N370AA
Registered owner: ANDURIL INDUSTRIES INC, CA (owner ≠ operator)
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.
101 reports on file, 1995-07-22 – 2017-07-27.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 95,020 hrs · 15,018 cycles
DAMAGED FUSELAGE SKIN (HIT),0.5" APPROX, STA 654+22, BETWEEN S-25L AND S-26L.
Part: STIFFENER — CRACKED (FUSELAGE) · airframe 95,020 hrs · 15,018 cycles
CRACK 0.5" LENGTH ON NOSE WHEEL WELL BULKHEAD VERTICAL STIFFENER AT STA 287, LBL 6.0, WL 135.1.
Part: FRAME — CRACKED (FUSELAGE) · airframe 95,020 hrs · 15,018 cycles
CRACK BY LENGTH OF 1.378" AT FRAME INNER CHORD TRANSITION RADIUS STA 903.5 RBL 89.
Part: SKIN — CORRODED (LT WING) · corrosion level 2 · airframe 95,020 hrs · 15,018 cycles
CORROSION ON THE FILL PORT SURFACE AT LT WING, WS 798.2, S15-S16.
Part: SKIN — CORRODED (RT WING) · corrosion level 2 · airframe 95,020 hrs · 15,018 cycles
CORROSION AROUND THE WING UPPER SURFACE FUEL FILL PORT AT WS 785, BETWEEN STRINGERS 15 AND 16.
Part: SKIN — CORRODED (FUSELAGE) · corrosion level 2 · airframe 95,020 hrs · 15,018 cycles
CORROSION ON FUSELAGE SKIN, INTERNAL SIDE, STA 1131, BETWEEN STRINGER 29L AND LEFT KEEL BEAM.
Earlier reports · 1995–2015 · 95 reports
2015
Part: LENS — MISSING (EMERGENCY LIGHT) · airframe 94,673 hrs · 14,962 cycles
R2 DOOR EXIT SIGN LENS MISSING. REMOVED AND REPLACED EXIT SIGN. SYSTEM CHECKS NORMAL.
2014
Part: INDICATOR — DEFECTIVE (HYDRAULIC SYS) · airframe 94,347 hrs · 14,905 cycles
AIR INTERRUPT, DIVERTED & EMER DECLARED. LANDING UNEVENTFUL & ACFT NOT OVERWEIGHT. DURING CLIMB LOST ALL LT HYD SYS FLUID. FOUND LT HYD MODULE DIFFERENTIAL PRESS INDICATOR FAILED. R & R DAMAGED DIFFERENTIAL PRESS INDICATOR ON LT ENG DRIVEN PUMP MODULE IAW AMM 29-11-17-404-028. PERFORMED FLUSH OF LT HYD SYS IAW AMM 29-11-00-172-113. SERVICED SYS TO PROPER LEVEL. PERFORMED LEAK CHECK. SYSTEM CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 92,455 hrs · 14,616 cycles
LEFT NR 4 DOOR EXTERNAL EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR EXTERNAL EMER LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — NOT SEATED (EXTERIOR) · airframe 91,995 hrs · 14,538 cycles
EXTERIOR EMER LIGHT AT LT NR 4 DOOR INOPERATIVE. RESEATED LIGHT TO LIGHT ASSEMBLY. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,995 hrs · 14,538 cycles
EMERGENCY LIGHT AT SEAT 30B INOPERATIVE. REPLACED LAMP FOR EMER LIGHT AT SEAT 30B. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 91,995 hrs · 14,538 cycles
LEFT NR 4 DOOR INTERIOR EMER LIGHT INOPERATIVE. REPLACED LAMP FOR LT NR 4 DOOR INTERIOR EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
2013
Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,438 hrs · 14,122 cycles
SEAT 32HJ EMERGENCY LIGHT INOPERATIVE. REPLACED HOUSING & LAMP FOR SEAT 32HJ EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 89,438 hrs · 14,122 cycles
