N395AN
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.
104 reports on file, 2000-01-06 – 2020-12-02.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 82,348 hrs · 13,221 cycles
FUSELAGE SKIN, STA 1347, 1.5" ABOVE STR-29R AND STR-30R, EXISTING BLEND OUTS (2 EA). SHOP FOUND EXISTING BLENDOUT IN FUSELAGE EXTERNAL SKIN THAT IS NOT PERMITTED IN ACCORDANCE WITH SRM 53-00-01, FIG 101, DETAIL II. PERFORMED NDT INSPECTION, ONE, ORIGINAL THICKNESS SKIN 0.205" AND NOMINAL 0.202" FOR NRC M0627. TWO, ORIGINAL THICKNESS SKIN 0.205" AND NOMINAL 0.202" FOR NRC M0628.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 82,348 hrs · 13,221 cycles
FUSELAGE SKIN STA 448-STA 455, STR 27R, DURING MAITENANCE FOUND EXISTING BLEND OUT AT FUSELAGE SKIN (SECTION 43) FROM STATION 448 TO STATION 455, STRINGER 27R. THE REWORK IS RESTRICTED, PER B767-300 SRM 53-00-01 ALLOWABLE DAMAGE 1 DETAIL II SEVERAL FASTENERS ARE LOCATED IN AFFECTED AREA AND THE BLEND OUT IS CLOSE TO THE LAVATORY SERVICE PANEL & PRESSURE PAN WHICH FALLS UNDER SRM 53-00-01 ALLOWABLE DAMAGE 1, DETAIL XII. AN ULTRASONIC THICKNESS (UT) INSPECTION WAS ACCOMPLISHED USING 0.5" GRIDS AND FOUND THE NOMINAL THICKNESS TO BE BETWEEN 0.112" 0.094" WITH A MINIMUM REMAINING THICKNESS BETWEEN 0.110"-0.092" (0.02", 2.1% REMOVED).
Part: SKIN — SCRATCHED (FUSELAGE) · airframe 82,348 hrs · 13,221 cycles
FUSELAGE SKIN, STA 1417 STA 1461; STR 33L-STR 34L. DURING THE MAINTENANCE INSPECTION AT IAI, MULTIPLE SCRATCHES BLENDED OUT ON EXTERNAL FUSELAGE SKIN BETWEEN STA 1417 STA 1461, STR 33L STR 34L WAS FOUND. THE BLEND OUTS WERE MEASURED AND IT WAS FOUND THAT THE MINIMUM SKIN THICKNESS WAS 0.181" WHILE THE NOMINAL SKIN THICKNESS WAS MEASURED AS BEING 0.190". HOWEVER, SEVERAL FASTENERS ARE LOCATED IN AFFECTED AREA, WHILE IT IS RESTRICTED PER SRM 53-00-01, ALLOWABLE DAMAGE 1, DETAIL II.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 82,348 hrs · 13,221 cycles
DURING MAINTENANCE INSPECTION AT IAI, AN EXISTING BLEND OUT WAS FOUND ON FUSELAGE EXTERNAL SKIN AT STA 372, STR 32R. A FASTENER IS LOCATED IN THE AFFECTED AREA WHILE IT IS RESTRICTED, PER SRM 53-00-01 ALLOWABLE DAMAGE 1. THE BLEND OUT WAS MEASURED AND FOUND THAT THE NOMINAL THICKNESS IS 0.067" WITH A MINIMUM REMAINING THICKNESS OF 0.064".
Part: SKIN — DAMAGED (FUSELAGE) · airframe 82,348 hrs · 13,221 cycles
UPPER FUSELAGE, STA 1197+66 TO STA 1197+132, STR 2L-STR 2R. DURING CONVERSION PROCESS, THE GLOBAL COMMUNICATION SUITE (G.C.S) ANTENNA WAS REQUESTED TO BE DEACTIVATED AND REMOVED FROM THE AIRCRAFT PER CUSTOMER REQUEST, PRODUCTION ORDER NR 11. THE SKIN UNDERNEATH ANTENNA REQUIRES REPAIR DUE TO COAX CABLE PIERCE POINTS.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 82,348 hrs · 13,221 cycles
FUSELAGE SKIN, STA 1043, STR 2L-STR 2R. DURING CONVERSION WORK, THE SATCOM ANTENNA HAS BEEN DEACTIVATED AND REMOVED FROM THE AIRCRAFT, PER CUSTOMER REQUEST. BURNT OUT FUSELAGE SKIN HAS BEEN FOUND AFTER THE REMOVAL.
