N376AN
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| AMR CORPORATION | Operator | on 2002-07-02 | Operator named in NTSB report |
Accident & incident history
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.
122 reports on file, 1996-02-24 – 2019-12-06.
Part: TRIM SYSTEM — MALFUNCTIONED (STAB) · airframe 92,930 hrs · 15,807 cycles
CREW REPORTS: REJECTED TAKE OFF @ 50 KIAS. UNSCHEDULED STAB TRIM @ 50 KIAS WITH MASTER CAUTION. AIRCRAFT GROUNDED FOR UNSCHEDULED MAINTENANCE. IAW B767 FAULT ISOLATION MANUAL 27-09-FT 813 AND WIRING DIAGRAM 27-41-11, 27-41-31, NO WIRE FAULTS WERE FOUND IN THE SYSTEM. FAULT ISOLATED TO RH AND LH FSPM AND RH POSITION TRANSMITTER. REMOVED AND REPLACED LH AND RH FSPM CARDS IN THE P50, M838, AND M840 IAW B767 AMM 27-58-01 AND REMOVED AND REPLACED POSITION TRANSMITTER IAW B767 AMM 27-58-01. SYSTEMS OPERATIONAL CHECK IAW B767 FIM 27-58-FT 804 AND MCDP TEST 65 IAW B767 FAULT ISOLATION MANUAL 22-04-FT 811, MCDP TEST 66 IAW B767 FIM 22-04FT813, MCDP TEST 30-40, ALL TEST SATISFACTORY. FAULT NOT DUPLICATED. ADDITIONAL MCDP TEST 64 IAW B767 AMM 22-00-02, B767 AMM 28-58-01 AND 27-48-01 TEST SATISFACTORY. HORIZONTAL STAB TRIM CONTROL SYSTEM FUNCTIONAL CHECKS SATISFACTORY. FAULT NOT DUPLICATED. ACFT RELEASED TO SERVICE CAT III FO.
Earlier reports · 1996–2018 · 121 reports
2018
Part: FRAME — CRACKED (FUSELAGE) · airframe 94,744 hrs · 15,241 cycles
DURING PERFORMANCE OF AD 2012-22-17 AND SB 767-53A0209 FOUND CRACK BY LENGTH OF 0.1576" AT FRAME INNER CHORD TRANSITION RADIUS RT STA 903.5 RBL 89.
Part: FRAME — CRACKED (FUSELAGE) · airframe 94,744 hrs · 15,241 cycles
DURING PERFORMANCE OF AD 2012-22-17 AND SB 767-53A0209 FOUND CRACK BY LENGTH OF 0.1182" AT FRAME INNER CHORD TRANSITION RADIUS LT STA 859.5 LBL 89.
Part: FRAME — CRACKED (FUSELAGE) · airframe 94,744 hrs · 15,241 cycles
DURING PERFORMANCE OF AD 2012-22-17 AND SB 767-53A0209 FOUND CRACK BY LENGTH OF 0.7092" AT FRAME INNER CHORD TRANSITION RADIUS LT STA 903.5 LBL 89.
Part: FRAME — CRACKED (FUSELAGE) · airframe 94,744 hrs · 15,241 cycles
DURING PERFORMANCE OF AD 2012-22-17 AND SB 767-53A0209 FOUND CRACK BY LENGTH OF 0.2364" AT FRAME INNER CHORD TRANSITION RADIUS RT STA 903.5 RBL 89.
2017
Part: CHARGER — INOPERATIVE (CABIN) · airframe 94,728 hrs · 15,238 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. EMERGENCY ESCAPE PATH LIGHTS IN THE MID CABIN ARE INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY (AALA20170919013) AND CHARGER ASSEMBLY. OPERATIONAL CHECK GOOD.
Part: BATTERY — DISCHARGED (CABIN) · airframe 94,728 hrs · 15,238 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. EMERGENCY ESCAPE PATH LIGHTS IN THE MID CABIN ARE INOPERATIVE. REMOVED AND REPLACED BATTERY ASSEMBLY AND CHARGER ASSEMBLY (AALA20170919014). OPERATIONAL CHECK GOOD.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 94,622 hrs · 15,211 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT THE FORWARD GALLEY JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY PER AMM 25-64-00. OPERATIONAL CHECK GOOD.
Part: FLASHLIGHT — MALFUNCTIONED (CABIN) · airframe 94,600 hrs · 15,205 cycles
FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT NR 8 JUMPSEAT REMAINS ON. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-64-00. OPERATIONAL CHECKED GOOD.