EMERGENCY LIGHTS ON LT SIDE OF AIRCRAFT FORWARD OF BULK CARGO INOPERATIVE. REPLACED BATTERY PACK AT M736.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 89,438 hrs · 14,122 cycles
EXIT SIGN ABOVE THE RT AFT EMERGENCY EXIT HATCH INOPERATIVE. REPLACED LAMPS FOR EXIT SIGN ABOVE THE RT AFT EMERGENCY EXIT HATCH. OPERATIONS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 89,438 hrs · 14,122 cycles
FOUND ALL EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT M733. OPERATIONS CHECKED NORMAL
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 89,438 hrs · 14,122 cycles
FOUND ALL EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT M731. OPERATIONS CHECKED NORMAL.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 89,438 hrs · 14,122 cycles
FOUND ALL EXTERIOR EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACKS AT M738. OPERATIONS CHECKED NORMAL.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 89,438 hrs · 14,122 cycles
FS SKIN BELOW & FWD OF THE LT NR 1 DOOR AT STATION 290 BELOW STRINGER 22 LT DAMAGED. INSTALLED A REPAIR DOUBLER IAW RM 53-00-01-2R REPAIR 14.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,438 hrs · 14,122 cycles
CABIN EMERGENCY LIGHT INOPERATIVE. REPLACED LIGHT SOCKET & LAMP FOR CABIN EMERGENCY LIGHT. OPERATIONS CHECKED NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 89,438 hrs · 14,122 cycles
EMERGENCY LIGHT ON OVERHEAD PANEL LT HAND SIDE AT ROW 28 INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD PANEL, LT HAND SIDE AT ROW 28. OPERATIONS CHECKED NORMAL.
Part: IRU — FAULTY (ZONE 100) · airframe 87,041 hrs · 13,745 cycles
LHR - INFLIGHT CDG-JFK. CREW REPORTED CENTER INERTIAL REFERENCE UNIT FAILED. EMERGENCY DECLARED FLIGHT DIVERTED LHR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CENTER IRU. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: CHARGER — INOPERATIVE (CABIN) · airframe 87,041 hrs · 13,745 cycles
EXIT SIGNS AT LEFT AND RIGHT NUMBER 4 DOOR INOPERATIVE. REPLACED CHARGER M1210. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,041 hrs · 13,745 cycles
OVERHEAD EMERGENCY LIGHT AT SEAT 27B INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT AT SEAT 27B. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 87,041 hrs · 13,745 cycles
OVERHEAD EMERGENCY LIGHT AT SEAT 31B INOPERATIVE. REPLACED LAMP FOR OVERHEAD EMERGENCY LIGHT AT SEAT 31B. OPS CHECK NORMAL.
2012
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 86,118 hrs · 13,599 cycles
RIGHT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP FOR RIGHT NUMBER 2 DOOR EXTERNAL EMERGENCY LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 86,118 hrs · 13,599 cycles
RIGHT AFT FUSELAGE EMERGENCY LIGHTS INOPERATIVE. REPLACED LAMPS FOR RIGHT AFT FUSELAGE EMERGENCY LIGHTS. OPS CHECK NORMAL.
