N80052
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.
63 reports on file, 1995-11-18 – 2008-08-31.
Part: COVER — BROKEN (CABIN PRESSURE)
NAS INFLIGHT T861/31AUG MCO TO SJU. CREW REPORTED PRESSURIZATION FAULT. LANDED NAS WITHOUT INCIDENT. REPLACED FLAPPER VALVE COVER. SYSTEM GROUND CHECKED NORMAL OPS.
Part: LINK ASSY — DEFECTIVE (LANDING GEAR) · airframe 51,483 hrs
JFK INFLIGHT T1299/11JUN. CREW REPORTED RED MAIN LANDING GEAR DOOR INDICATION AFTER TAKEOFF. RETURNED TO JFK AND LANDED WITHOUT INCIDENT. REPLACED LANDING GEAR PROXIMITY SENSOR LINK ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: PITOT TUBE — FAILED
PTY INFLIGHT T2110/07JUN LIM TO MIA. CAPTAINS AIR SPEED INDICATION INOPERATIVE. LANDED PTY WITHOUT INCIDENT. REPLACED CAPTAINS PITOT PROBE. SYSTEM GROUND CHECKED NORMAL OPERATION. (A)
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,893 hrs
JFK - EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER FOUR DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,893 hrs
JFK - EMERGENCY LIGHT AT LEFT NR 2 DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT LEFT NUMBER TWO DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 50,893 hrs
JFK - EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR INOPERATIVE. REPLACED LAMP FOR EMERGENCY LIGHT AT RIGHT NUMBER ONE DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Earlier reports · 1995–2007 · 57 reports
2007
Part: COMPUTER — INOPERATIVE (RUDDER SYSTEM)
MIA INFLIGHT T377/30NOV - BOTH NUMBER ONE AND TWO RUDDER SYSTEM FAILURE DURING CLIMB. RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NUMBER ONE AND TWO FEEL LIMITATION COMPUTERS, NUMBER ONE AND TWO SLAT FLAT CONTROL COMPUTERS, AND NUMBER ONE AND TWO FAULT WARNING CONTROL SYSTEM AND VARIABLE STOP ACTUATOR. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHTS)
JFK - SEAT MOUNTED EMERGENCY LIGHTS AT LEFT COACH INOPERATIVE. REPLACED BATTERY PACK FOR SEAT MOUNTED EMERGENCY LIGHTS AT LEFT COACH. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: VALVE — LEAKING (HYD SYSTEM)
BOG INFLIGHT T915/01OCT - BLUE HYDRAULIC SYSTEM AMBER LOW QUANTITY INDICATION AND CHIME. LANDED BOG WITHOUT INCIDENT. FOUND PRESSURE LINE IN WHEEL WELL LEAKING. TIGHTENED LINE AT C PORT OF RELIEF VALVE 2063. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS)
MIA - EMERGENCY LIGHT AT SEAT 29G INOPERATIVE. SECURED WIRE AT CONNECTOR FOR EMERGENCY LIGHT AT SEAT 29G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT AT SEAT 25G INOPERATIVE. RESEATED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 25G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT AT SEAT 24G HAS LENS MISSING. REPLACED LENS FOR EMERGENCY LIGHT AT SEAT 24G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
MIA - FOUND EMERGENCY LIGHT AT SEAT 16C INOPERATIVE. SECURED CONNECTOR FOR EMERGENCY LIGHT AT SEAT 16C. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: LENS — MISSING (EMERGENCY LIGHT)
MIA - EMERGENCY LIGHT IN FIRST CLASS AT LEFT SIDE OF GALLEY BULKHEAD MISSING COVER. REPLACED LENS FOR EMERGENCY LIGHT IN FIRST CLASS AT LEFT SIDE OF GALLEY BULKHEAD. SYSTEM GROUND CHECKED NORMAL OPERATION.