Part: BATTERY — DISCHARGED (MEGAPHONE) · airframe 94,212 hrs · 15,121 cycles
THE AIRCRAFT WAS NOT GROUNDED. FRONT MEGAPHONE DOES NOT WORK FWD GALLEY. REPLACED BATTERY IN MEGAPHONE IAW MM 25-63-02 OPS CHECKS GOOD.
Part: WIRE — FAULTY (MICROPHONE) · airframe 94,136 hrs · 15,105 cycles
AFTER TAKEOFF, CREW REPORTED BOTH HIGH FREQUENCY RADIOS FAILED TO TRANSMIT, RECEPTION GOOD. REMOVED AND REPLACED CAPTAIN`S HAND MICROPHONE CABLE IAW AMM 23-11-00. OPERATIONAL CHECKED GOOD. AIRCRAFT WAS GROUNDED.
Part: LENS — DETACHED (EXIT SIGN) · airframe 93,550 hrs · 15,001 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT SIGN OVER L1 DOOR HAS A DETACHED LENS COVER. SECURED LENS COVER IAW AMM 33-51-01. OPERATIONAL CHECK GOOD.
Part: LIGHT — DIM (COCKPIT) · airframe 93,420 hrs · 14,963 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY EXIT LIGHT IN THE COCKPIT IS DIM. REMOVED AND REPLACED LIGHT IAW AMM 33-51-00-201. OPERATIONAL CHECK GOOD.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT IN BASE MAINTENANCE. CORROSION ON AFT CARGO COMPARTMENT FLOOR BETWEEN STATION 1065(BULKHEAD) TO STATION 1090 AND STRINGER 36L TO STRINGER 38L (KEELBEAM). REPAIRED FUSELAGE SKIN PER SRM 53-00-01-2R-12 AND EA 266369.
Part: WIRE — BROKEN (CABIN) · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT IN BASE MAINTENANCE. GALLEY 3 EMERGENCY LIGHT WITH RED MARKING-INOPERABLE. RESPLICED WIRE PER WDM 33-51-15 AND SWPM 20-10-13. PERFORMED EMERGENCY LIGHT TEST PER AMM 33-51-00. CHECKED GOOD.
Part: BATTERY — DISCHARGED (CABIN) · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT IN BASE MAINTENANCE. NEED TO REPLACE EMERGENCY LIGHT BATTERY M739. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M739 PER AMM 33-51-07. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: BATTERY — DISCHARGED (CABIN) · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT IN BASE MAINTENANCE. NEED TO REPLACE EMERGENCY LIGHT BATTERY M735. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M735 PER AMM 33-51-07. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: BATTERY — DISCHARGED (CABIN) · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT IN BASE MAINTENANCE. NEED TO REPLACE EMERGENCY LIGHT BATTERY M737. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M737 PER AMM 33-51-07. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: BATTERY — DISCHARGED (CABIN) · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT IN BASE MAINTENANCE. NEED TO REPLACE EMERGENCY LIGHT BATTERY M731. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M731 PER AMM 33-51-07. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: BATTERY — DISCHARGED (CABIN) · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT IN BASE MAINTENANCE. NEED TO REPLACE EMERGENCY LIGHT BATTERY M733, REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M733 PER AMM 33-51-07 ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: BATTERY — DISCHARGED (CABIN) · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT IN BASE MAINTENANCE. NEED TO REPLACE EMERGENCY LIGHT BATTERY M734, REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M734 PER AMM 33-51-07. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: BATTERY — DISCHARGED (CABIN) · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT IN BASE MAINTENANCE. NEED TO REPLACE EMERGENCY LIGHT BATTERY M738, REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M738 PER AMM 33-51-07. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: BATTERY — DISCHARGED (CABIN) · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT IN BASE MAINTENANCE. NEED TO REPLACE EMERGENCY LIGHT BATTERY M730. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M730 PER AMM 33-51-07. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: BATTERY — DISCHARGED (CABIN) · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT IN BASE MAINTENANCE. NEED TO REPLACE EMERGENCY LIGHT BATTERY M1208., REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M1208 IAW MM 33-51-07. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: BATTERY — DISCHARGED (CABIN) · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT IN BASE MAINTENANCE. NEED TO REPLACE EMERGENCY LIGHT BATTERY M736. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M736 PER AMM 33-51-07. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: BATTERY — DISCHARGED (CABIN) · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT IN BASE MAINTENANCE. NEED TO REPLACE EMERGENCY LIGHT BATTERY M962. REMOVED AND REPLACED EMERGENCY LIGHT BATTERY M962 PER AMM 33-51-07. ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT IN BASE MAINTENANCE. MID CABIN FLOORBEAM HAS CORROSION NEAR SEAT TRACK AT STATION 764 BETWEEN LBL 31 TO 61. REPAIRED FLOOR FRAME PER SRM 53-0051-2R-4 FIG 201.