Part: TERMINAL — BROKEN (BLEED AIR SYS) · airframe 86,099 hrs · 13,595 cycles
HNL - CREW REPORTED LEFT PNEUMATIC HIGH PRESSURE BLEED FAILURE. EMERGENCY DECLARED FLIGHT RETURNED HNL LANDED WITHOUT INCIDENT. PLACARD LEFT HIGH PRESSURE BLEED PER MEL. FLIGHT CONTINUED TO DESTINATION. REPLACED BROKEN TERMINAL LUG AT POSITION NUMBER ONE OF HIGH PRESSURE SHUTOFF VALVE AT MIA ON 11/19/2012. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: CADC — INOPERATIVE (COCKPIT) · airframe 85,231 hrs · 13,463 cycles
CDG - INFLIGHT FCO-JFK. CREW REPORTED ALTIMETER SPLIT. EMERGENCY DECLARED FLIGHT DIVERTED CDG LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT CENTRAL AIR DATA COMPUTER AND REPLACED FIRST OFFICERS ALTIMETER. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: CHARGER — INOPERATIVE (MAIN BATTERY) · airframe 85,179 hrs · 13,454 cycles
CDG - CREW REPORTED LOSS OF DC POWER ON SHORT FINAL. FLIGHT LANDED CDG WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND MAIN BATTERY CHARGER CIRCUIT BREAKER POPPED. REPLACED MAIN BATTERY CHARGER. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: SKIN — DAMAGED (FUSELAGE) · airframe 84,862 hrs · 13,400 cycles
FUSELAGE DAMAGE AT STATION 290, 7.5 INCHES BELOW STRINGER 22 LEFT. INSTALLED DOUBLER PER SRM 53-00-01-2R.
Part: PROBE — MALFUNCTIONED (PITOT/STATIC SYS) · airframe 84,588 hrs · 13,353 cycles
LHR - INFLIGHT FRA-LHR CREW REPORTED CAPTAINS PITOT SYSTEM FAILED AND CIRCUIT BREAKERS POPPED. EICAS MESSAGES FOR BOTH ELECTRONIC ENGINE CONTROLS, AILERON LOCKOUT AND RUDDER RATIO. EMERGENCY DECLARED FLIGHT DIVERTED LHR LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED CAPTAINS PITOT PROBE. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 84,372 hrs · 13,321 cycles
LEFT NUMBER 4 DOOR EMERGENCY EXIT SIGN THRESHOLD LIGHT HAS ONE LAMP INOPERATIVE. REPLACED LAMP FOR LEFT NUMBER 4 DOOR EMERGENCY EXIT SIGN THRESHOLD LIGHT. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,849 hrs · 13,241 cycles
EMERGENCY LIGHT BY RIGHT NUMBER 2 DOOR AFT GALLEY INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT BY RIGHT NUMBER 2 DOOR AFT GALLEY. OPS CHECK NORMAL.
Part: LENS — UNSECURE (CABIN) · airframe 83,849 hrs · 13,241 cycles
RIGHT NUMBER 2 DOOR EMERGENCY LIGHT LENS NOT SECURED. RE-SECURED LENS FOR EMERGENCY LIGHT AT RIGHT NUMBER 2 DOOR. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (EXIT SIGN) · airframe 83,849 hrs · 13,241 cycles
RIGHT CEILING AISLE EMERGENCY SIGN IN FIRST CLASS AISLE FORWARD INOPERATIVE. REPLACED LAMPS FOR RIGHT CEILING AISLE EMERGENCY SIGN IN FIRST CLASS. OPS CHECK NORMAL.
Part: LENS — UNSECURE (CABIN) · airframe 83,849 hrs · 13,241 cycles
LEFT NUMBER 2 DOOR EMERGENCY LIGHT LENS NOT SECURED. RE-SECURED LENS FOR EMERGENCY LIGHT AT LEFT NUMBER 2 DOOR. OPS CHECK NORMAL.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 83,849 hrs · 13,241 cycles
LEFT NUMBER 1 DOOR EMERGENCY EXIT FLOOR LIGHT ON LOWER SIDEWALL INOPERATIVE. REPACED LAMP FOR LEFT NUMBER 1 DOOR EMERGENCY EXIT FLOOR LIGHT ON LOWER SIDEWALL. OPS CHECK NORMAL.
Part: SKIN — SCRATCHED (FUSELAGE) · airframe 83,362 hrs · 13,160 cycles
SCRIBE MARKS UNDER DECALS ON FUSELAGE SKIN AT STATION 622. INSTALLED REPAIR DOUBLER TO STATION 622.
Part: STRUCTURE — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,362 hrs · 13,160 cycles
CORROSION FOUND ON BOTTOM CHORD BELOW FAILSAFE STRAP IN FORWARD CARGO. CORROSION REMOVED AND FREEZE PLUGS INSTALLED PER EA B767-53-022201.
