N132DN
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.
19 reports on file, 1995-10-10 – 2008-04-09.
Part: COFFEEMAKER — INOPERATIVE (AFT 4 GALLEY) · airframe 54,553 hrs · 25,073 cycles
AFT GALLEY NR 4 COFFEEMAKER INOP. HEATING ELEMENT FOR POT WARMER BROKEN CAUSING IT TO SMOKE. REMOVED AND REPLACED COFFEEMAKER.
Earlier reports · 1995–2007 · 18 reports
2007
Part: FITTING — CORRODED (TE FLAP) · airframe 52,715 hrs · 24,405 cycles
CORROSION IN BORE OF HOLES FOR NR 4 AND 5 FLAP SUPPORT ATTACHMENTS. BUSHINGS REPLACED.
Part: LINK — CORRODED (TE FLAPS) · airframe 52,715 hrs · 24,405 cycles
WORKING EA 01-073591-12 FOUND LEFT AND RIGHT INDBD AFT DRIVE LINK FLAP ATTACH BOLT HOLES CORRODED REPAIRED PER ERA089397-14MA.
Part: ENGINE — POWER LOSS (NR 1) · airframe 51,460 hrs · 24,022 cycles
WHILE IN CLIMB AND AT LEVEL 34K AND THROTTLING BACK TO CRZ POWER THE LEFT ENGINE HAD A LOUD POP WITH LOSS OF THRUST WITH ENGINE AT IDLE THERE WAS NO THROTTLE RESPONSE THEN THE ENGINE WAS SHUT DOWN BY THE PILOT. A/C RETURNED TO ATL AND LANDED SAFELY. NUMBER ONE ENGINE REPLACED PER TRANS 1T144.
Part: KEELBEAM — CRACKED (FS 1042 WL 157) · airframe 51,116 hrs · 23,883 cycles
THE KEEL BEAM AT FS 1402, WL 157 WAS FOUND WITH A VERTICAL CRACK JUST FORWARD OF THE STA 1043 STIFFENER. THE CRACKED AREA WAS CUT OUT AND A DOUBLER WAS INSTALLED.
2006
Part: ENGINE — OVERTEMP (NR 1) · airframe 49,584 hrs · 23,288 cycles
LEFT ENGINE HIGH EGT DURING TAKEOFF ROLL. MAX 941C. ABORTED T/O AT LAS. PERFORMED ENGINE OVERTEMP INSPECTION PER FIM 71-05-00 FIG 112. ENG INLET AND EXH INSP, NO DAMAGE FOUND.
2005
Part: BATTERY PACK — FAILED (EMERGENCY LIGHTS) · airframe 46,461 hrs · 22,079 cycles
WHILE TS 2R DOOR EXT EMERG LIGHT FOUND RT WING OVERWING EGRESS LIGHTS INOP AND LT SLIDE LIGHTS INOP ALSO FOUND 2L EXT EMERG LIGHT INOP. RELAMPED 2L EXT EMERG LIGHT OPS CKS OK REPLACED M731 AND M738 PWR SUPPLIES AND BATTERIES RT O WING EGRESS LIGHTS AND LT WING SLIDE LIGHTS CKS OK.
Part: SWITCH — BURNED (COCKPIT) · airframe 45,703 hrs · 21,794 cycles
RIGHT FWD FUEL BOOST PUMP SWITCH REMOVED AND EVIDENCE OF BURNING NOTED AND PLASTIC MELTED. REPLACED SWITCH AND REPAIRED WIRING.
Part: FAN — OVERHEATED (EQUIP EXHAUST) · airframe 45,029 hrs · 21,485 cycles
EICAS MESSAGE FWD EQUIP EXHAUST FAN DISPLAYED. FWD EQUIP EXHAUST ELEC SMELL, SLIGHT SMOKE ODOR DETECTED. ATL MTC REPLACED FWD EQUIP EXHAUST FAN. EQUIP COOLING CHECKS NORMAL.