Earlier reports · 2000–2019 · 98 reports
2019
Part: ACCESS PANEL — DAMAGED (HYD SERVICE) · airframe 82,272 hrs · 13,208 cycles
AIRCRAFT WAS GROUNDED: UPON ARRIVAL AT MAN; THE HYDRAULIC SERVICE PANEL WAS FOUND TO BE MISSING. THE PANEL HINGES WERE SHEARED , SERVICING HOSE WAS FOUND LOOSE, THE RAT PANEL WAS FOUND TO BE CRACKED AND A MARK WAS NOTED ON THE RIGHT SIDE OF THE FUSELAGE. MAINTENANCE INSTALLED MISSING HYDRAULIC SERVICE PANEL (AALA201910239001), REPLACED DAMAGED RAT PANEL PER AMM 53-52-01 (AALA201911149017).
Part: ACCESS DOOR — MISSING (ZONE 100) · airframe 82,272 hrs · 13,208 cycles
AIRCRAFT WAS GROUNDED: UPON ARRIVAL AT MAN; THE HYDRAULIC SERVICE PANEL WAS FOUND TO BE MISSING. THE PANEL HINGES WERE SHEARED , SERVICING HOSE WAS FOUND LOOSE, THE RAT PANEL WAS FOUND TO BE CRACKED AND A MARK WAS NOTED ON THE RIGHT SIDE OF THE FUSELAGE. SUPPLEMENTAL REPORT: MAINTENANCE INSTALLED MISSING HYDRAULIC SERVICE PANEL (AALA201910239001), REPLACED DAMAGED RAT PANEL PER AMM 53-52-01 (AALA201911149017). (CLOSED)
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 81,240 hrs · 13,009 cycles
AIRCRAFT WAS NOT GROUNDED: FLIGHT ATTENDANT FLASHLIGHT, LEFT HAND SIDE MID CABIN BATTERY DISCHARGED. MAINTENANCE REPLACED BATTERY PER AMM 25-05-03.
Part: LENS — MISSING (CABIN) · airframe 81,240 hrs · 13,009 cycles
AIRCRAFT WAS NOT GROUNDED: 1R DOOR EMERGENCY EXIT LIGHT MISSING. MAINTENANCE REPLACED LIGHT LENS PER AMM 33-51-01.
Part: FLASHLIGHT — FAULTY (CABIN) · airframe 81,111 hrs · 12,989 cycles
AIRCRAFT WAS NOT GROUNDED: FLASHLIGHT AT FLIGHT ATTENDANT POSITION, 3L, RED LIGHT INDICATED LOW BATTERY. MAINTENANCE REPLACED 3L FLASHLIGHT PER MM 25-64-00.
Part: PORTABLE LIGHT — INOPERATIVE (COCKPIT) · airframe 80,634 hrs · 12,892 cycles
AIRCRAFT IN BASE MAINTENANCE: COCKPIT PORTABLE EMERGENCY LIGHT INOPERABLE. REPLACED EMERGENCY LIGHT ASSEMBLY PER AMM 33-51-00.
Part: BATTERY — DISCHARGED (CABIN) · airframe 80,612 hrs · 12,886 cycles
AIRCRAFT IN BASE VISIT: MAINTENANCE FOUND SEAT ROW 20HJ AND 21HJ EMERGENCY LIGHT (2X) INOP. REMOVED AND REPLACED BATTERY FOR SEAT ROW 20HJ / 21HJ AT M1209 STA871 RIGHT IAW AMM 33-51-07. OPS CHECKED NORMAL.
Part: BATTERY — DISCHARGED (CABIN) · airframe 80,612 hrs · 12,886 cycles
AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS SEAT ROW 21 HJ SIDE MARKER EMERGENCY LIGHTS 2 EA. INOP. MAINTENANCE REMOVED AND REPLACED BATTERY SUPPLY AT M1209 STA871 RIGHT IAW AMM 33-51-07. OPS CHECKED NORMAL.
Part: BATTERY — DISCHARGED (CABIN) · airframe 80,612 hrs · 12,886 cycles
AIRCRAFT WAS GROUNDED: MAINTENANCE REPORTS SEAT ROW 20 HJ SIDE MARKER EMERGENCY LIGHT 2 EA. INOP. REMOVED AND REPLACED BATTERY SUPPLY AT M1209 STA 871 RIGHT IAW MM 33-51-07 OPS CHECKED NORMAL.
Part: BATTERY — FAILED (FLASHLIGHT) · airframe 80,127 hrs · 12,777 cycles
MAINTENACNCE FOUND ONE EMERGENCY FLASHLIGHT BEHIND BUSINESS CLASS, BELOW THE F/A SEAT TO BE INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY. OPS TESTED GOOD.
