16,232 cycles
EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE DUE TO THE RIGHT ENGINE BLEED AND HIGH PRESSURE SHUTOFF VALVE FAULTS. LANDING UNEVENTFUL. REMOVED AND REPLACED HIGH PRESSURE SHUTOFF VALVE AMM 36-11-07 AND HIGH PRESSURE CONTROLLER IAW AMM 36-11-08. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.
Part: SHUTOFF VALVE — FAULTY (RT ENGINE) · airframe 101,159 hrs · 16,232 cycles
EMERGENCY DECLARED. FLIGHT RETURNED TO DEPARTURE DUE TO A RIGHT ENGINE BLEED AND HIGH PRESSURE SHUTOFF VALVE FAULTS. LANDING UNEVENTFUL. REMOVED AND REPLACED HIGH PRESSURE SHUTOFF VALVE IAW AMM 36-11-07 AND HIGH PRESSURE CONTROLLER IAW AMM 36-11-08. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.
Part: COVER — MISSING (EMERGENCY LIGHTS) · airframe 101,131 hrs · 16,223 cycles
EMERGENCY LIGHT COVER AT REAR MID GALLEY MISSING. REPLACED COVER IAW AMM 33-51-00.
Part: FLASHLIGHT — INOPERATIVE (MID CABIN) · airframe 101,131 hrs · 16,223 cycles
FLASHLIGHT IN MID CABIN IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-64-00.
Part: SIGN — DAMAGED (CABIN) · airframe 101,102 hrs · 16,218 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN FLOOR LEVEL BY THE R1 DOOR IS DAMAGED. REMOVED AND REPLACED SIGN PER AMM 33-51-01. OPERATIONAL CHECK GOOD.
Part: STRIKER — FAULTY (COCKPIT DOOR) · airframe 100,423 hrs · 16,090 cycles
EMERGENCY DECLARED. FLIGHT DIVERTED, DUE TO AN ODOR IN CABIN. LANDING UNEVENTFUL. REMOVED AND REPLACED FLIGHT DECK DOOR LOCK ELECTRIC STRIKER IAW AMM 52-51-07. OPERATIONAL CHECK GOOD. AIRCRAFT WAS GROUNDED.
Part: SKIN — CRACKED (BS 1219) · airframe 100,203 hrs · 16,037 cycles
AIRCRAFT BELLY HAS A 1 INCH CRACK BELOW THE AFT CARGO FLOORING OPENING AT BS 1219, STRINGER 39L. REPAIRED IAW SRM 53-00-01-2R-1. AIRCRAFT WAS GROUNDED.
Part: MECHANISM — LACK OF LUBE (L1 DOOR) · airframe 100,199 hrs · 16,036 cycles
AIRCRAFT WAS NOT GROUNDED. L1 DOOR IS DIFFICULT TO ARM. LUBRICATED GIRT BAR CARRIER ASSEMBLY (AALA201705089029) AND ARMING MECHANISM IAW AMM 12-21-18. OPERATIONAL CHECK IAW AMM 52-11-00 GOOD.
Part: CARRIER ASSY — LACK OF LUBE (L1 DOOR) · airframe 100,199 hrs · 16,036 cycles
AIRCRAFT WAS NOT GROUNDED. L1 DOOR IS DIFFICULT TO ARM. LUBRICATED GIRT BAR CARRIER ASSEMBLY AND ARMING MECHANISM (AALA201705099023) IAW AMM 12-21-18. OPERATIONAL CHECK IAW AMM 52-11-00 GOOD.
Part: FLASHLIGHT — INOPERATIVE (CABIN) · airframe 99,954 hrs · 15,978 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT ACROSS FROM SEATS 17A/B IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.
Part: SHOCK MOUNT — CORRODED (APU) · airframe 99,903 hrs · 15,965 cycles
LEFT AFT AUXILIARY POWER UNIT SHOCKMOUNT IS CORRODED. REMOVED AND REPLACED SHOCKMOUNT IAW AMM 49-13-02. OPERATIONAL CHECKED GOOD.
Part: COVER — MISSING (CABIN) · airframe 99,853 hrs · 15,953 cycles
AIRCRAFT WAS NOT GROUNDED. ESCAPE PATH LIGHT NEAR SEAT 43G AND LAVATORY A6 HAS AN EXPOSED WIRE. REPLACED MISSING WIRE COVER IAW ESO 11922 AND CMM 25-48-15 PAGE 1072. OPERATIONAL CHECK GOOD.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 99,784 hrs · 15,936 cycles
AIRCRAFT WAS GROUNDED. DURING WALK AROUND, FOUND SMALL AREA OF DEFORMATION/BULGE MEASURING 1.5 INCH AT FUSELAGE STATION 440 BETWEEN STRINGERS 33L AND 34L. REPAIRED IAW SRM 53-00-01-2R-1 AND SRM 53-30-03-2R-1.
