# N101FE: 1967 Boeing 727-22C, registration cancelled 2003-01-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: January 23, 2003 - Status when cancelled: Valid registration - Airframe: [Boeing 727-22C](https://openairdocs.org/model/boeing-727-22c) (registry code 138400F) - Engine: [Pratt & Whitney JT8D series](https://openairdocs.org/engine/pratt-whitney-jt8d-series) (registry code 52053) - Serial number: 19197 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: January 10, 1978 - Last registry action: January 23, 2003 - Mode S code: A008ED - Owner when cancelled: [First Union Commercial Corp](https://openairdocs.org/faa-owner/FIRST%20UNION%20COMMERCIAL%20CORP) - Location: [Winston Salem, NC](https://openairdocs.org/faa-place/NC/Winston%20Salem) - Owner type: Corporation - Owner's area on the map: 36.1108° N, 80.2004° W: Placed by OpenAirDocs at the center of ZIP code 27101, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N101FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=101FE - Page: https://openairdocs.org/deregistered/N101FE-2003-01-23 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 (16) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 01FDEA00973](https://openairdocs.org/sdr/01FDEA00973), Nov 9, 2001: LINKAGE. DEFECTIVE. LANDING GEAR FAILED TO RETRACT AFTER T/O. REMOVED AND REPLACED LANDING GEAR VALVE ACTUATING LINK PER AMM 32-31-00-5. TEST OK FOR SERVICE. - [SDR 00FDEA00378](https://openairdocs.org/sdr/00FDEA00378), Jun 5, 2000: SPAR. CRACKED. DURING ROUTINE INSPECTION, RIGHT I/B MIDFLAP REAR SPAR UPPER CHORD FOUND CRACKED AT WING BUTT LINE 120 UPPER ROW FWD FASTENER HOLE. REMOVED AND REPLACED PER IAW - [SDR 00FDEA00377](https://openairdocs.org/sdr/00FDEA00377), Jun 5, 2000: FLOORBEAM. CORRODED. DURING ROUTINE INSPECTION, FLOORBEAM BS 640 FOUND CORRODED BEYOND LIMITS 4 INCHES LEFT OF NR 4 SEAT TRACK. CUT OUT DAMAGED AREA, FAB AND INSTALLED REPAIR PER IA - [SDR 00FDEA00376](https://openairdocs.org/sdr/00FDEA00376), Jun 5, 2000: FLOORBEAM. CORRODED. DURING ROUTINE INSPECTION, FLOORBEAM BS 344 FOUND CORRODED BEYOND LIMITS ON UPPER CHORD AT RBL 50. CUT OUT DAMAGE, FAB AND INSTALL PER IAW SRM 53-10-8. - [SDR 00FDEA00375](https://openairdocs.org/sdr/00FDEA00375), Jun 5, 2000: FLOORBEAM. CORRODED. DURING ROUTINE INSPECTION, FLOORBEAM BS 344, RT O/B END FOUND CORRODED BEYOND LIMITS ON LWR FLANGE. CUT OUT DAMAGE. FAB AND INSTALLED PER IAW SRM 53-10-8. - [SDR 00FDEA00374](https://openairdocs.org/sdr/00FDEA00374), Jun 5, 2000: STRINGER. CRACKED. DURING ROUTINE INSPECTION, STR 25R FOUND CRACKED BS 520. STOP DRILLED CRACK, FAB AND INSTALLED REPAIR PER IAW SRM 53-10-3. - [SDR 