2018
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 78,505 hrs · 12,443 cycles
MIA - THE AIRCRAFT WAS NOT GROUNDED. FLT ATTENDANT FLASHLIGHT INOP AT SEAT AFT BY ROW 17B. MAINTENANCE REPLACED FLASHLIGHT BATTERY FOR FLIGHT ATTENDANT AFT SEAT BY ROW 17B IAW AMM 25-25-03 OPS CK OK.
Part: CHARGER — INOPERATIVE (EMERGENCY LIGHTS) · airframe 78,340 hrs · 12,413 cycles
EMERGENCY LIGHTS AT SEAT 23B WERE INOPERATIVE. REPLACED THE BATTERY CHARGER.
Part: WIRE HARNESS — INOPERATIVE (EMERGENCY LIGHT) · airframe 78,340 hrs · 12,413 cycles
EMERGENCY LIGHTS AT SEAT 23B WERE INOPERATIVE. REPLACED THE WIRE HARNESS ON SEAT 23B.
Part: BATTERY — DISCHARGED (EMERGENCY LIGHTS) · airframe 78,340 hrs · 12,413 cycles
ROW 32 RIGHT, AFT FLOOR EMERGENCY LIGHTS AND AISLE ILLUMINATION LIGHTS FAILED A 15 MINUTE CHECK. REPLACED THE BATTERY IAW AMM 33-51-07. OPS CHECKED GOOD.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 78,014 hrs · 12,343 cycles
BOTH LEFT AND RIGHT OVERWING EXIT LIGHTS GO OFF, 20 - 30 SECONDS INTO TEST. ALL OTHER EMERGENCY LIGHTS ON. REPLACED THE BATTERY CHARGERS M737 AND M734 IAW AMM 33-51-07. REPLACED THE BATTERY PACKS. OPS CHECKED OK.
Part: BATTERY PACK — NO TEST (EMERGENCY LIGHTS) · airframe 78,014 hrs · 12,343 cycles
BOTH LEFT AND RIGHT OVERWING EXIT LIGHTS GO OFF, 20 - 30 SECONDS INTO TEST. ALL OTHER EMERGENCY LIGHTS ON. REPLACED THE BATTERY CHARGERS M737 AND M734 IAW AMM 33-51-07. REPLACED THE BATTERY PACKS.
Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 78,014 hrs · 12,343 cycles
BOTH LEFT AND RIGHT OVERWING EXIT LIGHTS GO OFF, 20 - 30 SECONDS INTO TEST. ALL OTHER EMERGENCY LIGHTS ON. REPLACED BATTERY CHARGERS M737 AND M734 IAW AMM 33-51-07. REPLACED THE BATTERY PACKS. OPS CHECKED OK.
Part: CHARGER — NO TEST (EMERGENCY LIGHTS) · airframe 78,014 hrs · 12,343 cycles
BOTH LEFT AND RIGHT OVERWING EXIT LIGHTS GO OFF 20 - 30 SECONDS INTO TEST. ALL OTHER EMERGENCY LIGHTS ON. REPLACED THE BATTERY CHARGERS M737 AND M734 IAW AMM 33-51-07. REPLACED THE BATTERY PACKS.
Part: FLASHLIGHT — INOPERATIVE (FWD GALLEY) · airframe 77,384 hrs · 12,228 cycles
FORWARD GALLEY FLIGHT ATTENDANT SEAT FLASHLIGHT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-25-03.
2017
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 75,840 hrs · 11,940 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT IN THE MID CABIN AFT LEFT JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY PER AMM 25-64-00. OPERATIONAL CHECK GOOD.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 75,721 hrs · 11,925 cycles
FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AT THE L1 JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED THE FLASHLIGHT BATTERY IAW CMM 25-25-01. OPS CHECKED GOOD.
Part: BATTERY — INOPERATIVE (FLASHLIGHT) · airframe 74,681 hrs · 11,745 cycles
FLIGHT ATTENDANT EMERGENCY FLASHLIGHT AFT GALLEY LEFT JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 33-14-00. OPERATIONAL CHECKED GOOD.
Part: WIRE — BROKEN (CABIN) · airframe 74,551 hrs · 11,722 cycles
AIRCRAFT WAS NOT GROUNDED. EMERGENCY ESCAPE PATH LIGHT AT SEAT 24B IS INOPERATIVE. INSTALLED NEW SPLICE ON BROKEN HARNESS WIRE IAW SWPM 20-30-12. OPERATIONAL CHECK GOOD.
Part: BATTERY — NO TEST (FLASHLIGHT) · airframe 74,483 hrs · 11,709 cycles
FLIGHT ATTENDANT EMERGENCY FLASHLIGHT MID GALLEY LEFT SIDE AFT JUMPSEAT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.
Part: FLASHLIGHT — NO TEST (CABIN) · airframe 74,483 hrs · 11,709 cycles
FLIGHT ATTENDANT F1 EMERGENCY FLASHLIGHT IS INOPERATIVE. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-64-00. OPERATIONAL CHECKED GOOD.
