N14053
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
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.
62 reports on file, 1995-05-17 – 2001-05-09.
Part: FRAME — CORRODED (FUSELAGE)
TUL - FOUND FRAME 18 STRINGER 53R TO STRINGER 52R SHEAR TIE CORRODED, 3 INCHES BY 2 INCHES. INSTALLED NEW FRAME SECTION PER SRM 51-72-10. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND CORROSION ON STRINGER 53 RIGHT OUTBOARD OF ELECTRICAL POWER BOX, FS 1336, 3 INCHES BY 1 INCH. INSTALLED NEW STRINGER PER SRM 51-72-10. (M)
Part: FRAME — CORRODED (FUSELAGE)
TUL - FOUND FRAME 18 STRINGER 50R TO 49R CORROSION ON SHEAR TIE, FS 1336. INSTALLED NEW FRAME SECTION FRAME 18 STRINGER 50R TO 49R PER SRM 51-72-10. (M)
Part: STRINGER CLIP — CORRODED (FUSELAGE)
TUL - FOUND FRAME 18 STRINGER 51R STRINGER CLIP IS CORRODED, FS 1336. INSTALLED NEW STRINGER CLIP AT FRAME 18 STRINGER 51R PER SRM 51-72-10. (M)
Part: FRAME — CORRODED (FUSELAGE)
TUL - FOUND FRAME 18 STRINGER 52R TO 51R HAS CORROSION ON SHEAR TIE, 1 INCH BY 2 INCHES, BS 1336. INSTALLED NEW FRAME SECTION PER SRM 51-72-10. (M)
Part: FRAME — CORRODED (FUSELAGE)
TUL - FOUND FRAME 18, STRINGER 54R TO 54L HAS CORROSION ON SHEAR TIE. INSTALLED NEW FRAME SECTION PER SRM 51-72-10. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND FRAME 18 TO FRAME 19 STRINGER 53R IS CORRODED, 2 INCHES BY 1 INCH. INSTALLED NEW STRINGER AT FRAME 18 TO FRAME 19 PER SRM 51-72-10. (M)
Part: FRAME — CORRODED (FUSELAGE)
TUL - FOUND FRAME 18 STRINGER 54R TO 53R SHEAR TIE CORRODED. INSTALLED NEW FRAME SECTION PER SRM 51-72-10. (M)
Part: STRINGER CLIP — CORRODED (FUSELAGE)
TUL - FOUND FRAME 18 STRINGER 52R STRINGER CLIP IS CORRODED. INSTALLED NEW STRINGER CLIP AT FRAME 18 STRINGER 52R PER SRM 51-72-10. (M)
Part: FRAME — CORRODED (FUSELAGE)
TUL - FOUND FRAME 18 STRINGER 51R TO 50R, CORRODED ON SHEAR TIE, BS 1336. INSTALLED NEW FRAME SECTION PER SRM 51-72-10. (M)
Part: SKIN — CORRODED (FUSELAGE)
TUL - FOUND AREA OF LOWER FUSELAGE SKIN BULGED APPROX 1.5 SQUARE INCHES LOCATED BETWEEN FS 18-19 OF THE NOSE GEAR CUTOUT AFT DOUBLER, LEFT FINGER CORROSION IS AT PREVIOUS REPAIR EDGE. AREA REPAIRED PER ESO 30595 DATED 5/8/2001. (M)
Part: LIGHT — INOPERATIVE (R3 DOOR)
JFK - DURING OVERNIGHT MAINTENANCE, OVERHEAD R3 DOOR EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY AT R3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Earlier reports · 1995–2000 · 50 reports
2000
Part: CONNECTOR — UNSECURE (CABIN SEAT)
JFK - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 3G INOPERATIVE. RESECURED PIN CONNECTOR FOR SEAT 3G EMERGENCY EXIT LIGHT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: FLASHLIGHT — INOPERATIVE (CABIN)
