# N112FE: 1968 Boeing 727-22C, registration cancelled 2003-08-22

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: August 22, 2003
- Exported to: Canada
- Status when cancelled: Triennial form not returned
- Airframe: [Boeing 727-22C](https://openairdocs.org/model/boeing-727-22c) (registry code 138400F)
- Serial number: 19890
- Year built: 1968
- Type of aircraft: Fixed wing multi engine
- Airworthiness: Standard, transport
- Airworthiness date: September 12, 1968
- Certificate issued: October 11, 1979
- Last registry action: September 19, 2000
- Mode S code: A03423
- Owner when cancelled: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- Location: [Memphis, TN](https://openairdocs.org/faa-place/TN/Memphis)
- Owner type: Corporation
- Owner's area on the map: 35.0351° N, 89.9272° W: Placed by OpenAirDocs at the center of ZIP code 38118, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N112FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=112FE
- Page: https://openairdocs.org/deregistered/N112FE-2003-08-22

From the FAA registry file of October 28, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Boeing 727-22C: https://openairdocs.org/model/boeing-727-22c.md

## Service difficulty reports (25)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR 01FDEA00349](https://openairdocs.org/sdr/01FDEA00349), May 15, 2001: SWITCH. INOPERATIVE. 01-155 ON DEPART WHEN FLAP 2 DEG SEL ON RETRACTION LIGHT ON FWD PNL FLAP/SLAT IND REMAIN AMBER. FND L/E FLAP OVERRIDE TEST SWITCH IN OVERRIDE POS, RETURN TO NOR
- [SDR 00FDEA00838](https://openairdocs.org/sdr/00FDEA00838), Dec 2, 2000: DOWNLOCK SWITCH. FAILED. 00-333 NOSE GEAR DOWN LIGHT DID NOT ILLUMINATE WHEN MAINS CAME DOWN. R&R NOSE GEAR DOWN LOCK SWITCH PER MM 32-61-21. REMOVED GEAR PIN FOR FLIGHT. OPS CK NORMAL.
- [SDR 00FDEA00157](https://openairdocs.org/sdr/00FDEA00157), Mar 15, 2000: VALVE. FAILED. 00-87 - FUEL HEAT VALVE FAIL NR 1 ENGINE THEN OIL TEMP YELLOW ARC UNDER 15 MIN. REMOVED AND REPLACED VALVE PER 73-14-011-4. OPERATIONAL NORMAL.
- [SDR 00FDEA00032](https://openairdocs.org/sdr/00FDEA00032), Jan 25, 2000: LIGHT. MALFUNCTIONED. 00-19 - AFT RAISING LG 2 MIN WITH GEAR HANDLE OFF POS THE LMG DOOR LIGHT ILLUM. REMOVED AND REPLACED LMLG DOOR ACTUATOR PER MM 32-32-081. PERF GEAR EXT AND RETR
- [SDR 99FDEA00330](https://openairdocs.org/sdr/99FDEA00330), Aug 12, 1999: ACCESSORY UNIT. INOP. RETRACTION REPEAT GEAR WARN LIGHT PROBLEMS. SYMPTOMS INDENTICAL TO ARD REPORT ON 8/11/99. REMOVED AND REPLACED LAND GEAR ASSY UNIT PER MM 32-09-111-5 PG 1-5 GRO