Part: BATTERY — DISCHARGED (FLASHLIGHT) · airframe 73,835 hrs · 11,611 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT MID GALLEY LEFT SIDE IS LOW. REMOVED AND REPLACED FLASHLIGHT BATTERY IAW AMM 25-63-00. OPERATIONAL CHECK GOOD.
Part: FLASHLIGHT — FAILED (CABIN) · airframe 73,645 hrs · 11,574 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT EMERGENCY FLASHLIGHT MID GALLEY LEFT SEAT FAILED TEST. REMOVED AND REPLACED FLASHLIGHT IAW AMM 25-64-00. OPERATIONAL CHECK GOOD.
Part: ATTACH ANGLE — CRACKED (BS 246) · airframe 73,505 hrs · 11,552 cycles
CRACKED PULLEY ATTACH ANGLE ON FORWARD SIDE OF FRAME BS 246, RBL 11. REPLACED THE ATTACH ANGLE PER SRM 53-10-51-2R-3 AND EA 267806.
Part: ATTACH ANGLE — CRACKED (BS 246) · airframe 73,505 hrs · 11,552 cycles
CRACKED PULLEY ATTACH ANGLE ON FORWARD SIDE OF FRAME BS 246, LBL 4. REPLACED THE ATTACH ANGLE IAW SRM 53-10-51-2R-3 AND EA 267806.
Part: ATTACH ANGLE — CRACKED (BS 246) · airframe 73,505 hrs · 11,552 cycles
CRACK ON PULLEY ATTACH ANGLE ON FORWARD SIDE OF FRAME AT BS 246, BL 0. REPLACED THE ATTACH ANGLE IAW SRM 53-10-51-2R3 AND EA 267806.
Part: ATTACH ANGLE — CRACKED (BS 246) · airframe 73,505 hrs · 11,552 cycles
CRACKED PULLEY ATTACH ANGLE ON FORWARD SIDE OF FRAME BS 246 AND RBL 6. REPLACED THE ATTACH ANGLE IAW SRM 53-10-51-2R-3 AND EA 267806.
Part: FLASHLIGHT — MISSING (CABIN) · airframe 73,265 hrs · 11,504 cycles
AIRCRAFT WAS NOT GROUNDED. FLIGHT ATTENDANT FLASHLIGHT LEFT MID GALLEY AFT SEAT IS MISSING. REPLACED FLASHLIGHT IAW AMM 25-05-03. OPERATIONAL CHECK GOOD.
Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 73,128 hrs · 11,476 cycles
AIRCRAFT NOT GROUNDED. SMOKE DETECTOR IN LAVATORY FS3 CHIMES CONTINUOUSLY. REMOVED AND REPLACED SMOKE DETECTOR IAW AMM 26-13-01. OPERATIONAL CHECK GOOD.
2016
Part: COMPRESSOR — STALLED (LT ENGINE) · airframe 73,026 hrs · 11,457 cycles
AIRCRAFT WAS GROUNDED. EMERGENCY DECLARED. DFW-MIA FLIGHT RETURNED TO DFW ACCOUNT LEFT ENGINE HAD TWO COMPRESSOR STALLS. NO ENGINE SHUTDOWN. LANDING UNEVENTFUL. ACCOMPLISHED FIM TASK 71-05-00, MCM CARD 4218, IDLE AND TAKEOFF POWER ON NR 1 ENGINE IAW AMM 71-00-00. LEAK AND OPERATIONAL CHECK GOOD.
Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 72,755 hrs · 11,406 cycles
AIRCRAFT WAS NOT GROUNDED. F1 LAVATORY B/C SMOKE ALARM SOUNDED AND WAS RESET BY CABIN CREW TWICE WITH NO SMOKE OR FIRE OBSERVED. REMOVED AND REPLACED F1 SMOKE DETECTOR AND ACCOMPLISHED SATISFACTORY OPERATIONAL CHECK IAW AMM 26-13-01.
Part: UNKNOWN — MALFUNCTIONED (WEATHER RADAR) · airframe 72,431 hrs · 11,353 cycles
AIRCRAFT WAS GROUNDED. ORD, AIR INTERRUPT, ORD-MAN. EMERGENCY DECLARED. LANDING UNEVENTFUL. AIRCRAFT OVERWEIGHT. DURING CLIMB CREW REPORTED WEATHER RADAR INOPERATIVE. MAINTENANCE ACCOMPLISHED SYSTEM BITE AND OPERATIONAL CHECKS IAW AMM 34-43-00 WITH NO FAULTS FOUND.