Part: FLOORBEAM — CORRODED (BS 1197) · corrosion level 2 · airframe 93,417 hrs · 14,962 cycles
CORROSION ON AFT CARGO BAY FLOORBEAM AT BS 1197 AND RBL 40. REPAIRED FLOORBEAM IAW SRM 53-00-07, 51-40-02, 51-20-01, AND DWG 146T1206.
Part: FLOOR SUPPORT — CORRODED (BS 1197) · corrosion level 2 · airframe 93,417 hrs · 14,962 cycles
AFT CARGO BAY FLOOR SUPPORT AT BS 1197 +66 INCHES IS CORRODED AT LBL 30. REPAIRED SUPPORT IAW SRM 53-00-07-2R-4, FIGURE 201.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. AFT CARGO COMPARTMENT FLOORBEAM AT FUSELAGE STATION 1219 IS CORRODED AT LBL 6.5. REPAIRED FLOORBEAM IAW SRM 53-00-07-2R-4 FIGURE 201.
Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. CABIN FLOOR SUPPORT AT FUSELAGE STATION 246 IS CRACKED FROM FASTENER HOLE AT RBL 43. REMOVED, FABRICATED & INSTALLED SUPPORT CHANNEL IAW SRM 51-40-02.
2016
Part: STRAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 93,417 hrs · 14,962 cycles
AIRCRAFT WAS IN BASE MAINTENANCE. CABIN FLOOR BEAM RADIUS STRAP AT FUSELAGE STATION 1131 IS CORRODED AT LBL 40. REMOVED AND REPLACED STRAP IAW SRM 51-40-02 AND DRAWING 146T1203.
2015
Part: POWERPACK — DISCHARGED (CABIN) · airframe 93,124 hrs · 14,905 cycles
RIGHT EMER EXIT SIGNS, BY SEATS 19H - 20H, INOPERATIVE. R & R EMER LIGHT POWER PACK IAW AMM 33-51-00. OPERATIONAL CHECKED NORMAL.
Part: PRESSURE SWITCH — FAULTY (FUEL SYSTEM) · airframe 92,386 hrs · 14,791 cycles
AIR INTERRUPT, EMER DECLARED, LANDING UNEVENTFUL & ACFT OVERWEIGHT. DURING CLIMB RECEIVED A RT ENG FUEL FILTER EICAS MSG. R & R RT FUEL FILTER, REMOVED FILTER INSPECTED WITH NIL DEBRIS FOUND. R & R FUEL PRESS SWITCH. PERFORMED LEAK & OPERATIONAL CHECKS IAW AMM 73-34-01. SYS CHECKED NORMAL.
Part: CONDENSER — FAULTY (AC BAY) · airframe 90,970 hrs · 14,559 cycles
AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB CABIN TEMP WAS UNCONTROLLABLE WITH MID CABIN TEMP EICAS MSG. R & R LT AIR CONDITIONING CONDENSER IAW AMM 21-51-10. SYS CHECKED NORMAL. SEE ALSO AALA20150416003 & AALA20150421005.
Part: ACM — FAILED (RIGHT) · airframe 90,970 hrs · 14,559 cycles
DURING CLIMB CABIN TEMP WAS UNCONTROLLABLE WITH MID CABIN TEMP EICAS MESSAGE. RETURNED TO DEPARTURE, EMERGENCY DECLARED, AND LANDED UNEVENTFUL. REMOVED AND REPLACED RIGHT AIR CYCLE MACHINE IAW AMM 21-51-03. SYSTEM CHECKED NORMAL.
Part: CONDENSER — FAULTY (AC BAY) · airframe 90,970 hrs · 14,559 cycles
AIR INTERRUPT, RETURNED & EMER DECLARED. LANDING UNEVENTFUL & ACFT WAS OVERWEIGHT. DURING CLIMB CABIN TEMP WAS UNCONTROLLABLE WITH MID CABIN TEMP EICAS MG. R & R RT AIR CONDITIONING CONDENSER IAW AMM 21-51-10. SYS CHECKED NORMAL. SEE ALSO AALA20150416003 & AALA20150421004.
Part: SKIN — CRACKED (FUSELAGE) · corrosion level 2 · airframe 90,450 hrs · 14,459 cycles
FUSELAGE SKIN CORRODED AT STATION 1210 & STRINGER 39R. INSTALLED EXTERNAL DOUBLER & TRIPLER REPAIR IAW GUIDELINES OF SRM 53-00-01-2R. REPAIR 1 & EA 53-038662 DATED 02/19/2015.