- [SDR 99FDEA00327](https://openairdocs.org/sdr/99FDEA00327), Aug 11, 1999: ACCESSORY UNIT. INOP. 99-203 REPEAT, 3 GEAR RED INTRANSIT LIGHTS WOULD NOT EXTINGUISH AFT RAISING GEAR HANDLE TO UP FLT ENGINE DOOR ANNUNCIATOR PNL NORM. REMOVED AND REPLACED LANDING
- [SDR 99FDEA00325](https://openairdocs.org/sdr/99FDEA00325), Aug 11, 1999: ACCESSORY UNIT. INOP. 99-201 - AFT RAISING LAND GEAR HANDLE ALL 3 UNSAFE RED LIGHTS REMAIN ON. RERACKED LAND GEAR ACCESSORY UNIT, CYCLED LT MLG DOWNLOCK SWITCH, OPS CK NORM PER 727-1
- [SDR 99FDEA00289](https://openairdocs.org/sdr/99FDEA00289), Jul 28, 1999: SWITCH. FAILED. 99-174 - NR 3 ENGINE LOW OIL PRESS/FILTER BYPASS LIGHT CAME ON. ENG SHUTDOWN ACCOMPLISHED. REPLACED NR 3 ENG OIL FILTER BYPASS SWITCH PER MM 79-33-000-0. REPLAC
- [SDR 98FDEA00694](https://openairdocs.org/sdr/98FDEA00694), Nov 10, 1998: C1 DISK. BIRD STRIKE. AFT V1 AND BEFORE ROTATION NR 1 ENG GAVE A LOUD BANG AND APPEARED TO COMPRESSOR STALL, FOLLOWED BY A SMELL COMING FROM THE PACK A/C LEFT HAND. IN WORK AT THIS T
- [SDR 98FDEA00669](https://openairdocs.org/sdr/98FDEA00669), Oct 23, 1998: ACCESSORY UNIT. MALFUNCTIONED. 98-258 - AFTER GEAR HANDLE RAISED UP RIGHT MAIN GEAR INDICATED DOWN AND LOCKED. REMOVED AND REPLACED LAND GEAR ANNUNCIATOR PANEL DUE TO POSS OF PWR MM 33-10-00.
- [SDR 98FDEA00667](https://openairdocs.org/sdr/98FDEA00667), Oct 22, 1998: PROX UNIT. INOP. 98-25 - WHEN GEAR HANDLE RAISED, RT MAIN GEAR IND DOWN (GREEN LIGHT) AND RED TRANSIT LIGHT WAS ILLUM. RECYCLED GEAR IN ACCORD WITH EMER PROC, NO HELP. RETURN TO
- [SDR 97FDEA00699](https://openairdocs.org/sdr/97FDEA00699), Oct 2, 1997: DOWNLOCK SWITCH. FAILED. 97-0193 ON FINAL APPROACH, NOSE GEAR LIGHT WAS ON, WENT OUT WITH FLAPS 30. (GOT WARNING HORN), AND THEN CAME BACK ON GREEN. WENT AROUND, CYCLED GEAR, CHECKED SA
- [SDR 97FDEA00443](https://openairdocs.org/sdr/97FDEA00443), Jul 17, 1997: ENGINE. MALFUNCTIONED. 97-0134 AT T/O CREW FELT SLIGHT YAW AND OBSERVED NR 1 EPR DROP TO 1.4 ALL OTHER ENG IND REMAIN WITHIN LIMITS ALTHOUGH EGT WAS HIGHER THAN NORM. ENG WAS NEVER SH
- [SDR 95FDEA01807](https://openairdocs.org/sdr/95FDEA01807), Nov 27, 1995: FITTING. CRACKED. BS 870 LT TERMINAL FITTING LOWER HOLE NR 4 SHOWS CRACK WITH A HFEC AT STR 9 TO 10. STOP DRILLED CRACK, FABRICATED REPAIR PARTS AND DOUBLER IAW 727-53-0194 BOEIN
- [SDR 95FDEA01806](https://openairdocs.org/sdr/95FDEA01806), Nov 27, 1995: FLOORBEAM. CORRODED. HEAVY CORROSION ON FLOORBEAM STA 560 LBL 0 TO 22. REMOVED CORROSION, FABRICATED REPAIR PIECES IAW 53-10-8, INSTALLED REPAIR PIECES, DOUBLER AND FASTENERS PER 53
- [SDR 95FDEA01805](https://openairdocs.org/sdr/95FDEA01805), Nov 27, 1995: FLOORBEAM. CORRODED. STA 600 RBL 60 TO 41 WL 208.1 FLOORBEAM HAS CORROSION ON UPPER AND LWR LANDING. REMOVED TOP FLANGE OF FLOORBEAM RBL 44 TO 56 PER SRM 53-10-8 FIG 5 AND FABRICATE