Part: SKIN — DAMAGED (CARGO DOOR) · airframe 70,085 hrs · 10,951 cycles
FORWARD CARGO DOOR DAMAGED AT AFT DOOR FRAME & SEAL SEAT NEEDS TO BE REPAIRED. COMPLIED WITH ALL STEPS OF FWD CARGO SKIN REPAIR IAW EA 258113 FINAL STEPS 1 - 24. ACFT IN BASE MX.
2015
Part: SIGN — UNSECURE (CABIN) · airframe 69,765 hrs · 10,888 cycles
DOOR 4L EXIT SIGN FELL OFF. SECURED EXIT SIGN ON SIDE OF 4L DOOR. THE ACFT WAS NOT GNDED.
Part: WARNING SYSTEM — FALSE ACTIVATION (COCKPIT) · airframe 69,603 hrs · 10,858 cycles
EMERGENCY DECLARED, LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING APPROACH WHEN SELECTED FLAPS FROM 1 TO 5, CREW RECEIVED A TE FLAP ASYMMETRY WARNING. PERFORMED FSEU BITE IAW FIM 27-51-00 WITH FAULT MSG 27-51104 RETURNED. PERFORMED TROUBLESHOOTING IAW FIG 105, SYS CHECKED OK. PERFORMED FUNCTIONAL CHECK OF FLAPS SEVERAL TIMES. ALL OPERATIONAL & INDICATION CHECKED OK.
Part: SEAT TRACK — DAMAGED (FUSELAGE) · airframe 68,767 hrs · 10,733 cycles
NUMBER 2 SEAT TRACK, AT SEAT LOCATION 6AB, HAS A DAMAGED EAR AT TIE DOWN LOCATION. REMOVED DAMAGED SEAT TRACK & INSTALLED NEW SEAT TRACK & DOUBLERS IAW SRM 53-00-52-2R-2.
Part: BYPASS SWITCH — FAULTY (FUEL SYSTEM) · airframe 68,662 hrs · 10,718 cycles
AIR INTERRUPT, EMERGENCY DECLARED, LANDING UNEVENTFUL & AIRCRAFT OVERWEIGHT. DURING CRUISE LEFT ENGINE FUEL FILTER BYPASS WARNING OCCURRED. R & R THE FUEL FILTER BYPASS SWITCH IAW AMM 78-11-03. PERFORMED OPERATIONAL CHECK OF ENGINE AT VARIOUS POWER SETTINGS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,941 hrs · 10,484 cycles
R1 DOOR EMER LIGHT INOPERATIVE. REPLACED R1 DOOR EMER LIGHT IAW AMM 33-51-06. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 66,469 hrs · 10,414 cycles
L1 DOOR EMER LIGHT INOPERATIVE. RELAMPED L1 DOOR EXT EMER LIGHT IAW AMM 33-51-00. SYS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 66,469 hrs · 10,414 cycles
R1 DOOR EXTERNAL EMER LIGHT INOPERATIVE. R & R LAMP IAW AMM 33-51-0. SYS CHECKED NORMAL.
2014
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 66,367 hrs · 10,395 cycles
L1 DOOR EXTERIOR EMER EXIT , SLIDE, LIGHT INOPERATIVE. RELAMPED & PERFORMED GOOD OPERATIONS CHECK OF L1 DOOR EMER LIGHTS IAW MM 33-51-00-725-247.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 66,367 hrs · 10,395 cycles
FORWARD GALLEY RT LOWERED CEILING EMER LIGHT INOPERATIVE. REELAMPED & PERFORMED GOOD OPERATIONS CHECK OF THE FWD GALLEY RT LOWERED CEILING EMER LIGHT IAW MM 33-51-00-725-247.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,367 hrs · 10,395 cycles
CORROSION ON SEAT TRACK UNDER M1 LAVATORY AT STATION 768, LBL 54.78, WL 199. R & R SEAT TRACK UNDER M1 LAVATORY FROM STATION 730.5 TO 784.5, WL 199 IAW SRM 53-0052-2R-2 FIG 201.
Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 66,367 hrs · 10,395 cycles
CORROSION SEAT TRACK UNDER M1 LAVATORY HAS CORROSION AT STATION 768, LBL 88.5 WL 199. R & R CORRODED SEAT TRACK UNDER M1 LAVATORY FROM STATION 768 - 846 LBL 88.5 WL 199 IAW SRM 53-00-52-2R-3.
Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 66,367 hrs · 10,395 cycles
CORROSION ON SEAT TRACK UNDER M1 LAVATORY AT BS 728 LBL 88.5 WL 199. REPAIRED SEAT TRACK BETWEEN BS 708 - 753, LBL 88.5, WL 199 IAW SRM 53-00-52-2R 3 & EA-53-037898.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 66,003 hrs · 10,335 cycles
R4 DOOR EMER EXIT IDENTIFIER SIGN INOPERATIVE. REPLACED R4 DOOR EMER EXIT IDENTIFIER SIGN LAMPS IAW MM 33-51-01. SYS CHECKED NORMAL.