2014
Part: LENS — CRACKED (EXIT SIGN) · airframe 88,717 hrs · 14,169 cycles
LEFT NR 1 DOOR EMER EXIT SIGN LOWER LIGHT LENS CRACKED. REPLACED LOWER LIGHT LENS FOR EMER EXIT SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 88,259 hrs · 14,104 cycles
RIGHT WING EXTERIOR EMER OVERWING ESCAPE PATH LIGHT INOPERATIVE. REPLACED LAMPED FOR RT WING EXTERIOR EMER OVERWING ESCAPE PATH LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 88,259 hrs · 14,104 cycles
LEFT WING EXTERIOR EMER OVERWING ESCAPE PATH LIGHT INOPERATIVE. REPLACED LAMP FOR LT WING EXTERIOR EMER OVERWING ESCAPE PATH LIGHT. OPERATIONS CHECKED NORMAL.
Part: PORTABLE LIGHT — DISCHARGED (CABIN) · airframe 87,767 hrs · 14,022 cycles
FLIGHT DECK PORTABLE EMER LIGHT DID NOT TEST. REPLACED FLIGHT DECK PORTABLE EMER LIGHT. OPERATIONS CHECKED NORMAL.
Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 87,767 hrs · 14,022 cycles
EMERGENCY AISLE LIGHTS AT SEAT 21H INOPERATIVE. REPLACED ESCAPE PATH LIGHT HARNESS FOR SEAT 21H. OPERATIONS CHECKED NORMAL.
Part: WIRE HARNESS — DAMAGED (CABIN) · airframe 87,767 hrs · 14,022 cycles
EMERGENCY AISLE LIGHTS AT SEAT 20H INOPERATIVE. REPLACED ESCAPE PATH LIGHT HARNESS & CONNECTOR AT SEAT 20H. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 87,618 hrs · 13,991 cycles
LOWER PORTION OF LT NR 1 DOOR INTERIOR EXIT MARKER SIGN INOPERATIVE. REPLACED LAMP FOR DOOR HANDLE ILLUMINATING LIGHTS AT LT NR 1 DOOR EXIT MARKER SIGN. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,618 hrs · 13,991 cycles
EMERGENCY LIGHT FWD OF SEAT 20G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT FWD OF SEAT 20G, OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,618 hrs · 13,991 cycles
EMERGENCY LIGHT AT SEAT 28H INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT SEAT 28H, OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,618 hrs · 13,991 cycles
LEFT NR 4 DOORWAY EMERGENCY LIGHT, L334, INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOORWAY EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.
Part: LENS — BROKEN (EMERGENCY LIGHT) · airframe 87,136 hrs · 13,918 cycles
L1 DOOR EMERGENCY LIGHT LENS IS BROKEN. REPLACED LENS FOR LT NR 1 DOOR EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,136 hrs · 13,918 cycles
SEAT 21H EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 21H EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,136 hrs · 13,918 cycles
SEAT 20H EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 20H EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 86,743 hrs · 13,847 cycles
LT NR 1 ENTRY DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 1 ENTRY DOOR EXTERIOR EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.
Part: STRUCTURE — DAMAGED (LT WING) · airframe 86,600 hrs · 13,825 cycles
UPON REMOVAL OF LT HAND AFT PITCH LOAD BACK UP FITTING HI-LOCKS, FOUND UPPER AFT HOLE IN RIB NR 10 UPPER CHORD DAMAGED. REWORKED HOLE & INSTALLED FASTENER IAW ECO C3368AR & EA B767-57-033491.
2013
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 85,828 hrs · 13,701 cycles
INTERIOR LT FWD OVERWING LOWER EXIT MARKER 1 SEGMENT INOPERATIVE. REPLACED LAMP FOR EXIT SIGN FWD OF SEAT 20A. OPS CHECK NORMAL
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 85,828 hrs · 13,701 cycles
FOWARD OF SEAT 20G LOWER BULKHEAD EXIT SIGN LIGHT SEGMENT INOPERATIVE. REPLACED LAMP FOR EXIT SIGN FOWARD OF SEAT 20G. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 85,828 hrs · 13,701 cycles
LT NR 1 DOOR EMERGENCY EXIT SIGN HANDLE ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 1 DOOR EMERGENCY EXIT SIGN HANDLE ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 85,828 hrs · 13,701 cycles
AFT GALLEY BULKHEAD DIVIDER LT SIDE LOWER EXIT SIGN SEGMENTS INOPERATIVE. REPLACED LAMP FOR EXIT SIGN. OPERATIONS CHECKED NORMAL. OPS CHECK NORMAL
Part: LIGHT — INOPERATIVE (CABIN) · airframe 85,828 hrs · 13,701 cycles
RT NR 1 DOOR FRAME MOUNTED EXIT ILLUMINATION LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOOR FRAME MOUNTED EXIT ILLUMINATION LIGHT. OPERATIONS CHECKED NORMAL.