Part: CHARGER — FAILED (EMERGENCY LIGHTS) · airframe 99,697 hrs · 15,918 cycles
SEAT MOUNTED EMERGENCY LIGHTS FROM SEATS 20AB TO 24AB FAILED TO TEST. REMOVED AND REPLACED BATTERY CHARGER M737 IAW AMM 33-51-07. OPERATIONAL CHECKED GOOD.
Part: WIRE — UNSECURE (CABIN) · airframe 99,667 hrs · 15,905 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT HAS WIRES HANGING. SECURED EMERGENCY LIGHT WIRES IAW SWP 26-10-00. OPERATIONAL CHECK GOOD.
Part: CONNECTOR — DISCONNECTED (ZONE 100) · airframe 99,490 hrs · 15,871 cycles
DURING CRUISE THE CABIN TEMPERATURE BECAME UNCONTROLLABLE. MAINTENANCE FOUND LEFT PACK TURBINE INLET TEMPERATURE BULB CONNECTOR PLUG D1338 DISCONNECTED, RECONNECTED. FOUND RIGHT PACK COMPRESSOR OUTLET OVERHEAT SWITCH CONNECTOR PLUG D1562 DISCONNECTED, RECONNECTED. REMOVED AND REPLACED RIGHT COMPRESSOR OUTLET SWITCH AND RIGHT FLOW CONTROL CARD IAW AMM 21-51-09. SYSTEM CHECKED NORMAL.
Part: CONNECTOR — DISCONNECTED (ZONE 100) · airframe 99,490 hrs · 15,871 cycles
DURING CRUISE THE CABIN TEMPERATURE BECAME UNCONTROLLABLE. EMERGENCY DECLARED. RETURNED TO DEPARTURE. AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND LEFT PACK TURBINE INLET TEMPERATURE BULB CONNECTOR PLUG D1338 DISCONNECTED, RECONNECTED. FOUND RIGHT PACK COMPRESSOR OUTLET OVERHEAT SWITCH CONNECTOR PLUG D1562 DISCONNECTED, RECONNECTED. REMOVED AND REPLACED RIGHT COMPRESSOR OUTLET SWITCH AND RIGHT FLOW CONTROL CARD IAW AMM 21-51-09. SYSTEM CHECKED NORMAL.
Part: SWITCH — FAULTY (ZONE 100) · airframe 99,490 hrs · 15,871 cycles
DURING CRUISE THE CABIN TEMPERATURE BECAME UNCONTROLLABLE. EMERGENCY DECLARED. RETURNED TO DEPARTURE. AIRCRAFT WAS GROUNDED. MAINTENANCE FOUND LEFT PACK TURBINE INLET TEMPERATURE BULB CONNECTOR PLUG D1338 DISCONNECTED, RECONNECTED FOUND RIGHT PACK COMPRESSOR OUTLET OVERHEAT SWITCH CONNECTOR PLUG D1562 DISCONNECTED, RECONNECTED. REMOVED AND REPLACED RIGHT COMPRESSOR OUTLET SWITCH AND RIGHT FLOW CONTROL CARD IAW AMM 21-51-09. SYSTEM CHECKED NORMAL.
Part: CIRCUIT CARD — FAULTY (ZONE 100) · airframe 99,490 hrs · 15,871 cycles
DURING CRUISE THE CABIN TEMPERATURE BECAME UNCONTROLLABLE. EMERGENCY DECLARED. RETURNED TO DEPARTURE. MAINTENANCE FOUND LEFT PACK TURBINE INLET TEMPERATURE BULB CONNECTOR PLUG D1338 DISCONNECTED, RECONNECTED. FOUND RIGHT PACK COMPRESSOR OUTLET OVERHEAT SWITCH CONNECTOR PLUG D1562 DISCONNECTED, RECONNECTED. REMOVED AND REPLACED RIGHT COMPRESSOR OUTLET SWT5556 AND RIGHT FLOW CONTROL CARD PER AMM 21-51-09. SYSTEM CHECKS NORMAL. AIRCRAFT WAS GROUNDED.
2016
Part: SWITCH — DIRTY (ZONE 200) · airframe 98,813 hrs · 15,718 cycles
AIRCRAFT WAS NOT GROUNDED. NR 1 ENGINE DID NOT SHUTDOWN ON FIRST ATTEMPT, CYCLING THE FUEL CONTROL SWITCH TO RUN AND THEN CUTOFF SHUTDOWN THE ENGINE. CLEANED NR 1 ENGINE FUEL CONTROL SWITCH. OPERATIONAL CHECK GOOD IAW AMM 76-11-00.
Part: GIRT BAR — OBSTRUCTED (L1 DOOR) · airframe 98,672 hrs · 15,683 cycles
AIRCRAFT NOT GROUNDED. L1 DOOR EMERGENCY SLIDE WILL NOT ARM DUE TO SCREW/DEBRIS BLOCKING GIRT BAR PATH. REMOVED DEBRIS IAW GPM. OPERATIONAL CHECK GOOD.