Part: CONNECTOR — DISCONNECTED (CABIN) · airframe 66,003 hrs · 10,335 cycles
EMERGENCY SEAT MOUNTED LIGHT AT SEAT 32B INOPERATIVE. FOUND UNDER SEAT CONNECTOR DISCONNECTED. RECONNECTED CONNECTOR. SYS CHECKED NORMAL IAW MM 33-51-01.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 66,003 hrs · 10,335 cycles
L4 DOOR LOWER AFT EMER EXIT SIGN INOPERATIVE. REPLACED L4 DOOR LOWER AFT EMER EXIT SIGN LAMPS IAW MM 33-51-01. SYS CHECKED NORMAL.
Part: SIGN — DETACHED (CABIN) · airframe 65,965 hrs · 10,330 cycles
AFT CABIN EMER EXIT SIGN DETACHED & HANGING BY THE ELEC WIRE HARNESS. SECURED AFT CABIN EMER EXIT SIGN.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 63,818 hrs · 10,003 cycles
RIGHT NR 1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 1 DOOR EXTERIOR EMERGENCY LIGHT, OPERATIONS CHECKED NORMAL.
Part: SPLICE PLATE — CORRODED (RT WING) · corrosion level 2 · airframe 63,818 hrs · 10,003 cycles
CORROSION ON WING WALK PANEL SPLICE PLATE. R & R SPLICE PLATE.
Part: ANGLE — CRACKED (FUSELAGE) · airframe 63,818 hrs · 10,003 cycles
INTERCOSTAL UPPER CHORD IS CRACKED IN THE RADIUS. REPLACED THE INTERCOSTAL UPPER CHORD ANGLE IAW AARD 53-30-00-1.
2013
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 62,374 hrs · 9,764 cycles
RT NR 2 DOOR EXTERNAL EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 2 DOOR EXTERNAL EMERGENCY EXIT LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 62,374 hrs · 9,764 cycles
RT NR 2 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RT NR 2 DOOR EXTERIOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: INDICATOR — INOPERATIVE (COCKPIT) · airframe 61,104 hrs · 9,552 cycles
INTEGRATED FLIGHT STANDBY FLIGHT DISPLAY INOPERATIVE. REPLACED INTEGRATED STANDBY/AIRSPEED ALTIMETER. SYSTEM GROUND CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 61,103 hrs · 9,551 cycles
RT AFT ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR RT AFT ENTRY DOOR EXTERIOR EMERGENCY EXIT LIGHT. OPERATIONS CHECKED NORMAL
2012
Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,522 hrs · 9,164 cycles
SEAT 35B EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED LAMP FOR SEAT 35B EMERGENCY EXIT LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 58,522 hrs · 9,164 cycles
LEFT NUMBER 4 DOOR EMERGENCY EXIT SIGN HANDLE ILLUMINATION INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 EMERGENCY EXIT SIGN HANDLE ILLUMINATION. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 57,692 hrs · 9,041 cycles
SEAT 32B EMERGENCY LIGHT INOPERATIVE. REPLACED EMERGENCY LIGHT ASSEMBLY AT SEAT 32B. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,237 hrs · 8,970 cycles
LEFT NUMBER 1 EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 1 EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 57,237 hrs · 8,970 cycles
RIGHT NUMBER 1 DOOR EMERGENCY SIGN LOWER LIGHTS INOPERATIVE. REPLACED LAMPS FOR RIGHT NUMBER 1 DOOR EMERGENCY SIGN. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 57,237 hrs · 8,970 cycles
RIGHT NUMBER 1 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 1 DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 57,237 hrs · 8,970 cycles
RIGHT NUMBER 2 DOOR EMERGENCY SIGN LOWER LIGHTS INOPERATIVE. REPLACED LAMPS FOR RIGHT NUMBER 2 DOOR EMERGENCY LIGHT SIGN. OPS CHECK NORMAL.
Part: WARNING LIGHT — FALSE ACTIVATION (SHUTOFF VALVE) · airframe 55,859 hrs · 8,746 cycles
CREW REPORTED LEFT ENGINE HIGH PRESSURE SHUTOFF VALVE MESSAGE ON EICAS. EMERGENCY DECLARED FLIGHT RETURNED AND LANDED WITHOUT INCIDENT. SYSTEM GROUND CHECKED NORMAL.