Part: BRAKE — MALFUNCTIONED (MLG) · airframe 83,424 hrs · 13,277 cycles
JFK - CREW REPORTED SLIGHT BRAKE DRAG WITH EICAS ANTI-SKID MESSAGE. EMERGENCY DECLARED FLIGHT LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED NUMBER THREE AND FOUR BRAKES. SYSTEM GROUND CHECK NORMAL OPERATION.
2012
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 83,191 hrs · 13,238 cycles
RIGHT WING INBOARD END JUST FORWARD OF AFT SPAR HAS CORROSION. REWORKED CORROSION AND INSTALLED SECOND OVER FASTENERS AS PER EA B767-57-0273449.
Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 83,191 hrs · 13,238 cycles
INTERCOSTAL FROM STATIONS 1351 TO 1373 AT STRINGER 27 RIGHT DAMAGED. REPLACED INTERCOSTAL PER AARD 51-10-05-01.
Part: MOUNT — LOOSE (EMERGENCY LIGHTS) · airframe 82,138 hrs · 13,067 cycles
LIGHT NUMBER 1 DOOR EMERGENCY EXIT LIGHT MOUNT LOOSE. SECURED LEFT NUMBER 1 DOOR EMERGENCY EXIT LIGHT MOUNT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,138 hrs · 13,067 cycles
RIGHT NUMBER 2 DOOR EMERGENCY EXIT HANDLE SPOTLIGHTS INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EMERGENCY EXIT HANDLE SPOTLIGHTS. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,138 hrs · 13,067 cycles
RIGHT NUMBER 2 DOOR SLIDE LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR SLIDE LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,138 hrs · 13,067 cycles
SEAT MOUNTED EMERGENCY LIGHT AT 39H INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT 39H. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 82,138 hrs · 13,067 cycles
SEAT MOUNTED EMERGENCY LIGHT AT 29H INOPERATIVE. REPLACED LAMP FOR SEAT MOUNTED EMERGENCY LIGHT AT 29H. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,568 hrs · 12,987 cycles
LEFT NUMBER 2 DOOR UPPER EMERGENCY LIGHT LOWER LAMPS INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER UPPER EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 81,568 hrs · 12,987 cycles
RIGHT NUMBER 2 DOOR UPPER EMERGENCY SIGN LOWER LAMPS INOPERATIVE. REPLACED LAMPS FOR RIGHT NUMBER 2 DOOR UPPER EMERGENCY SIGN. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,568 hrs · 12,987 cycles
OVERHEAD AISLE EMERGENCY LIGHT AT 37B INOPERATIVE. REPLACED LAMP FOR OVERHEAD AISLE EMERGENCY LIGHT AT SEAT 37B. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 81,568 hrs · 12,987 cycles
RIGHT NUMBER 1 DOOR UPPER EMERGENCY SIGN LOWER LAMPS INOPERATIVE. REPLACED LAMPS FOR RIGHT NUMBER 1 DOOR UPPER EMERGENCY SIGN. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,568 hrs · 12,987 cycles
SEAT 33B EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 33B EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,568 hrs · 12,987 cycles
LOWER AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LOWER AFT EMERGENCY LIGHT. OPS CHECKS NORMAL.
Part: CONNECTOR — LOOSE (CABIN) · airframe 81,568 hrs · 12,987 cycles
SEAT 29H EMERGENCY LIGHT INOPERATIVE. RESECURED UNDERSEAT CONNECTOR AT SEAT 29H THAT WAS LOOSE.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 81,568 hrs · 12,987 cycles
LEFT NUMBER 1 DOOR UPPER EMERGENCY LIGHT LOWER LAMPS INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 DOOR UPPER EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LENS — UNSECURE (CABIN) · airframe 81,568 hrs · 12,987 cycles
LEFT AFT UPPER EMERGENCY EXIT LIGHT LENS FORWARD OF LAVATORY ON BULKHEAD PARTITION UNSECURE. RE-SECURED LEFT AFT UPPER EMERGENCY EXIT LIGHT LENS. OPS CHECK NORMAL.