Part: SLIDE — DAMAGED (R1 DOOR) · airframe 96,895 hrs · 15,318 cycles
DAMAGED R1 DOOR SLIDE, R & R R1 DOOR SLIDE IAW AMM 25-66-01. ACFT IN BASE MX.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,895 hrs · 15,318 cycles
CORROSION ON T CAP STATION 347, RBL 21 - 90. REPAIRED FLOORBEAM IAW SRM 53-00-51-2R-1. ACFT IN BASE MX.
Part: SKIN — CORRODED (RT HORIZ STAB) · corrosion level 2 · airframe 96,895 hrs · 15,318 cycles
CORROSION ON HORIZONTAL STABILIZER, UPPER SKIN AT FWD SPAR, 23" RBL. APPLIED DOUBLER REPAIR IAW EA 258491. ACFT IN BASE MX.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,895 hrs · 15,318 cycles
CORROSION ON T CAP, AT STATION 325, FROM RBL 62-LBL 30. ACCOMPLISHED T CAP REPAIR IAW SRM 53-00-51-2R-1. ACFT IN BASE MX.
Part: SKIN — GOUGED (FUSELAGE) · airframe 96,895 hrs · 15,318 cycles
GOUGE IN SKIN AT STATION 1280 & STRINGERS 38L-38R. COMPLIED WITH PERMANENT SKIN REPAIR IAW SRM 53-00-01 REPAIR 29. ACFT IN BASE MX.
Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 96,895 hrs · 15,318 cycles
R2 AFT SERVICE DOOR, FOUND CORROSION ON EDGE OF EXTRUSION, MIDDLE OF LOWER DOOR SILL, STATION 1510.5, WL 200. REPLACED EXTRUSION IAW AARD 51-00-05 & PRINT 146T0051. ACFT IN BASE MX.
2015
Part: POWERPACK — DISCHARGED (CABIN) · airframe 96,201 hrs · 15,171 cycles
EMERGENCY LIGHTS AT SEAT 17B INOPERATIVE. R & R EMER LIGHT POWER PACK AT ROW 19 IAW AMM 33-51-06. OPERATIONAL CHECKED NORMAL.
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 94,272 hrs · 14,859 cycles
SEAT 34B CEILING EMERGENCY LIGHT MISSING LENS. REPLACED LENS AT SEAT 34B EMERGENCY LIGHT IAW AMM 33-51-00. OPERATIONALLY CHECKED NORMAL.
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 94,272 hrs · 14,859 cycles
DOOR 4L EMERGENCY LIGHT LENS BROKEN. R & R EMERGENCY LIGHT ASSEMBLY CPN 4075752, CPN 4205890 AT 4L DOOR IAW AMM 33-51-00. OPERATIONS CHECKED NORMAL.
Part: COVER — LOOSE (CABIN) · airframe 93,996 hrs · 14,816 cycles
L4 EMER LIGHT COVER ASSEMBLY LOOSE. SECURED L4 EMER LIGHT COVER WITH PROPER HARDWARE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 93,273 hrs · 14,687 cycles
ON WALK THROUGH INSPECTION OF SEAT MOUNTED EMER PATH LIGHTING FOUND SEAT NR 25B LIGHT INOPERATIVE. REPLACED EMER PATH LIGHT BULB AT SEAT NR 25B. OPERATIONAL CHECK GOOD IAW MM 33-51-05.
2014
Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,880 hrs · 14,632 cycles
RIGHT AISLE EMER LIGHT AT SEAT 20G HAS ONE BULB INOPERATIVE. R & R LAMP IAW AMM 33-33-51-09. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,880 hrs · 14,632 cycles
ONE SEAT MOUNTED EMER LIGHT HAS ONE BULB INOPERATIVE AT SEAT 22B. R & R LAMP IAW AMM 33-51-10. SYS CHECKED NORMAL.
Part: LENS — MISSING (CABIN) · airframe 92,880 hrs · 14,632 cycles
LEFT AISLE CEILING EMER LIGHT LENS IS MISSING AT ROW 37. INSTALLED NEW LENS IAW AMM 33-51-04. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,880 hrs · 14,632 cycles
ONE SEAT MOUNTED EMER LIGHT HAS ONE BULB INOPERATIVE AT SEAT 36H. R & R LAMP IAW AMM 33-51-10. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,880 hrs · 14,632 cycles
ONE SEAT MOUNTED EMER LIGHT HAS ONE BULB INOPERATIVE AT SEAT 26H. R & R LAMP IAW AMM 33-51-10. SYS CHECKED NORMAL.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 92,880 hrs · 14,632 cycles
L1 DOOR EXIT HANDLE LIGHT HAS ONE BULB INOPERATIVE. R & R M1208 CHARGER IAW AMM 33-51-07. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 92,880 hrs · 14,632 cycles
RIGHT EXTERIOR EMER SLIDE LIGHT ABOVE AFT CORNER OF FAIRING IS INOPERATIVE. R & R LAMP IAW AMM 33-51-06. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 92,880 hrs · 14,632 cycles
L1 DOOR EXIT HANDLE LIGHT HAS ONE BULB INOPERATIVE. R & R LAMP IAW AMM 33-51-01. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 92,880 hrs · 14,632 cycles
R4 DOOR EXIT IDENTIFIER HAS ONE BULB INOPERATIVE. R & R LAMP IAW AMM 33-51-09. SYS CHECKED NORMAL.