2011
Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,317 hrs · 8,655 cycles
THE 31B EMERGENCY LIGHT CEILING INOPERATIVE. REPLACED LAMP FOR 31B EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — DAMAGED (CABIN) · airframe 55,317 hrs · 8,655 cycles
EMERGENCY LIGHT LEFT SIDE FORWARD OF BULK CARGO DOOR HAS ONE BROKEN NUT PLATE. REPLACED LIGHT ASSEMBLY FOR EMERGENCY LIGHT LEFT SIDE FORWARD OF BULK CARGO. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 55,317 hrs · 8,655 cycles
LEFT AFT EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR LEFT AFT EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: WIRE — SHORTED (BLEED AIR SYS) · airframe 55,163 hrs · 8,634 cycles
LAX - INFLIGHT OGG-DFW. CREW REPORTED RIGHT BLEED LIGHT ILLUMINATED ON OVERHEAD PANEL AND UNABLE TO EXTINGUISH. EMERGENCY DECLARED FLIGHT DIVERTED LAX LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. INSTALLED GROUND WIRE AT HIGH PRESSURE VALVE TERMINAL 2. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: SHUTOFF VALVE — MALFUNCTIONED (BLEED AIR SYS) · airframe 53,874 hrs · 8,447 cycles
LHR - INFLIGHT CDG-DFW. CREW REPORTED LEFT ENGINE HIGH PRESSURE SHUT-OFF VALVE STATUS MESSAGE. EMERGENCY DECLARED FLIGHT DIVERTED LHR LANDED WITHOUT INCIDENT. REPLACED LEFT ENGINE HIGH PRESSURE SHUT-OFF VALVE. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: GENERATOR — FAILED (RT ENGINE) · airframe 52,433 hrs · 8,247 cycles
DFW - CREW REPORTED RIGHT ENGINE GENERATOR DRIVE EICAS MESSAGE. EMERGENCY DECLARED FLIGHT RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECK NORMAL OPERATION.
2010
Part: SMOKE DETECTOR — FAULTY (LAVATORY) · airframe 51,152 hrs · 8,030 cycles
LHR - CREW REPORTED AFT A5 LAVATORY SMOKE DETECTOR WENT OFF. NO SMOKE WAS FOUND AND FLIGHT ATTENDANT RESET. EMERGENCY DECLARED FLIGHT LANDED LHR WITHOUT INCIDENT. AT GATE ARRIVAL ALARM WENT OFF AGAIN. REPLACED SMOKE DETECTOR IN LAVATORY A5. INSPECTED WATER HEATER, HEAT STRIP IN TRASH CAN, AND FIRE EXTINGUISHER NO DEFECTS FOUND. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 49,053 hrs · 7,677 cycles
AFT LEFT BODY EMERGENCY LIGHTS INOPERATIVE. REPLACE LAMP FOR AFT LEFT BODY EMERGENCY LIGHT. OPS CHECKED NORMAL.
Part: IDG — FAILED (RT ENGINE) · airframe 48,098 hrs · 7,510 cycles
DFE - CREW REPORTED THE RIGHT ENGINE GENERATOR FAILED IN FLIGHT. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,205 hrs · 7,340 cycles
EMERGENCY LIGHT AT SEAT 13H INOPERATIVE. RELAMPED 13H.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,205 hrs · 7,340 cycles
EMERGENCY LIGHT AT OVERHEAD SEAT 6G INOPERATIVE. RELAMPED SEAT 6G.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,205 hrs · 7,340 cycles
EMERGENCY LIGHT AT SEAT 20B INOPERATIVE. RELAMPED 20B.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,205 hrs · 7,340 cycles
EMERGENCY LIGHT AT SEAT 10B INOPERATIVE. RELAMPED 10B.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 47,205 hrs · 7,340 cycles
EMERGENCY LIGHT AT SEAT 30H INOPERATIVE. RELAMPED 30H.
2009
Part: FRAME — BENT (FUSELAGE) · airframe 46,585 hrs · 7,228 cycles
FOUND FUSELAGE STATION 500 FRAME INNER CHORD HORIZONTAL FLANGE BENT DOWN BETWEEN STATION 30 LEFT AND 31 LEFT DUE TO SUSPECTED IMPACT FROM A CARGO PALLET. APPROXIMATELY 6 INCHES LONG BY 0.5 INCH WIDE SECTION OF THE FLANGE WAS FOUND BENT DOWN A MAXIMUM OF 0.150 INCH. AS A PERMANENT REPAIR THE FLANGE WAS COLD WORKED BACK TO CONTOUR AND THEN A 0.125 INCH THICK STRAIGHT EXTRUSION WAS FITTED TO THE FORWARD SIDE OF THE FRAME ALONG THE DAMAGED AREA UNDER ENGINEERING AUTHORIZATION B767-53-007916.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,585 hrs · 7,228 cycles
CORROSION WAS FOUND AT CLIP NUT ATTACHMENT HOLES ALONG THE INNER CHORD OF THE STATION 325 FLOORBEAM. THE CORROSION WAS FOUND BETWEEN RIGHT BUTTLINE 35 AND RIGHT BUTTLINE 9. THE CORROSION WAS REMOVED BY BLENDING PER SRM STANDARD PRACTICES AND A 0.050 INCH 301.5 HARD STRAP WAS INSTALLED ACROSS ALL BLEND LOCATIONS EA B767-53-007944.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,585 hrs · 7,228 cycles
SEVERAL LOCATIONS OF CORROSION WERE FOUND AT CLIP NUT ATTACHMENT HOLES ALONG THE INNER CHORD OF THE STATION 347 FLOORBEAM. THE CORROSION WAS FOUND BETWEEN RIGHT BUTTLINE 22.5 AND RIGHT BUTTLINE 49. BLENDED CORROSION AND INSTALLED A FORMED ANGLE PER SRM 53-00-51-2R.