Part: STRUCTURE — CRACKED (STABILIZER) · airframe 83,362 hrs · 13,160 cycles
CRACK AT RIGHT FORWARD OUTER CHORD STATION 1809.5. REPAIR PIECE INSTALLED PER ECO C1945DN.
Part: STRINGER — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,362 hrs · 13,160 cycles
STRINGER 34 RIGHT HAS CORROSION AT STATION 742. ACCOMPLISHED SPLICE REPAIR PER SRM 53-00-03-2R.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,362 hrs · 13,160 cycles
SMALL J CAP FORWARD CARGO STATION 582 RIGHT BUTTLINE 40 CORRODED. REPLACED J CAP PER SRM 51-40-02.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,362 hrs · 13,160 cycles
FORWARD CARGO SMALL J CAP STATION 575 RIGHT BUTTLINE 40 CORRODED. REPLACED J CAP PER SRM 51-40-02.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,362 hrs · 13,160 cycles
CORROSION FOUND ON SHORT J-CAP AT STATION 610 FORWARD CARGO. REPLACED J-CAP PER SRM 51-40-02.
Part: CAP — CORRODED (FUSELAGE) · corrosion level 2 · airframe 83,362 hrs · 13,160 cycles
CORROSION ON SMALL J-CAP IN FORWARD CARGO AT STATION 513 RIGHT BUTTLINE 40. REPLACED J-CAP PER SRM 51-40-02.
Part: AILERON — DELAMINATED (LT WING) · airframe 83,362 hrs · 13,160 cycles
OUTBOARD AILERON 53 INCHES OUTBOARD OF INBOARD EDGE AT TRAILING EDGE DELAMINATED. ACCOMPLISHED HOT BOND REPAIR PER SRM 57-60-02.
Part: SPAR — CRACKED (LT PYLON) · airframe 83,362 hrs · 13,160 cycles
LEFT PYLON HAS CRACK AT UPPER SPAR WEB AT CUT OUT FOR FEEDER CABLE THROUGH HOLE. INSTALLED DOUBLER REPAIR PER AARD 54-52-01-1.
2011
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 82,036 hrs · 12,948 cycles
LEFT NUMBER 4 AND RIGHT NUMBER 4 DOORS EMERGENCY EXIT LIGHTS ARE INOPERATIVE. REPLACED BATTERY PACK AT RIGHT NUMBER 4 DOOR. OPS CHECK NORMAL.
Part: SLIDE — LOOSE (CABIN) · airframe 81,083 hrs · 12,800 cycles
LEFT OVERWING SLIDE DID NOT DEPLOY BECAUSE THE PACK BOTTLE WAS STILL PINNED, HOWEVER THE SLIDE PACK COVER CAME LOOSE. REPLACED ALL BLOW DOWN ACTUATORS, SPOILER, ALL THREE DOOR ACTUATORS, DEPLOYMENT CABLE, BOTTLE AND SLIDE PACK.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 79,161 hrs · 12,513 cycles
THREE EXTERIOR EMERGENCY LIGHTS AFT LEFT SIDE INOPERATIVE. REPLACED BATTERY PACK M738. OPS CHECK NORMAL.
2010
Part: FITTING — DAMAGED (LT PYLON) · airframe 77,795 hrs · 12,290 cycles
ABNORMALITIES NOTED ON LEFT PYLON MID SPAR FITTING INBOARD AND OUTBOARD EDGE OF UPPER TANG. PYLON WAS REMOVED AND AREAS WERE POLISHED PER 767-300 SRM CHAPTER 51, HIGH FREQUENCY EDDY CURRENT INSPECTION SHOWED NO CRACKS. AREAS WERE CAD PLATED PER SOPM 20-42-10. EA B767-54-013104 CLASSIFIED MAJOR AND APPROVED FOR STAGE I STATIC STRENGTH.