00FDEA00373](https://openairdocs.org/sdr/00FDEA00373), Jun 5, 2000: FLOORBEAM. CRACKED. DURING ROUTINE INSPECTION, LWR FLOORBEAM CORROSION AT BS 848 FROM RBL 0 - 24 AND CRACKED AT RBL 1. REMOVED CORROSION IAW SRM 51-10-6, STOP DRILLED CRACK. FABRIC - [SDR 00FDEA00372](https://openairdocs.org/sdr/00FDEA00372), Jun 5, 2000: SEAT TRACK. CORRODED. DURING ROUTINE INSPECTION, BS 870 FLOORBEAM FOUND CORRODED AT THE NR 1 SEAT TRACK. REMOVED AND REPLACED PER IAW SRM 51-10-6. FOUND WITHIN LIMITS IAW SRM 53-10-1 - [SDR 00FDEA00371](https://openairdocs.org/sdr/00FDEA00371), Jun 5, 2000: SKIN. CORRODED. DURING ROUTINE INSPECTION UPPER FUSELAGE SKIN FOUND CORRODED AND POPPED RIVETS FROM BS 430 - 440 AT STR 5L. REMOVED RIVET AND TRIMMED OUT DAMAGED AREA IAW SRM 5 - [SDR 00FDEA00370](https://openairdocs.org/sdr/00FDEA00370), Jun 5, 2000: SUPPORT BRACKET. CRACKED. DURING ROUTINE INSPECTION, SUPPORT BRACKET FOR NR 7 SPOILER ACTUATOR FOUND CRACKED AT BOTH SIDES. REMOVED AND REPLACED NR 7 SPOILER AND ACTUATOR FITTING PER IAW - [SDR 00FDEA00369](https://openairdocs.org/sdr/00FDEA00369), Jun 5, 2000: BELTFRAME. CRACKED. DURING ROUTINE INSP BS 930 BELTFRAME FOUND CRACKED ON FWD SIDE OF STR 14R. REPAIRED BELTFRAME PER IAW FEDEX EO 7-2310-7-4330. - [SDR 00FDEA00368](https://openairdocs.org/sdr/00FDEA00368), Jun 5, 2000: SKIN. CRACKED. DURING ROUTINE INSP FUSELAGE SKIN FOUND CRACKED AT FWD ENTRY DOOR UPPER HINGE CUTOUT. FUSELAGE SKIN REPAIR PER FEDEX EO 7-5330-7-2345 PART 2. - [SDR 00FDEA00367](https://openairdocs.org/sdr/00FDEA00367), Jun 5, 2000: FIREWALL. CRACKED. DURING ROUTINE INSP NR 2 ENG FIREWALL FOUND CRACKED AT APPROX 8 O''CLOCK POS AT FIRELOOP BRACKET. STOP DRILLED THE CRACK AND INSTALLED REPAIR DOUBLER IAW SRM 54 - [SDR 00FDEA00366](https://openairdocs.org/sdr/00FDEA00366), Jun 5, 2000: SKIN. CRACKED. DURING ROUTINE INSP, FWD LWR CARGO DOOR, EXT SKIN CRACKED IN LWR AFT CORNER. BLENDED OUT CRACK AND INSTALLED EXT DOUBLER IAW SRM 52-00-3. - [SDR 00FDEA00006](https://openairdocs.org/sdr/00FDEA00006), Jan 5, 2000: CONNECTOR. INOPERATIVE. 00-6 - REPEAT FROM 1/4/00; AFT T/O DOORS LIGHT AND L MAIN GEAR DOOR LIGHT REMAINED ON WITH GEAR HANDLE UP AND OFF. RECYCLED DID NOT CORRECT. ALL IND NORM WITH G - [SDR 96FDEA01554](https://openairdocs.org/sdr/96FDEA01554), Sep 30, 1996: NOSE GEAR. MALFUNCTION. WHEN LANDING GEARS WERE EXTENDED ON APPROACH, THE MAINS EXTENDED GREEN, BUT THE NOSE GEAR LIGHT REMAINED AMBER. NO NOSE GEAR DOOR LIGHT ON SECOND OFFICER'S PANE ## Other aircraft with N101FE - [Registered now](https://openairdocs.org/aircraft/N101FE): Boeing 767-3S2F, S/N 42706, built 2013 --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.