# N113FE: 1968 Boeing 727-22C, registration cancelled 2014-04-23 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: April 23, 2014 - 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: 19894 - Year built: 1968 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Experimental, showing compliance - Airworthiness date: November 19, 1987 - Certificate issued: February 1, 1980 - Last registry action: August 28, 2013 - Mode S code: A037DA - Owner when cancelled: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION) - 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/N113FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=113FE - Page: https://openairdocs.org/deregistered/N113FE-2014-04-23 From the FAA registry file of October 29, 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 (23) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 99FDEA00387](https://openairdocs.org/sdr/99FDEA00387), Sep 15, 1999: AIR DIST. FUMES. AIRCRAFT NEEDS INSP FOR ODOR. CVG FIRE DEPT FOUND FUMES EMANATING FROM CRATE IN NR 2 CONTAINER. RAMP AGENT REMOVED CRATE. INSP AC COMP AND FOUND NO CONTAMINATIO - [SDR 98FDEA00750](https://openairdocs.org/sdr/98FDEA00750), Dec 19, 1998: CONNECTOR. LOOSE. 98-303 NR 2 COWL ANTIICE TEMP OFF SCALE AT OVER 250C. NR 2 COWL VALVE STUCK. FOUND CANNON PLUG OFF ANTI DUCT TEMP SENSOR. LOCK WIRED ELECT CONN TO SENSOR PER MM - [SDR 98FDEA00599](https://openairdocs.org/sdr/98FDEA00599), Sep 29, 1998: SWITCH. FAILED. ON APPROACH WITH GEAR LEVER DOWN, NOSE GEAR IND UNSAFE. DURING GO-AROUND LIGHT WENT OUT AND GREEN NOSE GEAR DOWN CAME ON. REPLACED NOSE LAND GEAR POSITION SWITC - [SDR 97FDEA00778](https://openairdocs.org/sdr/97FDEA00778), Oct 28, 1997: RETRACT MECH. FAILED. DURING GEAR EXTENSION, THE NOSE GEAR DOOR LIGHT FLICKERED OFF AND ON AND NEVER TURNED GREEN. RECYCLED GEAR AND GOT A GREEN DOWN AND LOCKED INDICATION. CLEANED N - [SDR 97FDEA0765](https://openairdocs.org/sdr/97FDEA0765), Oct 15, 1997: ACTUATOR. STICKING. NOSE GEAR SLOW TO SHOW DOWN AND LOCKED (GREEN). RED LIGHT REMAINS ON LONGER THAN NORMAL. INSPECTED AND FOUND RT DOOR PLUNGER STICKING. REPLACED PLUNGER, OPS CK - [SDR 96FDEA01508](https://openairdocs.org/sdr/96FDEA01508), Sep 18, 1996: BELLFRAME. DENTED. MAIN CABIN STA 520 AT STR 6R BELLFRAME DENTED, NR0760 MAIN CABIN STA 520 4 INCHES BELOW STR 6R TO BELL FRAME DENTED NR0261. MAIN CABIN STA 520 BETWEEN STR 7 TO - [SDR 96FDEA01509](https://openairdocs.org/sdr/96FDEA01509), Sep 17, 1996: BELLFRAME. DENTED. MAIN CABIN STA 580 BELLFRAME DENTED AND DISTORTED AT FLOOR LEVEL RIGHT SIDE ABOVE STR 17R. CUT OUT DAMAGE AND REPAIRED PER SRM 51-40-3 FIG 1. - [SDR 96FDEA01507](https://openairdocs.org/sdr/96FDEA01507), Sep 11, 1996: FITTING. CORRODED. UPPER LOBE MAIN CARGO FLOOR LT BARRIER NET FITTING 9G CORRODED AND CRACKED IN NUMEROUS PLACES STA 365 LBL 60. REMOVED DAMAGED FITTING, FABRICATED NEW FITTING PE - [SDR 96FDEA01505](https://openairdocs.org/sdr/96FDEA01505), Sep 11, 1996: SEAT TRACK. CORROSION. UPPER LOBE CORROSION AT LBL 35 FROM FS 540 TO 560. REMOVED CORROSION FOUND OUT OF LIMITS. REMOVED AND REPLACED SEAT TRACK PER SRM 51-10-1. - [SDR 96FDEA01506](https://openairdocs.org/sdr/96FDEA01506), Sep 10, 1996: FLOOR BEAM. CORRODED. UPPER LOBE, CORROSION ON FLOOR BEAM STA 681 UPPER CHORD, LBL 45 ON BOTTOM OF AFT FLANGE AT FLOOR BOARD ATTACH HOLE. REMOVED CORROSION, INSTALLED REPAIR STRAP PE - [SDR 