MIA - DURING OVERNIGHT MAINTENANCE EMERGENCY FLASHLIGHT AT 4R DOOR INOPERATIVE. REPLACED EMERGENCY FLASHLIGHT. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: TRANSMITTER — LEAKING (HYDRAULIC SYS)
MCO - FLT 915 - DURING FLIGHT, GREEN HYDRAULIC SYSTEM LEAKING. DIVERTED AND LANDED MCO WITHOUT INCIDENT. REPLACED HYDRAULIC PRESSURE TRANSMITTER. SYSTEM GROUND CHECK NORMAL OPERATION. (M)
Part: STRINGER — CORRODED (BS 34 TO 36)
TUL - STRINGER CORRODED. SPLICED IN NEW SECTION PER ESO 30595 DATED 1-5-00 FROM FR 34 TO FR 36. TST: 3,224.11 HOURS. CYCLES: 12,979. (X)
Part: SHEAR TIE — CORRODED (BS 36)
TUL - CORROSION FROM STR 49L TO STR 50L AT FRAME 36. ALODINED, PRIMED, AND PAINTED PER SRM 51-74-10. INSTALLED NEW SHEARTIE PER SRM 51-72-10. TST: 32,241 HOURS. CYCLES: 12,979. (X)
Part: SHEAR TIE — CORRODED (BS 35)
TUL - CORROSION ON SHEAR TIE BETWEEN 50L AND 51L AT FRAME 35. REMOVED CORROSION PER SRM 51-74-10. ALODINED, PRIMED, AND PAINTED PER SRM 51-74-10. INSTALLED NEW SHEAR TIE PER SRM 51-72-10. TST: 32,241 HOURS. CYCLES: 12,979. (X)
1999
Part: SKIN — CORRODED (BS 32-33)
TUL - SKIN UNDER ANTENNA CORRODED. INSTALLED DOUBLER PER SRM 53-10-12. TST: 32,241.11 HOURS. CYCLES: 12,979. (X)
Part: LAVATORY TRACK — CORRODED (BS 30-31)
TUL - CORROSION ON LAVATORY SUPPORT IKNBOARD FLANGE BRACKET TRACK B ANC C LEFT SIDE BETWEEN FRAMES 30 AND 31. INSTALLED NEW LAVATORY SUPPORT TRACK PER SRM 51-72-10-0. TST: 32,241.11 HOURS. CYCLES: 12,979. (X)
Part: FLOORBEAM — CORRODED (BS 75-80)
TUL - NUMEROUS SPOTS OF CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 75 AND 80 ON FLOOR TRACK E, RIGHT. INSTALLED NEW FLOOR TRACK E RIGHT, PER SRM 51-72-10-0. TST: 32,241.11 HOURS. CYCLES: 12,979. P/N A53278453200. (X)
Part: FLOORBEAM — CORRODED (BS 4862)
TUL - NUMEROUS SPOTS OF CORROSION ON FLOOR SUPPORT BETWEEN FRAMES 76 AND 82 ON FLOOR TRACK E LEFT. INSTALLED NEW FLOOR TRAK E LEFT, CPN 4035847 PER SRM 51-72-10-0. TST: 32,291.11 HOURS. CYCLES: 12,979. (X)
Part: FLOORBEEAM — CORRODED (BS 4574)
TUL - CORROSION ON FLOOR SUPPORT BETWEEN SEAT TRACKS 'E' RIGHT AND 'D' RIGHT, LOCATED BETWEEN FRAMES 71 1/2 AND 74. REMOVED AND REPLACED FLOOR SUPPORT FROM FRAME 71 1/2 TO FRAME 74 BETWEEN TRACK 'E' RIGHT, AND 'D' RIGHT PER SRM 51-72-10-0. ALODINED, PRIMED, PAINTED PER SRM 51-21-00. TST: 32,241.11 HOURS. CYCLES: 12,979. (X)
Part: ACM — DEFECTIVE (ACM BAY)
KIN - FLT 628 - AFTER TAKEOFF KIN EN ROUTE TO MIA, SMOKE AND FUMES WERE NOTED IN COCKPIT. AIRCRAFT RETURNED TO KIN AND LANDED WITHOUT INCIDENT. REPLACED NR 1 AIR CONDITIONING PACK ACM. ALSO, REPLACED NR 1 AIR CONDITIONING PACK FLOW CONTROL VALVE AS PRECAUTIONARY MEASURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1998