Part: PORTABLE LIGHT — INOPERATIVE (CABIN) · airframe 92,880 hrs · 14,632 cycles
FLIGHT DECK PORTABLE EMER LIGHT IS INOPERATIVE. R & R LIGHT ASSEMBLY IAW AMM 25-64-00. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,880 hrs · 14,632 cycles
L1 DOOR FLIGHT ATTENDANT PANEL EMER GUARDED PUSHBUTTON LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-23-03. SYS CHECKED NORMAL.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 92,880 hrs · 14,632 cycles
R1 DOOR EXIT HANDLE LIGHT HAS ONE BULB INOPERATIVE. R & R M1208 CHARGER IAW AMM 33-51-07. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 92,880 hrs · 14,632 cycles
EXTERIOR EMER SLIDE LIGHT ABOVE AIR DEMAND PUMP EXHAUST IS INOPERATIVE. R & R LAMP IAW AMM 33-51-06. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,880 hrs · 14,632 cycles
ONE SEAT MOUNTED EMER LIGHT HAS ONE BULB INOPERATIVE AT SEAT 25B. R & R LAMP IAW AMM 33-51-10. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 92,880 hrs · 14,632 cycles
LEFT FWD OVERWING EXIT IDENTIFIER HAS ONE BULB INOPERATIVE. R & R LAMP IAW AMM 33-51-09. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (ZONE 200) · airframe 92,880 hrs · 14,632 cycles
R1 DOOR EXIT HANDLE LIGHT HAS ONE BULB INOPERATIVE. R & R LAMP IAW AMM 33-51-01. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 92,880 hrs · 14,632 cycles
ONE SEAT MOUNTED EMER LIGHT HAS ONE BULB INOPERATIVE AT SEAT 24B. R & R LAMP IAW AMM 33-51-10. SYS CHECKED NORMAL.
Part: FASTENER — IMPROPER PART (PSU) · airframe 92,374 hrs · 14,544 cycles
SEAT 39CEG FAILED TO DEPLOY O2 MASKS DURING OPERATIONAL CHECK. IMPROPER FASTENERS ALLOWED PSU FWD FRAME OF SEAT 39CEG TO HANG LOOSELY & WEDGE THE LATCH. INSTALLED PROPER FASTENERS IN PSU FWD FRAME FOR SEAT 39CEG IAW AMM 25-23-01.
Part: O-RING — DAMAGED (HYDRAULIC SYS) · airframe 92,216 hrs · 14,517 cycles
CREW REPORTED CTR HYD SYS QTY LOSS. EMER DECLARED FLIGHT RETURNED & LANDED WITHOUT INCIDENT. ACFT REMOVED FROM SERVICE. REPLACED O RING AT C2 ALTERNATING CURRENT MOTOR PUMP FILTER MODULE OUTERMOST PRESS LINE. SYS GND CHECKED NORMAL OPERATION CLOSED.
Part: STRUCTURE — CRACKED (FUSELAGE) · airframe 92,086 hrs · 14,495 cycles
AN ATYPICAL CRACK CONFIGURATION WAS OBSERVED ON THE ABOVE INDICATED PART AT THE LOCATION DEPICTED IN THE SKIN & BULKHEAD OUTER CHORD STATION 1725.5 & STRINGER 7 RT. ACCOMPLISHED REPAIR IAW EA B767-53-036337 DATED 8/28/2014.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 91,780 hrs · 14,434 cycles
LEFT NR 1 DOOR, UPPER FWD EMER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR LT NR 1 DOOR UPPER FWD EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 91,780 hrs · 14,434 cycles
LEFT NR 4 DOOR, LOWER AFT EMER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 91,780 hrs · 14,434 cycles
EMERGENCY EXIT SIGN FWD OF SEAT 20G INOPERATIVE. REPLACED LAMP FOR EMER EXIT SIGN FWD OF SEAT 20G. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 91,780 hrs · 14,434 cycles
RIGHT NR 4 DOOR LOWER AFT EMER EXIT SIGN INOPERATIVE. REPLACED LAMP FOR RT NR 4 DOOR LOWER AFT EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: MOUNT — BROKEN (CABIN) · airframe 91,262 hrs · 14,349 cycles
LEFT AFT SERVICE DOOR EMERGENCY EXIT LIGHT ASSEMBLY MOUNT IS BROKEN. REINSTALLED LT AFT SERVICE DOOR EMERGENCY LIGHT ASSEMBLY & REPLACED LENS. OPERATIONS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,858 hrs · 14,282 cycles
CABIN EMERGENCY LIGHT ASSEMBLY INOPERATIVE. REPLACED BATTERY PACK & CHARGER, OPERATIONS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 90,452 hrs · 14,221 cycles
LT LOWER FUSELAGE SLIDE EMERGENCY LIGHT INOPERATIVE. REPLACED BATTERY PACK, OPERATIONS CHECKED NORMAL.