2011
Part: WEB — CRACKED (PYLON) · airframe 77,908 hrs · 12,394 cycles
LEFT PYLON STRUT TORQUE BOX FORWARD UPPER WEB POWER FEEDER CUTOUT CRACKED. INSTALLED AN INTERNAL DOUBLER WITH SOME HARDWARE/MOUNTING BRACKET CHANGES FOR THE POWER FEEDER CABLES PER MAJOR EA B767-54-017977.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 75,948 hrs · 12,072 cycles
EMERGENCY LIGHT IN CEILING ON LEFT SIDE AISLE ABOVE ROW 43 IS INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT IN CEILING ON LEFT SIDE AISLE ABOVE ROW 43. OPS CHECK NORMAL.
2010
Part: COVER — MISSING (CABIN) · airframe 75,732 hrs · 12,031 cycles
PASSENGER EXIT SIGN AT RIGHT AFT WING EXIT DOOR MISSING COVER. REPLACED RIGHT AFT OVERWING EXIT SIGN COVER. OPS CHECK NORMAL.
Part: TAT PROBE — FAULTY (ZONE 200) · airframe 75,625 hrs · 12,013 cycles
MIA - CREW REPORTED DURING CLIMB TOTAL AIR TEMPERATURE PROBE EICAS AND OTHER ASSOCIATED FAILURE MESSAGES. FLIGHT RETURNED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED TAT PROBE. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: TRANSMITTER — FAULTED (LE SLAT) · airframe 74,389 hrs · 11,795 cycles
MIA - INFLIGHT JFK-PAP. CREW REPORTED FLAP/SLAT ELECTRONIC EICAS MESSAGE IN FLIGHT. FLIGHT DIVERTED MIA LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. BITE OF FLAP SLAT ELECTRONIC UNIT FAULTED OUTBOARD SLAT NUMBER 2 TRANSMITTER. REPLACED TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: SKIN PANEL — DAMAGED (RT WING) · airframe 73,924 hrs · 11,705 cycles
DAMAGE TO RIGHT WING LOWER SKIN TRAILING EDGE PANEL. REPLACED PANEL NUMBER 112T4601-2 PER SRM 51-40-05 AND EA B767-57-010871.
Part: FSEU — FAULTY (WING) · airframe 73,096 hrs · 11,566 cycles
DFW - CAPTAIN REPORTED FLAP DISAGREE MESSAGE ON DESCENT. EMERGENCY DECLARED LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED FLAP SLAT ELECTRONIC UNIT. FLAPS OPERATED NORMAL NO FAULTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
2009
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,772 hrs · 11,506 cycles
FLOORBEAM AT STATION 325 HAS CORROSION REMOVAL ON HORIZONTAL FLANGE. REPAIRED UNDER ENGINEERING AUTHORITY B767 008461.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,772 hrs · 11,506 cycles
FLOORBEAM AT STATION 347 HAS CORROSION REMOVAL ON HORIZONTAL FLANGE. REPAIRED UNDER ENGINEERING AUTHORITY B767 008460.
Part: INDICATOR — TRIPPED (COCKPIT) · airframe 72,731 hrs · 11,500 cycles
WHILE CONFIGURING FLAP FOR LANDING FROM 5 DEGREES TO 20 DEGREES RECEIVED TRAILING EDGE FLAP DISAGREE EICAS STATUS. WENT AROUND AND FOLLOWED QRH AFTER DECLARING AN EMERGENCY. UPON COMPLETION OF QRH, RETURNED FOR FLAPS 20 DEGREE LANDING. NO OTHER ISSUES WITH FLIGHT CONTROLS. FOUND FLAP OVERLOAD INDICATOR TRIPPED. RESET INDICATOR.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 70,555 hrs
SFO SEAT 2H EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY FOR SEAT 2H.
Part: LENS — MISSING (CABIN) · airframe 70,555 hrs
SFO - SEAT 12B EMERGENCY LIGHT LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 12B.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 70,555 hrs
SFO - RIGHT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT EMERGENCY EXIT LIGHT.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,110 hrs · 11,052 cycles
AFW - FUSELAGE SKIN AND TEAR STRAP AT STATION 1219 AND STRINGER 37 LEFT HAD CORROSION. SKIN CUT OUT MEASURES 5.3 INCH FORWARD/AFT BY 4.5 INCH INBOARD/OUTBOARD. PERFORM HIGH FREQUENCY EDDY CURRENT INSPECTION. INSTALLED SPLICE IN ACCORDANCE WITH MRB 767-3408.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 70,110 hrs · 11,052 cycles
AFW - FUSELAGE STRINGER 34 LEFT AT STATION 1219 HAD CORROSION. FABRICATED AND INSTALLED REPAIR SPLICE IN ACCORDANCE WITH MRB 767-3407.