Part: SKIN — CORRODED (RT WING)
TUL - FOUND RIGHT WING LOWER SURFACE AFT AND OUTBOARD OF NR 2 ENGINE PYLON HAS CORROSION TWO AREAS. REMOVED CORROSION, INSTALLED INTERAL DOUBLER REPAIR PER ESO 30595, DATED 9-24-98. (M)
1997
Part: STRINGER — CORRODED (FUSELAGE)
TUL - STR 52R HAS SURFACE CORROSION AT FRAME 54.1 FORWARD SIDE. REPAIRED PER ESO 30595 DATED 12-18-97. TST: 26,718.41 HOURS. CYCLES: 10,861. (X)
Part: SEAT TRACK — CORRODED (BS 1976)
TUL - FOUND CORROSION ON NR 3 SEAT TRACK. INSTALLED NEW SEAT TRACK PER SRM 51-72-10-0. (M)
Part: SUPPORT — CORRODED (RT LE FLAP ACT)
TUL - CORROSION ON OUTBOARD SHELF FOR RT KRUEGER FLAP ACT. REMOVED AND REPLACED SUPPORT PER SRM 57-45-11-0 PAGE 2 ITEM 20. TST: 26,718.41 HOURS. CYLES: 10,861. (X)
Part: FRAME — CORRODED (BS 572)
TUL - BELL FRAME CORRODED AT STATION 57.2 FRONG AND BACK SIDE BETWEEN STRINGER 55R AND 55L. REPAIRED BELL FRAME PER SRM 53-10-13 ALODINED PRIMED AND PAINTED PER SRM 51-75-10. (M)
Part: FRAME — CORRODED (FUSELAGE)
TUL - BELLFRAME AT FRAME STATION 60 HAS CORROSION ON AFT SIDE. INSTALLED DOUBLER AS PER SRM 53-10-13. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - STRINGER 49R HAS CORROSION AT FRAME STATION 60 ON FORWARD SIDE. INSTALLED DOUBLER AND FILLER AS PER SRM 53-10-14 WHERE CORRODED SECTION OF LONGERON REMOVED. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - STRINGER 49L HAS CORROSION FORWARD SIDE AT STATION FRAME 59. REPAIRED STRINGER PER SRM 53-10-14 PAGE 203-204. ALODINED, PRIMED AND PAINTED PER SRM 51-25-10. (M)
Part: BEAM — CORRODED (RT TE FLAP)
TUL - RIGHT KRUGER FLAP ACT CROSSBEAM HAS CORROSION ON BEAM. REMOVED AND REPLACED CROSSBEAM PER SRM 57-45-11 PAGE 2 ITEM NR 5. (M)
Part: ROLLER TRAY — CORRODED (CARGO COMPT)
TUL - FOUND CORROSION ON NR 3 ROLLER TRAY. REPLACED NR 3 ROLLER TRAY BETWEEN FRAMES 30 TO 32 PER SRM 53-10-15. (M)
Part: ROLLER TRAY — CORRODED (CARGO COMPT)
TUL - FOUND CORROSION ON OUTBOARD SIDE OF ROLLER TRAY, FORWARD CARGO NR 1 TRAY LEFT SIDE OF A/C. INSTALLED NEW SECTION OF ROLLER TRAY, NR 1 LEFT SIDE OF FWD CARGO BETWEEN FRAMES 27 TO 31, PR 53-10-15. (M)
Part: SUPPORT — CORRODED (RT WING)
TUL - RIGHT WING LE SUPPORT HAS CORROSION. REPAIRED PER ESO30595, DATED 12-12-97. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - FOUND CORROSION ON STRINGER 48 LEFT. REPLACED SECTION OF STRINGER AT FRAMES 70 AND 71, STRINGER 48L PER SRM 51-72-10. (M)
Part: STRINGER — CORRODED (FUSELAGE)
TUL - TOP OF STRINGER HAS CORROSION ON IT STRINGER 54 FROM FRAME 19 TO 20. INSTALLED STRINGER REPAIR PER SRM 53-10-14 PAGE 203 AND 204. (M)