Part: LENS — BROKEN (EXIT SIGN) · airframe 89,961 hrs · 14,141 cycles
LT NR 4 DOOR EXIT SIGN BROKEN. SECURED BROKEN BRACKET & REPLACED LENS ON EXIT SIGN AT LT NR 4 DOOR. OPERATIONS CHECKED NORMAL.
2013
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 89,021 hrs · 13,988 cycles
LT SIDE EXTERIOR FS MOUNTED EMERGENCY EXIT ILLUMINATION LIGHTS 1 TO 4 INOPERATIVE. REPLACED BATTERY PACK M00736. OPERATIONS CHECKED NORMAL.
Part: POWER SUPPLY — DISCHARGED (CABIN) · airframe 88,738 hrs · 13,936 cycles
RT HAND SIDE MID GALLEY EMERGENCY LIGHT INOPERATIVE. REPLACED POWER SUPPLY M732. OPERATIONS CHECKED NORMAL.
Part: SMOKE WARNING — FALSE ACTIVATION (COCKPIT) · airframe 88,354 hrs · 13,878 cycles
CDG CREW REPORTED DURING CLIMB, SMOKE DETECTORS FROM LAVATORIES F1 & FS3 ACTIVATED. NO SMOKE, FIRE OR SMELL NOTED. FLIGHT LANDED CDG WITHOUT INCIDENT. ACCOMPLISHED LAVATORY SMOKE DETECTION & FIRE PROTECTION PROBLEM WITH NO FAULTS FOUND. SYSTEM GROUND CHECKED NORMAL. OPERATION (CLOSED).
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 86,657 hrs · 13,617 cycles
SKIN BULGING AROUND FASTENER HEADS AT STATION 1197. CUTOUT DAMAGE AND INSTALLED REPAIR DOUBLER AND FILLER PER SRM 53-00-01-2R-1.
Part: SKIN — DENTED (FUSELAGE) · airframe 86,657 hrs · 13,617 cycles
DENT AT STATION 412 AND STRINGER 19 RIGHT. INSTALLED SKIN DOUBLER PER SRM 53-00-01-2R-1.
Part: SKIN — DENTED (FUSELAGE) · airframe 86,657 hrs · 13,617 cycles
UPPER SKIN ALONG TRAILING EDGE 48 INCHES FROM INBOARD END OF FLAP. ACCOMPLISHED BONDED REPAIR PER SRM 51-70-10-2R.
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,716 hrs · 13,470 cycles
PORTABLE EMERGENCY LIGHT OVER COCKPIT DOOR INOPERATIVE. REPLACED LIGHT ASSEMBLY. OPS CHECK NORMAL.
Part: WIRE — BROKEN (LE SLAT) · airframe 85,013 hrs · 13,368 cycles
LHR - CREW REPORTED LEADING EDGE SLAT ASYMMETRY EICAS MESSAGE DURING CLIMBOUT. EMERGENCY DECLARED FLIGHT RETURNED LHR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPAIRED PROXIMITY SENSOR S279 THAT HAD BROKEN WIRE. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: FITTING — CRACKED (LT WING) · airframe 83,751 hrs · 13,177 cycles
LEFT WING AFT OUTBOARD PITCHLOAD FITTING HOLE CRACKED. FREEZE PLUG INSTALLED PER ECO C3194.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,391 hrs · 13,117 cycles
LEFT AFT FUSELAGE EMERGENCY LIGHTS INOPERATIVE. REPLACED LAMP FOR LEFT AFT FUSELAGE EMERGENCY LIGHTS. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,391 hrs · 13,117 cycles
SEAT MOUNTED EMERGENCY LIGHT AT 23H INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT 23H. OPS CHECK NORMAL.
Part: LENS — MISSING (CABIN) · airframe 83,391 hrs · 13,117 cycles
EMERGENCY LIGHT AT SEAT 23H MISSING CLEAR LENS. REPLACED LENS FOR EMERGENCY LIGHT AT 23H. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,440 hrs · 12,960 cycles
LEFT AFT FUSELAGE EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT AFT FUSELAGE EMERGENCY LIGHT. OPS CHECK NORMAL.