2008
Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS) · 67,739 cycles
MIA EXTERIOR EMERGENCY LIGHTS AT LOWER FORWARD AND AFT OVERWING EMERGENCY EXIT DOOR. REPLACED BATTERY PACK FOR EXTERIOR EMERGENCY LIGHTS AT LOWER FORWARD AND AFT OVERWING EMERGENCY EXIT DOOR. SYSTEM GROUND CHECKED NORMAL OPS.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHTS) · airframe 65,893 hrs
SFO - EMERGENCY LIGHT AT OVERHEAD FORWARD GALLEY RIGHT SIDE INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD FORWARD GALLEY RIGHT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE — DAMAGED (EMERGENCY LIGHTS) · airframe 65,893 hrs
SFO - EMERGENCY LIGHTS AT SEATS 17EH INOPERATIVE. REPAIRED WIRING FOR EMERGENCY LIGHTS AT SEATS 17EH. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: BULB — INOPERATIVE (EMERGENCY LIGHTS)
ORD - EMERGENCY LIGHT AT OVERHEAD SEAT 24G INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — INOPERATIVE (ESCAPE SLIDE)
JFK - DURING SQUIB TEST LEFT WING SLIDE SQUIB INOPERATIVE. RESEATED CONNECTOR TO BATTERY PACK FOR LEFT WING SLIDE SQUIB. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: LENS — MISSING (CABIN)
DFW - CEILING EMERGENCY LIGHTS AT FORWARD GALLEY LEFT SIDE MISSING LENS. REPLACED LENS FOR CEILING EMERGENCY LIGHTS AT FORWARD GALLEY LEFT SIDE. SYSTEM GROUND CHECKED NORMAL OPERATION.
2005
Part: CONNECTOR — INOPERATIVE (CABIN)
DFW - EMERGENCY LIGHT AT SEAT 40AB INOPERATIVE. RESEATED CONNECTOR AT INSIDE WALL CONNECTION FOR EMERGENCY LIGHT AT SEAT 40AB. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: CONNECTOR — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, FOUND SEAT MOUNTED EMERGENCY LIGHT AT SEAT 32H INOPERATIVE. REPLACED CONNECTOR FOR SEAT 32H MOUNTED EMERGENCY LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — LOOSE (EMERGENCY LIGHT)
OVERNIGHT MAINTENANCE OBSERVED EMERGENCY LIGHT INOPERATIVE AT SEAT 24B. CONNECTED ELECTRICAL WIRE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, RIGHT MID GALLEY EMERGENCY DIRECTIONAL FLOODLIGHT NEXT TO FLIGHT ATTENDANT INOPERATIVE. REPLACED RIGHT MID GALLEY EMERGENCY DIRECTIONAL FLOOD LIGHT NEXT TO FLIGHT ATTENDANT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: GENERATOR — INOPERATIVE (RIGHT GENERATOR)
GENERATOR , POSN RIGHT GENERATOR. ENGINE DRIVEN GENERATOR SYSTEMS, INOPERATIVE. DELTA P TRIP AND HIGH OIL TEMPERATURE.
Part: SMOKE — DETECTED (COCKPIT)
ENROUTE, EXPERIENCED STRONG ELECTRICAL SMELL WITH HAZE IN CABIN, COCKPIT AND AT OVERWING EMERGENCY EXIT. EMERGENCY DECLARED. LANDED WITHOUT INCIDENT. PERFORMED CHECK OF ELECTRICAL SYSTEM. RAN PACKS AT FULL POWER. UNABLE TO DUPLICATE PROBLEM. SYSTEM GROUND CHECKED NORMAL OPERATION.