Part: AXLE — BROKEN (RT MLG) · airframe 44,541 hrs · 21,272 cycles
NR 8 MAIN LANDING GEAR TIRE FOUND AT 30 DEGREE ANGLE UPON WALKAROUND INSP BY MTC, FOUND AXLE BROKEN. REPLACED SAME. REPAIRED WIRING HARNESS.
2004
Part: SKIN — LIGHTNING STRIKE (FUSELAGE) · airframe 42,919 hrs · 20,456 cycles
LIGHTNING STRIKE ON THE FUSELAGE SKIN AT STATION 564 AND STRINGER 3L. REPAIRED IAW ER/A 090627-14.
2003
Part: APU — LEAKING (APU BAY) · airframe 41,173 hrs · 19,522 cycles
ODOR OF HOT AIR CONDITIONING, SMOKE DETECTORS ALL OVER AIRCRAFT WENT OFF. DESCENDED FROM 410 TO 310 AND SMOKE/ODOR DISSIPATED. ALL SMOKE DETECTORS DISABLED. UPON ENTERING A/C ODOR OF BURNED OIL. INSPECTED ENGS, APU AND PACK BAY AREAS AND ALL NORMAL. SUSPECT RESIDUAL OIL IN DUCTS FROM APU OIL LEAK. REF LOG E729128 ITEM OO1. PERFORMED REMOVAL OF OIL CONTAMINATION FROM AIR CONDITIONING AND PNEUMATIC SYSTEMS PER M/M 21-00-21. NO ODOR PRESENT FROM APU AIR SOURCE. RAN PACKS FROM ENGINES, NO ODOR PRESENT. BURN ODOR GONE AND NO SMOKE EVER PRESENT. CHECKS NORMAL. ENABLED ALL SMOKE DETECTORS. CHECKS NORMAL.
2002
Part: THRUST REVERSER — MALFUNCTIONED (NR 2 ENGINE) · airframe 38,979 hrs · 18,440 cycles
RT THRUST REVERSER YELLOW LIGHT CAME ON ON TAKEOFF WITH NO THRUST REVERSER SELECTED. ABORTED T/O AT 90KTS. FWD MCO/PLAC PER MEL 78-36-01. RT THRUST REVERSER LOCKED OUT
Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 36,603 hrs · 17,277 cycles
TWO EMERGENCY LIGHTS INOP ON LEFT SIDE OF A/C AND ONE ON RIGHT SIDE, L-4, AFT OF LEFT WING AND FWD OF R-4. RELAMPED LIGHTS.
1998
Part: SKIN — CORRODED (BS 687)
FUSELAGE SKIN AT STA 687 WAS FOUND WITH CORROSION DAMAGE AT THE LT AIRFONE ANTENNA ATTACH POINT BETWEEN STR 35L AND 36L. REPAIRED PER ERA 331718-14.
Part: SKIN — CORRODED (BS 1197-1296)
FUSELAGE SKIN AT STA 1197 + 99 FOUND WITH CORROSION DAMAGE AT VHF ANTENNA ATTACH POINT BETWEEN STR 39L AND 39R. REPAIRED PER ERA 331730-14.
1996
Part: SKIN — DELAMINATED (NR 8 LE FLAP)
THE NR 8 L/E SLAT T/E WEDGE WAS FOUND WITH UPPER SKIN DELAMINATION. THE DELAMINATED AREA WAS TRIMMED OUT AND REPAIRED PER SRM 57-43-02, FIG 201.
Part: OVEN — SPARKING (FWD GALLEY)
NR 1 UPPER OVEN MADE A LOUD POP AND SPARKS FLEW WHEN TURNED ON. REPLACED OVEN.
1995
Part: FAN — FAILED (FLIGHT DECK)
ELECTRICAL OVERHEATING ODOR IN COCKPIT AT FL370 FOR APPROX 30 SECS. LATER, RT RECIRC FAN EICAS MSG ILLUMINATED. RT RECIRC FAN TO OFF POS. RT RECIRC FAN FAILED. REPLACED FAN, OPERATION NORMAL.