2006
Part: BATTERY PACK — DISCHARGED (CABIN)
MIA - EMERGENCY LIGHTS FROM SEATS 16G TO 22G ARE DIM. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS SEATS 16G TO 22G. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: POWER SUPPLY — INOPERATIVE (EMERGENCY LIGHTS)
TUL - EMERGENCY EXIT LIGHTS AT LEFT AND RIGHT NUMBER TWO DOORS INOPERATIVE. REPLACED POWER SUPPLY UNIT FOR EMERGENCY EXIT LIGHTS AT LEFT AND RIGHT HAND NUMBER TWO DOORS. SYSTEM GROUND CHECKED NORMAL OPERATION.
Part: CONNECTOR — LOOSE (EMERGENCY LIGHT)
JFK - EMERGENCY LIGHT AT 36C INOPERATIVE. FOUND LOOSE CONNECTOR. RESECURED CONNECTOR FOR EMERGENCY LIGHT AT 36C. SYSTEM GROUND CHECKED NORMAL OPERATION.
2003
Part: O-RING — CUT (HYD SYSTEM)
AIRCRAFT LOST GREEN SYSTEM HYDRAULIC QUANTITY. AIRCRAFT LANDED BOS WITHOUT INCIDENT. FOUND GREEN SYSTEM PRESSURE LINE TO MANIFOLD O-RING CUT AND LEAKING. REPLACED O-RING AND BACK UP RING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2001
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 9G INOPERATIVE. RESECURED EMERGENCY EXIT LIGHT CONNECTOR AT SEAT 9G. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
2000
Part: BOTTLE — DISCHARGED (PAX DOOR ASSIST)
MIA - DURING OVERNIGHT CHECK, L1, L2, AND R1 DOOR ASSIST BOTTLES LOW PRESSURE. SERVICED BOTTLES. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: CONNECTOR — LOOSE (CABIN)
TUL - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT DOOR R2 INOPERATIVE. RECONNECTED CONNECTOR ON BATTERY PACK. SYSTEM GROUND CHECKED, NORMAL OPERATION. (X)
Part: BOTTLE — DISCHARGED (PAX DOOR)
JFK - DURING OVERNIGHT MAINTENANCE, R1 DOOR ASSIST BOTTLE PRESSURE BELOW LIMITS. SERVICED BOTTLE. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
1999
Part: SUPPORT — CORRODED (BS 56)
TUL - FLOOR SUPPORT AT FRAME 56 HAS CORROSION ON TOP SIDE. INSTALLED FLOOR SUPPORT SECTION PER SRM 53-10-15. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: STRINGER — CORRODED (BS 54.1)
TUL - CORROSION ON STR 55R. INSTALLED ANGLE REPAIR PER SRM 53-10-14-2. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: STRINGER — CORRODED (BS 54.2)
TUL - CORROSION ON STR 55R. INSTALLED ANGLE REPAIR PER SRM 53-10-14-2. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: STRINGER — CORRODED (BS 54.1)
TUL - CORROSION ON STR 53R. INSTALLED ANGLE REPAIR PER SRM 53-10-14-2. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: STRINGER — CORRODED (CARGO COMPT)
TUL- STR 45R CORRODED - FRAME FITTING. REPLACED STRINGER AND FRAME FITTING PER SRM 53-17-18. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: FRAME — CORRODED (FUSELAGE)
TUL - CORROSION ON FRAME 58 BETWEEN STR 55L AND STR 55R. INSTALLED DOUBLER PER SRM 51-10-13. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: SPLICE — CORRODED (BS 65)
TUL - CORROSION ON STRINGER SPLICE AT STR 57 AND AFT SIDE OF FRAME 65. REMOVED AND REPLACED STRINGER SPLICE PER SRM 53-10-14. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: BEAM — CORRODED (FRAME 72)
TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: FRAME — CORRODED (FUSELAGE)