2001
Part: WIRE — BROKEN (CABIN)
ORD - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 35B INOPERATIVE. REPAIRED EMERGENCY EXIT LIGHT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: ODOR — DETECTED (CABIN)
FLT 111 - FCO - LEFT BUSINESS CLASS LAV HAS A STRONG ODOR EITHER PETROLEUM BASED OR DETERGENT BASED. LEFT BUS CLASS LAV CLEARED AND SERVICED BY CBN SERVICE. NO FUEL SMELL DETECTABLE INFOR NOTED A/C OK FOR SERVICE. (M)
Part: WIRE — LOOSE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY LIGHT INOPERATIVE SEAT 37H. REPAIRED LOOSE WIRE TO WALL/SEAT CONNECTOR FOR SEAT 37H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: LIGHT — DISCONNECTED (EXIT DOOR)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT AFT EXIT DOOR INOPERATIVE. RE-CONNECTED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — DAMAGED (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, SEAT MOUNTED EMERGENCY EXIT AT 21H INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE AT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: LIGHT — INOPERATIVE (COCKPIT)
LAX - DURING OVERNIGHT MAINTENANCE, COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED COCKPIT EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: INVERTER — DEFECTIVE (ELECTRICAL RACK)
JFK - FLT 131 - DURING FLIGHT, CREW REPORTED SMOKE IN COCKPIT. DIVERTED AND LANDED YYR WITHOUT INCIDENT. REPLACED STATIC INVERTER AND FORWARD EQUIPMENT FAN AS A PRECAUTION. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: CONNECTOR — DISCONNECTED (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 9AB INOPERATIVE. RECONNECTED EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 9AB CONNECTOR. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: LIGHT — BROKEN (CABIN)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT PATH LIGHT BEHIND SECOND CLASS GALLEY BROKEN. REPLACED EMERGENCY EXIT PATH LIGHT STRIP BEHIND SECOND CLASS GALLEY. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (ROW 23B)
SFO - DURING OVERNIGHT MAINTENANCE, SEAT 23B EMERGENCY EXIT SEAT PATH LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT SEAT LIGHT ASSEMBLY AT SEAT 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: VIDEO UNIT — DEFECTIVE (CABIN)
MAN - FLT 0054 - EN ROUTE SEAT 3A AND 3B PERSONAL VIDEO UNITS HAD REPORT OF SMOKING. LANDED MAN WITHOUT INCIDENT. REPLACED PERSONAL VIDEO UNIT AT 3A. ROCKWELL COLLINS PERFORMED VOTLAGE TEST TO POWER SUPPLY OF PERSONAL VIDEO UNIT AND AT INPUT. VOLTAGES ARE ALL PROPER. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO NOTICE OF SMOKE. (X)
1998
Part: FLOORBEAM — CORRODED (BS 347)
AFW - FLOORBEAM AT STATION 347 RBL 46 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLENDED OUT ALL CORROSION. ALODINED ALL BARE ALUMINUM SURFACES, APPLIED TWO COATS OF BMS 10-11 PRIMER AND FILLED BLENDS WITH BMS 5-92 PER SRM. (M)
Part: FLOORBEAM — GOUGED (BS 938)
AFW - FLOORBEAM AT STATION 938 LBL 33.06 HAD GOUGE BLENDED BEYOND SRM LIMITS. BLENDED OUT GOUGE. ROTO/FLAP PEENED BLENDED AREA. ALODINED AREA. APPLIED TWO COATS OF BMS 10-11 PRIMER AND FILLED BLENDED AREA WITH BMS 5-92 PER SRM. (M)
Part: FLOORBEAM — CORRODED (BS 347)
AFW - FLOORBEAM AT STATION 347 RBL 82 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLENDED OUT ALL CORROSION. ALODINED ALL BARE ALUMINUM SURFACES, FINISHED BLENDED AREAS WITH TWO COATS OF BMS 10-11. PRIMED AND FILLED BLENDS WITH BMS 5092 PER SRM 53-00-51 FIG 101. (M)
Part: FLOORBEAM — CORRODED (BS 1480)
AFW - FLOORBEAM AT STATION 1480 LBL 50 AND 60 HAD CORROSION BLENDED BEYOND SRM LIMITS. BLENDED OUT CORROSION. ALODINED ALL BARE ALUMINUM SURFACES. APPLIED TWO COATS OF BMS 10-11 PRIMER AND FILLED BLENDS WITH BMS 5-92 PER SRM. (M)
Part: HARNESS — FAILED (RT EGT)
JFK - FLT 956 - RIGHT EGT WENT TO ZERO ONE HOUR INTO FLIGHT CAME BACK ON ABOUT 6 HOURS INTO FLIGHT OPERATION INTERMITTENT FOR REMAINDER OF FLT. CHECKED WIRING FROM RT ENGINE 'J' BOX TO FIRE WALL CONNECTOR AND WIRING CHECKED GOOD. REPLACED RT ENGINE LOWER EGT HARNESS PER MM RAN RT ENGINE AND EGT WAS NORMAL OK FOR SERVICE. (M)
Part: LIGHT — BROKEN (FWD GALLEY)
LHR - DURING MAINTENANCE, FORWARD GALLEY RIGHT ESCAPE PATH LIGHT BROKEN. REPLACED LAMP HOLDER AND EMERGENCY LIGHT COVER ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: CONNECTOR — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 17B INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 17B. SYTEM GROND CHECKED NORMAL OPERATION. (M)
1996
Part: WIRE — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 32H INOPERATIVE. REPAIRED BROKEN EMERGENCY EXIT LIGHT WIRE AT PAX SEAT 32H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PASSENGER SEAT 28B INOPERATIVE. RESECURED LOOSE EMERGENCY EXIT LIGHT CONNECTOR AT PASSENGER SEAT 28B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)