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 46,585 hrs · 7,228 cycles
CORROSION WAS FOUND AT CLIP NUT ATTACHMENT HOLES ALONG THE INNER CHORD OF THE FLOORBEAM AT STATION 347. THE CORROSION WAS FOUND BETWEEN RBL 22.5 AND RBL 49. BLENDED CORROSION AND INSTALLED A FORMED ANGLE PER SRM 53-00-51-2R.
2008
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 39,929 hrs
EZE - EMERGENCY LIGHTS AT SEAT ROWS 32H TO 41H INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT SEAT ROWS 32H TO 41H. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT) · airframe 39,871 hrs
MIA - EMERGENCY LIGHTS AT SEAT 20B TO 24B INOPERATIVE. REPLACED BATTERY PACK AT M737 FOR EMERGENCY LIGHTS AT SEAT 20B TO 24B. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: BULB — INOPERATIVE (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHT AT LEFT OVERWING MID POSITION INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT OVERWING MID POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — INOPERATIVE (EMERGENCY LIGHT)
DFW EMERGENCY LIGHT AT LEFT OVERWING FORWARD POSITION INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT OVERWING FORWARD POSITION. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WIRE HARNESS — BROKEN (EMERGENCY LIGHTS)
LGA - SEAT MOUNTED EMERGENCY LIGHTS AT SEATS 41HJ INOPERATIVE. REPAIRED HARNESS FOR EMERGENCY LIGHTS AT SEATS 41HJ. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISLOCATED (EMERGENCY LIGHT)
MIA - SEAT MOUNTED EMERGENCY LIGHT AT SEAT 21H AFT HAS RED LENS INSTEAD OF CLEAR. REPLACED RED LENS WITH CLEAR LENS FOR SEAT MOUNTED EMERGENCY LIGHT AT SEAT 21H. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: BATTERY PACK — DISCHARGED (CABIN)
SFO EMERGENCY LIGHT ON CEILING NEAR SEAT 13H INOPERATIVE. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION.--CLOSED--
2003
Part: IDG — FAILED (RT ENGINE)
FIVE HOURS INTO FLIGHT RIGHT GENERATOR TRIPPED AND RIGHT FIELD OFF LIGHT ILLUMINATED. REMOVED AND REPLACED RIGHT ENGINE IDG PER MM. OPS AND LEAK CHECK OK. (M)
2001
Part: BRAKE ASSY — SEIZED (MLG)
DFW - FLT 102 - EN ROUTE HNL-DFW, UPON LANDING DETECTED NR 1 WHEEL ASSEMBLY DRAG. LANDED DFW WITHOUT FURTHER INCIDENT. AT GATE ARRIVAL DETECTED FIRE AT NR 1 WHEEL ASSEMBLY CHOCKS. EXTINGUISHED FLAMES. REPLACED NR 1 TIRE ASSY DUE TO BRAKE SEIZURE. REPLACED NR 1 WHEEL BRAKE ASSY. PERFORMED INSPECTION OF THE MLG PER THE MM. NO DEFECTS NOTED. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — INOPERATIVE (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 29 AB INOPERATIVE. RE-PINNED EMERGENCY EXIT LIGHT CONNECTOR AT SIDE WALL. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: THROTTLE — JAMMED (COCKPIT)
MIA - FLT 1300 - DURING TAKEOFF ROLL, LEFT THROTTLE JAMMED AT TAKEOFF POWER. SHUTDOWN ENGINE AND RETURNED AND LANDED MIA WITHOUT INCIDENT. (M)
Part: LIGHT — INOPERATIVE (SEAT 40)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT FLOOR PATH LIGHTS AT SEAT 40 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT SEAT 40. SYSTEM GROUND CHECK NORMAL OPERATION. (M)