Part: COMPUTER — FAILED (EICAS) · airframe 77,256 hrs · 12,188 cycles
ORD - DURING CLIMB NUMEROUS SPONTANEOUS EICAS ANNUNCIATIONS OCCURRED. EMERGENCY DECLARED, RETURNED ORD LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT EICAS COMPUTER. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 77,040 hrs · 12,154 cycles
EMERGENCY EXIT SLIDE LIGHT AT RIGHT NUMBER 1 DOOR INOPERATIVE. REPLACED BATTERY PACK FOR RIGHT NUMBER 1 DOOR. OPS CHECKS GOOD.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 77,040 hrs · 12,154 cycles
EMERGENCY EXIT SLIDE LIGHT AT RIGHT NUMBER 1 DOOR INOPERATIVE. REPLACED EXIT LIGHT ASSEMBLY FOR RIGHT NUMBER 1 DOOR. OPS CHECKS GOOD.
Part: PUMP — LEAKING (RT ENGINE) · airframe 75,480 hrs · 11,861 cycles
JFK - CREW REPORTED RIGHT HYDRAULIC SYSTEM FAILURE. EMERGENCY DECLARED RETURNED JFK LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE DRIVEN PUMP THAT WAS LEAKING. SYSTEM GROUND CHECK NORMAL OPERATION.
Part: HYDRAULIC LINE — LEAKING (HYDRAULIC SYS) · airframe 75,454 hrs · 11,855 cycles
MIA - FLIGHT CREW REPORTED EICAS MESSAGES - RIGHT HYDRAULIC SYSTEM PRESSURE AND RIGHT HYDRAULIC QUANTITY. FLIGHT LANDED MIA WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND RIGHT ENGINE DRIVEN PUMP CASE DRAIN RIGID LINE LEAKING. REPLACED LINE. SYSTEM GROUND CHECK NORMAL OPERATION.
2009
Part: FLOORBEAM — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,151 hrs · 11,279 cycles
AFW - FLOORBEAM AT STATION 325 HAS CORROSION AT RIGHT BUTTLINES 21, 25, 49, AND 57 THAT EXCEEDS SRM LIMITS. INSTALLED REPAIR STRAP IN ACCORDANCE WITH MRB 767-3385.
Part: FLOORBEAM — CRACKED (FUSELAGE) · airframe 72,151 hrs · 11,279 cycles
AFW - FLOORBEAM AT STATION 347 TOP SURFACE CRACKED AT RIGHT BUTTLINE 84. INSTALLED FLOORBEAM REPAIR, REPAIR ANGLES AND STRAP IN ACCORDANCE WITH MRB 767-3387 AND SRM 53 00 51 2R.
Part: SILL — CORRODED (FUSELAGE) · corrosion level 2 · airframe 72,151 hrs · 11,279 cycles
AFW - AFT CARGO DOOR CUTOUT LOWER MAIN SILL INNER CHORD HAS CORROSION. AREA OF DISCREPANCY IS 3.5 INCHES BY 2.3 INCHES WITH A DEPTH OF .021 INCH. HIGH FREQUENCY EDDY CURRENT INSPECTION ACCOMPLISHED IN AFFECTED FASTENERS WITH NO CRACKS NOTED. BLENDED CORROSION AND REPAIRED IN ACCORDANCE WITH MRB 767-3382.
2008
Part: LIGHT — INOPERATIVE (ZONE 200)
DFW - SEAT MOUNTED EMERGENCY LIGHT AT AFT SEAT 34J INOPERATIVE. REPLACED LIGHT ASSEMBLY AT SEAT 34J. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LIGHT — INOPERATIVE (CABIN)
DFW - EMERGENCY LIGHT AT LEFT CENTER OVERWING INOPERATIVE. REPLACED LAMPS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: GENERATOR — FAILED (LEFT)
YOW INFLIGHT T55/03SEP MAN TO ORD. CREW REPORTED LT GENERATOR FAILED AND UNABLE TO START AUXILIARY POWER UNIT APU. LANDED YOW WITHOUT INCIDENT. REPLACED LT INTEGRATED DRIVE GENERATOR. SYSTEM GROUND CHECKED NORMAL OPS.