- [SDR 95FDEA01804](https://openairdocs.org/sdr/95FDEA01804), Nov 27, 1995: CLIP. CORRODED. WING TEE CLIP STA 760 RBL 665 HAS CORROSION. REMOVED CORRODED TEE CLIP, COLD WORKED HOLES PER EO 7-5710-7-2308 AND INSTALLED TEE CLIP.
- [SDR 95FDEA01803](https://openairdocs.org/sdr/95FDEA01803), Nov 27, 1995: FLOORBEAM. CORRODED. FLOORBEAM HAS CORROSION STA 680 LBL 50 TO 55. CUT AWAY CORRODED AREA FABRICATED REPAIR PARTS AND INSTALLED PER SRM 53-10-8.
- [SDR 95FDEA01809](https://openairdocs.org/sdr/95FDEA01809), Nov 26, 1995: FITTING. CRACKED. SEVERAL STR END FITTINGS AT STA 870 AND 740 CRACKED ON INNER LANDING STR 8R AND L MPN'S 69-16380-3 AND 69-34593-1. REMOVED AND REPLACED END FITTINGS PER STANDAR
- [SDR 95FDEA01808](https://openairdocs.org/sdr/95FDEA01808), Nov 26, 1995: FRAME. CRACKED. BS 804.5 LT SIDE 23 ABOVE WL 208.1 STR 14 FRAME CRACKED. STOP DRILLED CRACK AND INSTALLED DOUBLER PER 51-40-3.
- [SDR 95FDEA01699](https://openairdocs.org/sdr/95FDEA01699), Nov 8, 1995: FITTINGS. CRACKED. SEVERAL STRINGER END FITTINGS AT STA 870 TO 740 CRACKED ON INNER LANDING STR 8 RT AND LT MPN'S 69-16380-3 AND 69-34593-1.
- [SDR 95FDEA01693](https://openairdocs.org/sdr/95FDEA01693), Nov 7, 1995: FLOORBEAM. CORRODED. FLOORBEAM STA 640 LBL 53 HAS CORROSION.
- [SDR 95FDEA01692](https://openairdocs.org/sdr/95FDEA01692), Nov 7, 1995: FLOORBEAM. CORRODED. CORROSION ON FLOORBEAM STA 640 RBL 21 TO 58.
- [SDR 95FDEA01691](https://openairdocs.org/sdr/95FDEA01691), Nov 7, 1995: FLOORBEAM. CORRODED. FLOORBEAM HAS CORROSION STA 680 LBL 50 TO 55.
- [SDR 95FDEA01690](https://openairdocs.org/sdr/95FDEA01690), Nov 7, 1995: CLIP. CORRODED. WING TOE CLIP STA 760 LBL 65 HAS CORROSION.

## FAA accident and incident reports (2)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 19990727018109I](https://openairdocs.org/incident/19990727018109I), Jul 27, 1999: Boeing 72722C (N112FE), Ontario, CA. (-5)During climb out at approximately 9000 feet, the #3 engine low oil pressure/filter bypass light came on. The engine oil pressure and temperature were…
- [Incident 19990325002629I](https://openairdocs.org/incident/19990325002629I), Mar 25, 1999: Boeing 72722C (N112FE), Grand Forks, ND, Minor damage. Federal express cargo acft experienced an engine failure while taxiing for take-off, the pilot aborted take-off, the acft sustained substantial engine damage,…

## Other aircraft with N112FE

- [Registered now](https://openairdocs.org/aircraft/N112FE): Boeing 767-3S2F, S/N 43543, built 2015

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