TUL - CORROSION ON FRAME BETWEEN STR 49L TO STR 49R. INSTALLED DOUBLER REPAIR PER SRM 53-10-13. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: BEAM — CORRODED (FRAME 72)
TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: BEAM — CORRODED (FRAMES 75-76)
TUL - CORROSION BEYOND LIMITS. STRAP REPAIRED PER AARD 53-20-00-2. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: BEAM — CORRODED (GALLEY)
TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: BEAM — CORRODED (FRAMES 72-73)
TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: SEAT TRACK — CORRODED (FRAMES 28-31)
TUL - CORROSION BEYOND LIMITS. SECTION SPLICE PER SRM 53-10-16. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: BEAM — CORRODED (FRAMES 79-80)
TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: BEAM — CORRODED (FRAMES 77-80)
TUL - CORROSION BEYOND LIMITS. STRAP REPAIR PER AARD 53-20-00-2. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: BEAM — CORRODED (FRAMES 77-79)
TUL - CORROSION BEYOND LIMITS. STRAP REPAIRED PER AARD 53-29-00-2. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: BEAM — CORRODED (FRAME 74)
TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-74-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: BEAM — CORRODED (FRAMES 29-33)
TUL - CORROSION BEYOND LIMITS. REMOVED AND REPLACED BEAM PER SRM 51-72-10-0. TST: 31,677 HOURS. CYCLES: 12,770. (X)
Part: LIGHT — INOPERATIVE (L4/R4 DOOR)
MIA - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT SIGN ON FLOOR AT R4 AND L4 INOPERATIVE. REPLACED EMERGENCY EXIT FLOOR PATH LIGHT STRIP AT R4 AND L4 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: WIRE — BROKEN (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE, RIGHT SIDE EMERGENCY EXIT FLOOR PATH LIGHTING INOPERATIVE. REPAIRED WIRE ON RIGHT SIDE OF EMERGENCY EXIT FLOOR PATH LIGHTING. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: ANGLE — CRACKED (BS 2612)
TUL - EFO252X CALLS FOR INSPECTION OF RT FUSE WING ROOT PICKUP ANGLE FOR CRACKS. A .75 INCH CRACK RADIATING OUT OF FASTENER TO THE OUTBOARD EDGE OF THE FITTING WAS FOUND. REMOVED PICKUP ANGLE, HFEC ACCOMPLISHED. NO CRACKS FOUND, INSTALLED NEW ANGLE PER ECO EO794. (M)
1997
Part: MOUNT — CORRODED (LAVATORY)
TUL - CORROSION BEYOND LIMITS UNDER L LAVATORY. REMOVED AND REPLACED TRACK SECTION PER SRM 51-72-10. (M)
Part: SUPPORT — CORRODED (WATER PUMP)
TUL - SUPPORT TRAY FOR WATER TANK PERSS PUMP EXFOLIATED. MANUFACTURED NEW SUPPORT TRAY PER ESO 30595 DABED 8/6/97, TRAY INSTALLED ON E58 NR 0094616. (M)
Part: SILL — CORRODED (BS 1446-1754)
TUL - FORWARD CARGO DOOR BEAM, TOP FLANGE HAS CORROSION TOP SURFACE PLACE AND FROM FRAME 20 TO 25A. INSTALLED DOUBLERS AND LEVEL BLEND PER ESO 30595 DATED 8/6/97. (M)
Part: SUPPORT — CORRODED (CABIN)
TUL - CORROSION ON FLOOR SUPPORT NR 8 AT FRAME 74. REMOVED OLD FLOORBOARD SUPPORT FROM FRAME 73.5 THROUGH FRAME 75. MADE NEW PART PER AARD 51-10-3 INSTALLED NEW FLOORBOARD SUPPORT PER SRM 51-72-10-0. INSTALLED SPLICE AT FRAME 75 PER ESO3095. (M)
Part: SUPPORT — CORRODED (CABIN)