Part: LIGHT — INOPERATIVE (CABIN) · airframe 69,847 hrs
SFO - EMERGENCY LIGHT AT OVERHEAD SEAT 5B INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT OVERHEAD SEAT 5B. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 68,056 hrs
JFK - EMERGENCY LIGHT AT LEFT AFT LAVATORY DOOR AISLE EXIT SIGN LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT LEFT AFT LAVATORY DOOR AISLE EXIT SIGN. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHTS) · airframe 68,035 hrs
JFK - EMERGENCY LIGHT AT RIGHT SIDE AFT OF FORWARD GALLEY MISSING LENS. REPLACED LENS FOR EMERGENCY LIGHT AT RIGHT SIDE AFT OF FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: TRANSMITTER — INOPERATIVE (FUEL FLOW) · airframe 67,975 hrs
JFK INFLIGHT T0041/20JAN CDG TO ORD - CREW REPORTED FUEL DISAGREE MESSAGE IN FLIGHT. LANDED JFK WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED LEFT FUEL FLOW TRANSMITTER. SYSTEM GROUND CHECKED NORMAL OPERATION.
2007
Part: BATTERY PACK — DISCHARGED (CABIN)
SFO - OVERWING EMERGENCY LIGHTS AT LEFT AND RIGHT INOPERATIVE. REPLACED BATTERY PACK FOR OVERWING EMERGENCY LIGHTS AT LEFT AND RIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: PIN — LOOSE (CONNECTOR)
DFW - EMERGENCY LIGHTS AT SEAT 17B INOPERATIVE. RESEATED WALL TO SEAT CONNECTOR PIN AT SEAT 17B FOR INOPERATIVE EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BULB — BURNED OUT (EMERGENCY LIGHTS)
DFW - EMERGENCY LIGHT AT SEAT ROW 23B INOPERATIVE. RELAMPED OVERHEAD EMERGENCY LIGHT AT ROW 23B. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: BULB — INOPERATIVE (EMERGENCY LIGHT)
SFO - EMERGENCY LIGHT AT LEFT FORWARD OUTSIDE OVERWING INOPERATIVE. RELAMPED EMERGENCY LIGHT AT LEFT FORWARD OUTSIDE OVERWING. SYSTEM GROUND CHECKED NORMAL OPERATION.
2004
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)
DFW - EMERGENCY LIGHTS ON AFT SIDE OF FORWARD GALLEY INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS ON AFT SIDE OF FORWARD GALLEY. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: WARNING LIGHT — ILLUMINATED (COCKPIT)
CDG - LEFT GENERATOR DRIVE LIGHT WARNING ILLUMINATED. COULD NOT DUPLICATE ON GROUND. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: IDG — MALFUNCTIONED (LT ENGINE)
FCO - LEFT GENERATOR DRIVE EICAS MESSAGE APPEARED, FLICKERED AND THEN EXTINGUISHED. SERVICED LEFT HAND IDG. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
MIA EMERGENCY ESCAPE LIGHT AT SEAT 29H INOPERATIVE. FOUND LOOSE CONNECTOR. SECURED LOOSE CONNECTOR FOR EMERGENCY ESCAPE LIGHT AT SEAT 29H. SYSTEM GROUND CHECKED NORMAL OPERATION. (CLOSED)
2003
Part: BEAM — CORRODED (FUSELAGE)
THE 9-10 BEAM BOTH LEFT AND RIGHT HAD CORROSION REMOVED IN THE 2ND HOLE FROM OUTBOARD END, LEFT HOLE AT 463 AND RIGHT HOLE AT .532. FABRICATE A1-N1-BR BUSHING WITH .001 INTERFERENCE FIT WET WITH BMS 6-95 SEALANT. FINAL REAM ID TO ORIGINAL DUB SPEC. INSTALLED REPAIR WASHER PER AARD 51-20-01-1. (M)
Part: IDG — FAILED (LT ENGINE)