2011
Part: GENERATOR — FAILED (RT ENGINE) · airframe 81,921 hrs · 12,886 cycles
MVD - CREW REPORTED RIGHT ENGINE GENERATOR FAILED WITH AUXILIARY POWER UNIT ON MEL. EMERGENCY DECLARED FLIGHT RETURNED MVD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.
2010
Part: COVER — LOOSE (CABIN) · airframe 77,748 hrs · 12,237 cycles
EMERGENCY EXIT LIGHT COVER LOOSE AT SEAT 20A. REPLACED LENS AT OVERWING DOOR. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 76,276 hrs · 12,008 cycles
EMERGENCY LIGHT IN CABIN INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN CABIN. OPS CHECK NORMAL.
Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 75,666 hrs · 11,893 cycles
MIA - INFLIGHT ORD-MBJ CREW REPORTED LEFT HYDRAULIC SYSTEM QUANTITY DECREASING SLOWLY IN FLIGHT. FLIGHT DIVERTED LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED HYDRAULIC LINE THAT WAS LEAKING. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,451 hrs · 11,854 cycles
STATIONS 525 TO 526 BOTTOM CHORD AT LOWER DOOR CUTOUT CORRODED. ACCOMPLISHED REPAIR PER EA B767-53-010003.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,451 hrs · 11,854 cycles
STATION 1307 STRINGER 35 LEFT CORRODED. ACCOMPLISHED SPLICE REPAIR PER EA B767-53-010006.
Part: FAILSAFE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,451 hrs · 11,854 cycles
STATION 614 BOTTOM SIDE OF FAIL SAFE STRAP CORRODED. ACCOMPLISHED REPAIR PER EA B767-53-010004.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 75,451 hrs · 11,854 cycles
STATION 1307 STRINGER 35 LEFT CORRODED. ACCOMPLISHED SPLICE REPAIR PER EA B767-53-010005.
Part: FRAME — DAMAGED (FUSELAGE) · airframe 75,451 hrs · 11,854 cycles
FRAME STATION 500 STRINGER 30 LEFT AND 31 LEFT DAMAGED. ACCOMPLISHED REPAIR PER EA B767-53-010067.
2009
Part: RELAY — INOPERATIVE (ESCAPE SLIDE) · airframe 74,314 hrs · 11,659 cycles
LEFT SLIDE DOES NOT TEST ON SYSTEM 1. REPLACED RELAY.
Part: LENS — BROKEN (CABIN) · airframe 74,118 hrs · 11,617 cycles
EMERGENCY LIGHT AT SEAT 33B BROKEN. REPLACED LENS AND LAMPS.
Part: SOCKET — BROKEN (CABIN) · airframe 74,118 hrs · 11,617 cycles
EMERGENCY LIGHT AT SEAT 27B BROKEN. REPLACED SOCKET ASSEMBLY AND LAMPS.
Part: LIGHT — CRACKED (CABIN) · airframe 73,935 hrs · 11,592 cycles
PRIOR TO DEPARTURE FLIGHT ATTENDANT REPORTED EMERGENCY EXIT LIGHT AT MID GALLEY WALL WAS CRACKED. REPLACED THE MID GALLEY EMERGENCY EXIT LIGHT ASSEMBLY.
Part: CONNECTOR — DAMAGED (EMERGENCY LIGHTS) · airframe 71,532 hrs
SFO - EMERGENCY FLOOR PATH LIGHTING AT SEAT 29HJ INOPERATIVE DUE TO BROKEN WIRING. REPLACED SEAT 29HJ EMERGENCY LIGHT CONNECTOR.
Part: LAMP — BURNED OUT (EMERGENCY LIGHTS) · airframe 71,532 hrs
SFO - LEFT EXTERIOR EMERGENCY LIGHT 6TH FROM FORWARD POSITION INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT EXTERIOR 6TH FROM FORWARD POSITION.
Part: POWER SUPPLY — DISCHARGED (EMERGENCY LIGHTS) · airframe 71,532 hrs
SFO - EMERGENCY PATH LIGHTING AT SEAT 24HJ AND 22HJ INOPERATIVE. REPLACED POWER SUPPLY AT 23H.
2008
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 70,464 hrs
DFW - EMERGENCY LIGHT AT SEAT 41H MISSING LENS. REPLACED LENS AT SET 41H. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
JFK EMERGENCY LIGHT EXIT SIGN AT LT OVERWING INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT EXIT SIGN AT LT OVERWING. SYSTEM GROUND CHECKED NORMAL OPS.
Part: EEC — INOPERATIVE (NR 1 ENGINE)
BDL INFLIGHT T160/06 SEP SAN TO JFK. CREW REPORTED UNCOMMANDED SHUTDOWN OF NR 1 ENGINE. LANDED BDL WITHOUT INCIDENT. REPLACED NR 1 ENGINE ELECTRONIC ENGINE CONTROL UNIT. SYSTEM GROUND CHECKED NORMAL OPS.