TUL - FLOOR SUPPORT NR 4 IS CORRODED AT FRAME 74. REMOVED OLD SUPPORT FROM FRAME 73.5 THROUGH FRAME 75 MADE NEW PART PER AARD 51-10-3. INSTALLED NEW FLOORBOARD SUPPORT PER SRM 51-72-10-0. INSTALLED SPLICE AT FRAME 75 PER E20 30595. (M)
Part: SEAT TRACK — CORRODED (CABIN)
TUL - SEAT TRACK NR 8 HAS CORROSION AT FLOORBOARD LANDING AT FRAME 34. SPLICED IN SECTION OF SEAT TRACK FROM FRAME 33-35 PER FIG SRM 53-10-16-2 FIG 203. (M)
Part: SEAT TRACK — CORRODED (FUSELAGE)
TUL - FOUND SEAT TRACK HAS CORROSION IN SEVERAL PLACES BEYOND LIMITS FROM FRAME 31-32. REMOVED AND REPLACED SUPPORT FROM FRAME 26-33 PER SRM 51-72-10-0. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND CORROSION ON STRINGER 46R WHEN WEB REMOVED. REMOVED CORROSION PER 51-74-10 AND INSTALLED REPAIR ANGLE TO STRINGER 46R PER SRM 53-10-14-2. (M)
Part: FRAME — CORRODED (FUSELAGE)
TUL - FRAME C63 CORRODED FROM STRINGER 54L TO 54R. CUT OUT CORRODED AREA INSTALL FROM REPAIR PER SRM 53-10-13 PAGE 203. (M)
Part: SEAT TRACK — CORRODED (CABIN)
TUL - SEPARATE AREAS OF CORROSION ON TRACK 8 FROM FRAME 25-32. REMOVED AND REPLACED SECTION OF TRACK NR 8 FROM FRAME 26-33 PER SRM 51-72-10-0. (M)
Part: SEAT TRACK — CORRODED (CABIN)
TUL - SEAT TRACK HAS CORROSION AROUND BOLT HOLES BETWEEN FRAME 28 AND 29. REMOVED AND REPLACED SEAT TRACK SECTION FROM FRAME 26 TO 29 PER SRM 51-72-10-0. (M)
Part: SEAT TRACK — CORRODED (CABIN)
TUL - SEPARATE AREAS ALONG TRACK CORROSION 8A BEYOND LIMITS. REMOVED AND REPLACED SECTION OF TRACK 8A FROM 26 TO 29, REF SRM 51-72-10-0. (M)
Part: SEAT TRACK — CORRODED (CABIN)
TUL - SEAT TRACK NR 10 HAS CORROSION FROM FRAMES 26 TO 33. REMOVED AND REPLACED SEAT TRACK FROM FRAMES 26 TO 33 PER SRM 52-10-0. (M)
Part: FLOORBEAM — CORRODED (CABIN)
TUL - FLOORBEAM CORRODED AT FROM C69 IN RIGHT TOP CORNER. REPLACED SECTION OF FLOORBEAM PER SRM 53-10-15. (M)
Part: FRAME — CORRODED (CARGO COMPT)
TUL - FRAME C64 CORRODED FROM STRINGER 54L TO 54R. CUT OUT CORRODED AREA INSTALLED FROM REPAIR PER SRM 53-10-15 PAGE 203. (M)
Part: FLOORBEAM — CORRODED (CABIN)
TUL - FLOORBEAM SEAT TRACK NR 3 HAS CORROSION AT LAVATORY L FRAME 29-32. REMOVED AND REPLACED BEAM SRM 53-10-00. (M)
Part: SUPPORT — CORRODED (CABIN)
TUL - FOUND FLOOR SUPPORT TRACK 2A HAS SMALL AREA OF CORROSION. REMOVED AND REPLACED FLOOR SUPPORT TRACK 2A PER SRM 51-72-10. (M)
1996
Part: CONNECTOR — LOOSE (CABIN)
SJU - DURING OVERNIGHT CHECK, EMERGENCY POWER SUPPLY FOR EXIT LIGHTS AT L4 DOOR DID NOT TEST. RESEATED CANNON PLUG ON EMERGENCY POWER SUPPLY UNIT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1995
Part: RELIEF VALVE — DEFECTIVE (ACM COMPT)
TUL - FLT 9186 - DURING FUNCTIONAL AT FL 370 - AMBER SAFETY VALVE INDICATED OPEN AND CABIN ALTITUDE BEGAN TO CLIMB. NR 1 PRESSURE REGULATOR FAULTED. MANUALLY SWITCHED TO NR 2 REGULATOR AND REGAINED CONTROL OF CABIN PRESSURIZATION. ACCOMPLISHED EMERGENCY DESCENT AND AIRCRAFT LANDED TUL WITHOUT INCIDENT. REPLACED NR 2 SAFETY RELIEF VALVE. REPLACED NR 1 AND NR 2 CABIN PRESSURIZATION CONTROLLERS. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)