MIA - DURING FLIGHT, THE LEFT GEN DRIVE LIGHT FLICKERED. SOON THE LEFT GEN DRIVE LIGHT BEGAN TO FLICKER. THIS CONTINUED FOR A PERIOD AND LEFT DRIVE WAS DISCONNECTED. LEFT IDG VERIFIED INOPERATIVE NO SPARE IDG AT MAD DEFERRED PER MEL 24-01 AUTH 01-455DC-A IDG 1 NAD 2 SERVICED. APU OIL VERIFIED FULL IDG DEC ENTERED ON MIC SHEET. REMOVED AND REPLACED IDG ON LEFT ENGINE, REQUIRES OP AND LEAK CHECK. LEFT IDG OP CHECK GOOD. LEAK CHECK OK. (M)
Part: CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, LEFT WING SLIDE EMERGENCY EXIT LIGHT FAILED TO ILLUMINATE DURING TEST. SECURED LEFT WING SLIDE EMERGENCY EXIT LIGHT CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2002
Part: ADC — FAILED (E/E COMP)
FRA - FLT 71 - AFTER TAKEOFF FIRST OFFICERS AIRSPEED AND ALTIMETER FAILED. SELECTING ADC TO ALTIMETER RESTORED INFORMATION. REPLACED F/O ADC PER MM 34-12-01-4. ALL CHECKS OK. (M)
2001
Part: CONNECTOR — BROKEN (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9B INOPERATIVE. REPAIRED CONNECTOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: BATTERY PACK — INOPERATIVE (CABIN)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY ESCAPE PATH LIGHTS SEAT 2B INOPERATIVE. REPLACED BATTERY PACK AFT OF SEAT 2B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — DIRTY (RT WING)
LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT RIGHT SIDE AFT WING INOPERATIVE. CLEANED EMERGENCY EXIT LIGHT AT RIGHT WING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — BROKEN (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 37H INOPERATIVE. REPAIRED EMERGENCY EXIT WIRE AT SEAT 37H. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, OVERHEAD EMERGENCY EXIT LIGHT INOPERATIVE. EMERGENCY EXIT CABIN SEAT LIGHTS INOPERATIVE. LEFT FIRST CLASS EMERGENCY EXIT LIGHT INOPERATIVE. FIRST ROW BUSINESS CLASS EMERGENCY EXIT LIGHT INOPERATIVE. RE-CONNECTED EMERGENCY EXIT CONNECTOR AT BATTERY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — SHORTED (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT ESCAPE SEAT PATH LIGHTS AT ROW 32 TO ROW 41 INOPERATIVE. REPAIRED SHORTED WIRE AT ROW 36. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (SEAT 27B)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 27B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 27B. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: LIGHT — INOPERATIVE (SEAT 40B)
DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 40B INOPERATIVE. REPLACED EMERGENCY EXIT SEAT PATH LIGHT AT SEAT 40B. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1998
Part: FLOORBEAM — CORRODED (BS 782-830)
AFW - FOUND AND BLENDED CORROSION IN CABIN FLOORBEAMS. THE BLENDOUTS EXCEED SRM MAX ALLOWABLE LIMITS. SPLICED IN NEW SECTION OF FLOORBEAM ON BOTH FLOORBEAM PER MRB767-1614. (M)
Part: FRAME — CORRODED (BS 1219)
AFW - FOUND AND BLENDED OUT CORROSION ON THE LOWER SURFACE OF THE FRAME INNER CHORD AFT FLANGE IN THE AFT CARGO COMPARTMENT. THE BLENDOUT EXCEEDED SRM MAX LIMITS. ALODINED PRIMED AND PAINTED BLENDED AREA, APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1613. (M)
Part: FRAME — CORRODED (BS 1285)