96FDEA01502](https://openairdocs.org/sdr/96FDEA01502), Sep 8, 1996: FLOOR BEAM. CORRODED. UPPER LOBE CORROSION AT FS 480 LBL 10 TOP FLOOR BEAM. REMOVED CORROSION PER SRM 51-10-6 OUT OF LIMITS PER SRM 53-10-1. INSTALLED FLOOR BEAM REPAIR STA 480 LBL 4 - [SDR 96FDEA01494](https://openairdocs.org/sdr/96FDEA01494), Sep 7, 1996: FLOOR BEAM. CORRODED. STA 640 BL 0 LBL 60 FLOOR BEAM IS CORRODED ON UPPER FLANGE TOP AND BOTTOM SIDES. FLOOR BEAM HAS BEEN REPAIRED PER SRM 53-10-8 FIG 15. - [SDR 96FDEA01504](https://openairdocs.org/sdr/96FDEA01504), Sep 6, 1996: FLOOR BEAM. CORROSION. HEAVY CORROSION ON MAIN CARGO FLOOR BEAM STA 480. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER SRM 53-10-08. - [SDR 96FDEA01501](https://openairdocs.org/sdr/96FDEA01501), Sep 6, 1996: SKIN. CORRODED. CORROSION ON FUSE SKIN BETWEEN STR 4 TO 6L AT STA 680 TO 700. CUT OUT DAMAGED SECTION OF FUSE SKIN, INSTALLED REPAIR DOUBLER PER SRM 53-30-3. - [SDR 96FDEA01499](https://openairdocs.org/sdr/96FDEA01499), Sep 4, 1996: FLOOR BEAM. CORRODED. UPPER LOBE STA 640 FLOOR BEAM CORRODED ON BOTTOM OF UPPER CHORD, FWD AND AFT FLANGES BETWEEN RBL 45 TO 65. REMOVED CORROSION PER SRM 51-10-6 FOR A SMOOTH BLEND - [SDR 96FDEA01510](https://openairdocs.org/sdr/96FDEA01510), Aug 29, 1996: WEB. CORRODED. CENTER WING BOX 3RD BAY WEB AT STA 870 RBL 25.08 TO 45.61 POPPED FASTENER. REMOVED CORRODED AREA AND INSTALLED DOUBLER PER EA 7-5771-28858. - [SDR 96FDEA1500](https://openairdocs.org/sdr/96FDEA1500), Aug 28, 1996: FLOOR BEAM. CORRODED. UPPER LOBE STA 680 FLOOR BEAM WAS CORRODED. CORROSION WAS REMOVED ON NR0484 LBL 50, MATERIAL REMOVED EXCEEDED SRM 53-10-1 LIMIT MEASURES .121. ACCOMPLISHED REPA - [SDR 96FDEA01503](https://openairdocs.org/sdr/96FDEA01503), Aug 28, 1996: FLOOR BEAM. CORROSION. UPPER LOBE STA 680 FLOOR BEAM WAS CORRODED. CORROSION WAS REMOVED ON NR0484 LBL 5, MATERIAL REMOVAL EXCEEDED SRM 53-10-1 LIMITS MIN .140 MINIMUM PER SRM IS .150 - [SDR 96FDEA01498](https://openairdocs.org/sdr/96FDEA01498), Aug 28, 1996: FLOOR BEAM. CORRODED. CABIN FLOOR BEAM CORRODED AROUND HOLE LWR SURFACE OF UPPER FLANGE STA 440 RBL 35 MKD. CUT OUT DAMAGED SECTION OF FLOOR BEAM UPPER CHORD, FWD ANGLE, INSTALLED FL - [SDR 96FDEA01497](https://openairdocs.org/sdr/96FDEA01497), Aug 27, 1996: FLOOR BEAM. CORRODED. FLOOR BEAM AT STA 344 TOP SURFACE CORRODED FROM LBL 55 RBL 15. REMOVED DAMAGED SECTION OF UPPER CHORD, INSTALLED REPAIR CHORD AND ANGLES PER FEDEX SRD NR SR 27- - [SDR 96FDEA01496](https://openairdocs.org/sdr/96FDEA01496), Aug 27, 1996: FLOOR BEAM. CRACKED. STA 680 LBL 48 FLOOR BEAM IS CRACKED AROUND CORRODED FASTENER HOLE. REMOVED CORROSION PER 51-10-6, INSTALLED REPAIR PER SRM 53-10-8. - [SDR 96FDEA01495](https://openairdocs.org/sdr/96FDEA01495), Aug 27, 1996: FLOOR BEAM. CORRODED. STA 680 BL 0 LBL 60 FLOOR BEAM IS HEAVY CORRODED BL 0 TO LBL 50 MEDIUM CORROSION 50 TO 60 LBL. REMOVED CORROSION PER 51-10-6 INSTALLED REPAIR PER SRM 53-10-8 FI - [SDR 96FDEA00719](https://openairdocs.org/sdr/96FDEA00719), Mar 30, 1996: STRUT. REQD SERVICE. NOSE GEAR DOORS WOULD NOT RETRACT ON TAKEOFF. RECYCLED THE GEAR AND TRIED AGAIN, STILL NO GEAR DOORS RETRACTED. WE OBSERVED AIR SPEED LIMITS, LIGHT EXTINGUISHED ## Other aircraft with N113FE - [Registered now](https://openairdocs.org/aircraft/N113FE): Boeing 767-3S2F, S/N 42711, built 2015 --- 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.