Part: SUPPORT — CORRODED (FUSELAGE)
TUL - FOUND CORROSION ALONG SUPPORT AT SEVERAL PLACES BETWEEN FRAME 60-63. REMOVED AND REPLACED FRAME SUPPORT FROM FRAME 59-64 PER SRM 53-10-14. (M)
Part: INTERCOSTAL — CORRODED (CARGO COMPT)
TUL - FOUND CORROSION ON INTERCOSTAL RT SIDE CARGO COMPT. REMOVED CORROSION AND INSTALLED DOUBLER PER SRM 51-71-30. (M)
Part: FRAME — CORRODED (CARGO COMPT)
TUL - HEAVY CORROSION ON FRAME NR 25 UNDER ROLLER TRAY NR 3. INSTALLED NEW TOP CAP BEAM SECTION AS PE SRM 53-10-15. (M)
Part: BRACKET — CORRODED (RT WING)
TUL - SWITCH BRACKET A5351094120000 CORRODED IN KRUEGER WELL. REMOVED CORRODED BRACKET AND INSTALLED NEW SWITCH BRACKET PER A360 SRM 51-72-10. (X)
Part: MOUNT — CORRODED (LE FLAP)
TUL - KRUEGER FLAP OUTBOARD CARRIER MOUNT CORRODED. REMOVED OUTBOARD CARRIER MOUNT. REPLACED WITH NEW MOUNT. A-300 MM 27-87-14-4. TST: 26,718.41 HOURS. CYCLES: 10,861. (X)
Part: SUPPORT — CORRODED (CARGO COMPT)
TUL - FOUND CORROSION ON 'T' ANGLE SUPPORT UNDER NR 1 ROLLER TRAY. SPLICED IN NEW TOP CAP PER SRM 53-10-15, ALODINE, PAINT PER SRM 51-75-10. (M)
Part: SEAT TRACK — CORRODED (BS 1764)
TUL - FOUND CORROSION ON NR 8 SEAT TRACK. INSTALLED NEW SEAT TRACK PER SRM 51-72-10-0. INSTALLED NEW SEAT TRACK PER SRM 51-72-10-0. (M)
Part: TIE DOWN TRACK — CORRODED (BS 2029)
TUL - FOUND CORROSION ON TIE DOWN TRACK BETWEEN SEAT TRACKS 8 AND 9. INSTALLED NEW TRACK PER 51-72-10-0 SRM. (M)
Part: SEAT TRACK — CORRODED (BS 2082)
TUL - FOUND CORROSION ON NR 8 SEAT TRACK. INSTALLED NEW SEAT TRACK PER SRM 51-72-10-0. (M)
Part: SUPPORT — CORRODED (CARGO COMPT)
TUL - ROLLER TRAY SUPPORT AT NR 6 TRAY IS CORRODED. REPAIRED ROLLER TRAY SUPPORT PR SRM 53-10-15. (M)
Part: SEAT TRACK — CORRODED (BS 1208)
TUL - FOUND CORROSION ON NR 7 SEAT TRACK. REPAIRED PER AARD 53-20-00-2 BY INSTALLING STRAP. (M)
Part: SUPPORT — CORRODED (BS 1091)
TUL - FOUND CORROSION ON SUPPORT AT 'A' LAV. REPLACED SUPPORT PER SRM 51-72-10. (M)
Part: BEAM — CORRODED (BS 1161)
TUL - FOUND CORROSION ON BEAM BETWEEN SEAT TRACKS 8 AND 9. REPLACED BEAM PER SRM 51-72-10. (M)
Part: ROLLER TRAY — CORRODED (CARGO COMPT)
TUL - FOUND CORROSION ON NR 3 ROLLER TRAY. CUT OUT CORROSION, INSTALLED DOUBLER PER SRM 53-10-15. (M)
Part: STRUCTURE — CORRODED (FUSELAGE FLOOR)
TUL - FOUND CORROSION ON FLOOR SUPPORT STRUCTURE. REMOVED SUPPORT AND REPLACED PER SRM 51-74-10-2. (M)
Part: CONNECTOR — LOOSE (CABIN)
JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PAX SEAT ROWS 25H THROUGH 29H AND 23B THROUGH 25B INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 25H AND REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR BY PAX SEAT ROW 23B. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