AFW - FOUND AND BLENDED OUT CORROSION ON THE LOWER SURFACE OF THE FRAME INNER CHORD FORWARD FLANGE IN THE AFT CARGO. THE BLENDOUT EXCEEDED SRM MAX LIMITS. ALODINED, PRIMED AND PAINTED BLENDED AREA. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB 767-1617. (M)
Part: FLOORBEAM — CORRODED (BS 786-830)
AFW - FOUND AND BLENDOUT CORROSION IN CABIN FLOORBEAM. THE BLENDOUT EXCEEDS SRM MAX ALLOWABLE LIMITS. SPLICED IN NEW SECTION FLOORBEAM FROM STATION 782 TO STATION 831 PER MRB 767-1615. (M)
Part: CHORD — CORRODED (CARGO DOORWAY)
AFW - FOUND AND BLENDED OUT CORROSION ON THE UPPER SURFACE OF THE INNER CHORD OF THE AFT CARGO DOOR LOWER MAIN SILL. THE BLEND OUT EXCEEDS SRM MAX LIMITS. ALODINED, PRIMED AND PAINTED AREA. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB767-1612. (M)
Part: SUPPORT — CORRODED (R2 DOORWAY)
AFW - FOUND AND BLENDED OUT CORROSION ON THE FLOOR SUPPORT TEE 146T0051-40 AT THE R2 DOOR LOWER SILL. REFINISHED THE BLENDOUT PER SRM 53-00-15. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB767-1616. (M)
Part: TRUNNION — CORRODED (RT MLG)
AFW - RIGHT MAIN AFT TRUNNION OUTER BUSHING HOLE HAD LIGHT SCORING AND CORROSION BLENDED. REMOVED CORROSION AND LIGHTLY BLENDED SCORING. APPLIED ALODINE TO INSIDE SURFACE OF BORE AND APPLIED SEALANT FOR BUSHING INSTALLATION. APPROVED FOR CONTINUED SERVICE WITH NOTED CONDITION BY ENGINEERING PER MRB767-1611. (M)
Part: IDG — FAILED (LT GEN)
SCL - FLT 2101 - AFTER TAKEOFF DURING CLIMB-OUT PASSING 12,000 FEET, LEFT GENERATOR LIGHT ILLUMINATED. TRIED RESET, BUT LT GEN CAME BACK ON. AFTER CONSULTATION WITH COMPANY AND TULSA TECH, CONTINUED ON WITH APU RUNNING FOR ENTIRE FLIGHT. REMOVED AND REPLACED LT ENG IDG PER MM 24-11-01-4-2. RUN LT ENG IDG WORKS OK. NOTE: EXTENDED RANGE EVENET REPORT (ER) NR AFW770. (X)
Part: PIN — DEFECTIVE (CABIN)
SFO - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHTS INOPERATIVE AT PAX SEATS 19B, 20B AND 21B. REPLACED PINS AT PAX SEATS 19B, 20B AND 21B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1997
Part: CONNECTOR — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 36AB INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 36AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: PIN — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 36AB INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT PINS AT CONNECTOR ON PAX SEAT 36AB. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHT AT PAX SEAT 36B INOPERATIVE. CLEANED AND RESECURED EMERGENCY EXIT LIGHT CONNECTOR AT PAX SEAT 36B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — BROKEN (CABIN)
SFO - DURING OVERNIGHT CHECK, EMERGENCY EXIT LIGHTS AT PAX SEATS 36B AND 40B INOPERATIVE. REPLACED BROKEN EMERGENCY EXIT LIGHT CONNECTORS AT PAX SEATS 36B AND 40B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1995
Part: EEL CONNECTOR — LOOSE (CABIN)
SFO - DURING OVERNIGHT CHECK, FOUND EMERGENCY EXIT PATH LIGHTS AT SEAT 17B INOPERATIVE. RECONNECTED CONNECTOR AT SEAT 17B TO FLOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)