Part: LENS — MISSING (CABIN) · airframe 68,735 hrs
JFK - EMERGENCY LIGHT AT RT MID GALLEY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RT MID GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 68,723 hrs
SFO - EXTERNAL EMERGENCY LIGHT AT LT AFT INOPERATIVE. REPLACED LAMP FOR EXTERNAL EMERGENCY LIGHT AT LT AFT. SYSTEM GROUND CHECK NORMAL OPERATION. (A)
2007
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 66,332 hrs
MIA - EMERGENCY LIGHT AT SEAT 25B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 25B. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE — DAMAGED (EMERGENCY LIGHTS)
LAX - EMERGENCY LIGHT AT AFT LEFT OVERWING EXIT SIGN INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHT AT AFT LEFT OVERWING EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: BULB — INOPERATIVE (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT AT AFT LEFT EXIT INOPERATIVE. RELAMPED EMERGENCY LIGHT AT AFT LEFT HAND EXIT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — INOPERATIVE (EMERGENCY LIGHTS)
MIA - EMERGENCY LIGHT AT SEAT 37H INOPERATIVE. RESECURED CONNECTION FOR EMERGENCY LIGHTS AT SEAT 37H. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
LAX - EMERGENCY EXIT LIGHT AT SEATS 41HJ INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY FOR SEATS 41HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY LIGHT AT SEAT 37H INOPERATIVE. RELAMPED EMERGENCY LIGHT AT SEAT 37H. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY LIGHT AT MID GALLEY BULKHEAD ON LEFT SIDE INOPERATIVE. REPLACED LIGHT ASSEMBLY AT MID GALLEY BULKHEAD ON LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: SKIN — DAMAGED (FUSELAGE)
AFW - FUSELAGE SKIN AND SPLICE PLATE AT STATION 434 BETWEEN S 25R AND S 24R IS DAMAGED AND CRACKED. DISCREPANCY AREA IS 5.5 INCH BY 5.5 INCH. REPAIRED DAMAGE AT THE SKIN AND AT THE BUTT SPLICE STRAP PER REPAIR INSTRUCTIONS IN PAGE 2 AND FIGURE 1 AND 2 OF MRB 767 2599.
Part: STRINGER — CRACKED (FUSELAGE)
AFW - STRINGER 25R AT STATION 439 HAS A CRACK OF ONE INCH ON THE VERTICAL LEG AFT OF THE LAST FASTENER HOLE OF THE STRINGER SPLICE. REPAIRED STRINGER S25R USING MRB 767 2598. STRINGER SPLICE EXTENDED BY TWO FASTENER ROWS BEYOND THE EDGE OF THE REPAIR DOUBLER.
Part: LIGHT — BROKEN (SEAT 24B)
LAX - EMERGENCY LIGHT ASSEMBLY AT SEAT 24B BROKEN. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 24B. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: COMPUTER — ERRATIC (E/E COMPT)
LEFT EICAS COMPUTER STATUS MESSGE TURNING SELECTOR TO LEFT BOTH SCREENS BLANK. LEFT EICAS COMPUTER WORKING NORMAL ON ARRIVAL. LEFT EICAS COMPUTER CHECKED SECURE, LEFT EICAS COMPUTER C/B CYCLED STATUS MESSAGE SELF ERASED EICAS TEST CARRIED OUT PASSED NIL FAULTS. (M)
Part: CONNECTOR — INOPERATIVE (CABIN)
DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 33H INOPERATIVE. REPLACED EMERGENCY EXIT ILGHT PIN IN CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35C INOPERATIVE. SECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 35C. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SOCKET — DEFECTIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 24H INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT SOCKET ON SEAT 24H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: SOCKET — DISCONNECTED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35H INOPERATIVE. RECONNECTED EMERGENCY EXIT LIGHT SOCKET ON SEAT 35H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — DAMAGED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 29B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE ON SEAT 29B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: WIRE — BROKEN (RT ENGINE)
EN ROUTE ORD-LHR, RIGHT ENGINE BLEED OVER TEMP. DECLARED EMERGENCY AND LANDED JFK UNEVENTFULLY. AIRCRAFT LANDED OVERWEIGHT. REPAIRED WIRES FOR RIGHT OVER TEMP SWITCH AND REPLACED SENSE LINE TO RIGHT PRE-COOLER. PERFRMED ENGINE RUN AND OVERWEIGHT INSPECTION. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT ROW 31 INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT ROW 31. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE LIGHTS AT ROW 2H THROUGH 8H INOPERATIVE. REPLACED EMERGENCY ESCAPE LIGHTING ASSEMBLY AT ROW 2H THROUGH 8H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY PACK — DISCHARGED (CABIN)
ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS ROW 2H AND 8H INOPERATIVE. REPLACED EMERGENCY ESCAPE PATH LIGHTS BATTERY PACK FOR ROWS 2H AND 8H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: CONNECTOR — INOPERATIVE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 28B INOPERATIVE. RESEATED EMERGENCY EXIT LIGHT CONNECTOR AT BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: LIGHT — INOPERATIVE (CABIN)
MIA - DURING OVER-NIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE PATH LIGHT AT SEAT 34B INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 34B. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1999
Part: CONNECTOR — BROKEN (SEAT 37)
ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 37H INOPERATIVE. REPAIRED EMERGENCY EXIT SEAT PATH LIGHT CONNECTOR AT SEAT 37H. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: LIGHT — INOPERATIVE (SEAT 34H)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 34H INOPERATIVE. REPAIRED WIRING AT EMERGENCY EXIT LIGHT AT SEAT 34H. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: WIRE — BROKEN (ROW 38H)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 38H INOPERATIVE. REPAIRED WIRING TO EMERGENCY EXIT FLOOR PATH LIGHT AT SEAT 38H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — DAMAGED (ROW 39AB)
SFO - DURING MAINTENANCE CHECK, EMERGENCY EXIT PATH LIGHT AT PASSENGER SEAT ROW 39AB INOPERATIVE. REPAIRED EMERGENCY EXIT PATH CONNECTOR AT SEAT ROW 39AB. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
1998
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT 7H INOPERATIVE. SECURED EMERGENCY EXIT SEAT LIGHT CONNECTOR AT 7H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FLOORBEAM — CORRODED (BS 347)
AFW - FLOORBEAM AT STATION 347, RBL 11 HAD CORROSION BLENDED ON TOP SURFACE. FLOORBEAM AT STATION 347, RBL NR 11 HAD CORROSION BLENDED ON TOP SURFACE BEYOND SRM LIMITS. (M)
Part: FLOORBEAM — CORRODED (BS 1480)
AFW - FLOORBEAM AT STATION RBL 78 AND 75 HAD CORROSION BLENDED ON TOP SURFACE BEYOND SRM LIMITS. FABRICATED EXTENDED REPAIR STRAP FROM .063-7075-T6. INSTALL REPAIR STRAP WET WITH BMS 5-95 USE BACB3DW6 FASTENERS OR EQUIVALENT. (M)
Part: FLOORBEAM — CORRODED (BS 347)
AFW - FLOORBEAM AT STATION 347 HAS CORROSION REMOVAL ON UPPER SURFACE. FABRICATED REPAIR STRAPS FROM .063-7-75-T6. INSTALLED REPAIR STRAPS, WET WITH BMS5-95. SEALANT USE BACB30NW6, FASTENERS OR EQUIVALENT. (M)
Part: CONNECTOR — FAILED (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT SEAT LIGHTS AT 36AB INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AND PINS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — FAILED (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT SEAT LIGHTS AT 7HJ INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT TERMINAL CONNECTOR. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: CONNECTOR — FAILED (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT LIGHT AT SEAT 36 A/B INOPERATIVE. REPLACED CONNECTOR ON LOWER SEAT LEG OF SEAT 36. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS AT SEAT 7H INOPERATIVE. RECONNECTED EMERGENCY LIGHT CONNECTOR AT SEAT 7H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: IDG — FAILED (RT ENGINE)
MIA - FLT 920 - RT GEN DRIVE LT REMAINED ON STEADY DURING DESCENT. RT GEN DRIVE DISCONNECTED AS PER FT MANUAL, APU STARTED. REMOVED AND REPLACE RT ENGINE IDG GEN ASSY, OPS CHECK NORMAL. LEAK CHECKS NORMAL. OK FOR SERVICE. (M)
1997
Part: ECU — FAILED (LE FLAPS)
JFK - FLT 45 - AFTER TAKEOFF WHEN FLAP HANDLE WAS SELECTED FROM 1 DEGREE TO UP EICAS MESSAGE LE ASSEMBLY SLAT AND LEADING EDGE YELLOW LIGHT ILLUMINATED. AIRSPEED WAS APPROX 210 KIAS INCREASING. REPLACED FLAP/FLAT ELECTRONICS UNIT PERFORMED BITE. REPLACED PSEU, PERFORMED BITE AND OPS CHECKS GOOD. NO DEFECTS NOTED. (M)
1995
Part: SEAT TRACK — CORRODED (FS 772)
AFW - FOUND AND BLENDED OUT CORROSION ON UPPER SURFACE OF SEAT TRACK AT RBL 11.0, STA 772. BLEND BEYOND SRM LIMITS. REPAIRED PER MRB 767-909 DATED 4-23-95. CYCLES, 1808. (X)
Part: EEL CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE AT SEAT 34H. RESECUERD LOOSE EMERGENCY EXIT FLOOR PATH LIGHT CONNECTOR AT SEAT LEG. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)