1996
Part: ACM — DEFECTIVE (NR 2 ACM BAY)
MIA - FLT 1901 - AFTER TAKEOFF MIA DURING CLIMB-OUT, AIR CYCLE MACHINE NR 2 FAILED AND PRODUCED SMOKE IN CABIN. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 2 AIR CYCLE MACHINE, RIGHT PACK TURBINE BYPASS VALVE, SENSE LINE AND REPLACED COALESCER BAG. ACCOMPLISHED PACK BURNOUT PROCEDURE. SYSTEM GROUND CHECKED NORMAL OPERATION WITH NO SMOKE OR ODOR NOTED. (M)
Part: CONNECTOR — DEFECTIVE (CABIN)
JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN L3 AND R3 DOORS INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT L3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — BROKEN (CABIN)
JFK - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT CROSS AISLE BETWEEN L3 AND R3 DOOR AND AT RIGHT AISLE JUST FORWARD OF R3 DOOR INOPERATIVE. REPLACED BROKEN EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT CROSS AISLE BETWEEN L3 AND R3 DOOR AND REPLACED BROKEN POWER FEED WIRE AT RIGHT AISLE JUST FORWARD OF R3 DOOR. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: CONNECTOR — LOOSE (CABIN)
MIA - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS AT LEFT AISLE IN AFT SECTION OF MAIN CABIN INOPERATIVE. RESECURED LOOSE EMERGENCY FLOOR LIGHT STRIP CONNECTOR AT LEFT AISLE IN AFT SECTION OF MAIN CABIN. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: ATTACH SECTION — CORRODED (FUSELAGE)
TUL - CORRODED ALONG LENGTH. REPLACED ATTACH SECTION PER SRM 51-72-10. TST: 21,713 HRS. CYCLES, 8,831. (X)
Part: ATTACH SECTION — CORRODED (FUSELAGE)
TUL - ATTACH SECTION CORRODED BEYOND MM (SRM) LIMITS. REPLACED ATTACH SECTION PER SRM 51-72-10. TST: 21,713 HRS. CYCLES, 8,831. (X)
1995
Part: TRANS/RECTIFIER — DEFECTIVE (NR 2 POSITION)
MIA - FLT NR 0916 - AFTER TAKEOFF BOG DURING CLIMB-OUT, ECAM ADVISORY ELECTRICAL DC PAGE TRANSFORMER RECTIFIER 2 SHOWED 31 VOLTS AND ZERO AMPS. ORANGE LINE TO NORMAL DC BUS AND BURNING ODOR NOTED COCKPIT. AIRCRAFT PROCEEDED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED NR 2 TRANSFORMER RECTIFIER. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)
Part: COALESCER — CONTAMINATED (LT ACM)
MIA - FLT 1815 - AFTER TAKEOFF DURING CLIMB-OUT, ODOR NOTED IN CABIN AND COCKPIT. AIRCRAFT RETURNED TO MIA AND LANDED WITHOUT INCIDENT. REPLACED LEFT AND RT COALESCER BAGS DUE TO LEFT BAG CONTAMINATED WITH HYDRAULIC FLUID. CLEANED HYDRAULIC FLUID RESIDUE FROM WHEEL WELL AREA. NO HYDRAULIC LEAKS NOTED. ACCOMPLISHED PACK BURNOUT PROCEDURE. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)