# N147FE: 1966 Boeing 727-22, registration cancelled 2003-03-06 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 6, 2003 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 727-22](https://openairdocs.org/model/boeing-727-22) (registry code 1384002) - Engine: [Pratt & Whitney JT8D-1](https://openairdocs.org/engine/pratt-whitney-jt8d-1) (registry code 52044) - Data sheets: [TCDS E2EA](https://openairdocs.org/tcds/E2EA) (OpenAirDocs) - Serial number: 19080 - Year built: 1966 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard, transport - Airworthiness date: May 18, 1966 - Certificate issued: August 5, 1987 - Last registry action: September 19, 2000 - Mode S code: A0BD33 - 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/N147FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=147FE - Page: https://openairdocs.org/deregistered/N147FE-2003-03-06 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 727-22: https://openairdocs.org/model/boeing-727-22.md ## Service difficulty reports (18) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 01FDEA00238](https://openairdocs.org/sdr/01FDEA00238), Mar 30, 2001: CONTROL UNIT. MALFUNCTIONED. WHILE HOLDING FOR T/O DURING CROSSBLEED START OF NR 3 ENG. AFT CARGO SMOKE WARNING AND BELL ACTIVATED. FIRED NR 1 FIRE BOTTLE INTO AFT CARGO COMPARTMENT. WARNIN - [SDR 00FDEA00644](https://openairdocs.org/sdr/00FDEA00644), Sep 8, 2000: FRAME. GOUGED. DURING ROUTINE INSP, BS 1342 FRAME FOUND GOUGED BEYOND ALLOWED LIMITS ABOVE STR 20R. CUT OUT DAMAGED SECTION, FAB AND INSTALL PER IAW B727 SRM 51-40-3 AND B727 - [SDR 00FDEA00643](https://openairdocs.org/sdr/00FDEA00643), Sep 8, 2000: FRAME. WORN. DURING ROUTINE INSP, APPROX 4 IN OF FRAME AT BS 1342 FOUND WORN BEYOND LIMITS AT STR 15R. CUT OUT DAMAGED SECTION, FAB AND INSTALL PER IAW B727 SRM 51-40-3 AND - [SDR 00FDEA00638](https://openairdocs.org/sdr/00FDEA00638), Sep 8, 2000: COVER. CRACKED. DURING ROUTINE INSP, THE EMERGENCY ESCAPE SLIDE COVER FOUND CRACKED IN SEVERAL PLACES. REPAIRED COVER PER IAW B727 SRM 51-40-8. - [SDR 00FDEA00641](https://openairdocs.org/sdr/00FDEA00641), Sep 7, 2000: FRAME. WORN. DURING ROUTINE INSP, APPROX 5 IN OF THE FRAME AT BS 1342 WAS FOUND WORN BEYOND LIMITS AT STR 20R. CUT OUT DAMAGED SECTION, FAB AND INSTALL PER IAW SRM 51-40-3 A - [SDR 00FDEA00642](https://openairdocs.org/sdr/00FDEA00642), Sep 7, 2000: SKIN. WORN. DURING ROUTINE INSP, FUSELAGE SKIN WAS FOUND WORN BEYOND LIMITS AT BS 1342 UNDER RAIN GUTTER. REMOVED AND REPLACED, FAB PER IAW B727 SRM 53-30-3. - [SDR 00FDEA00640](https://openairdocs.org/sdr/00FDEA00640), Sep 6, 2000: SKIN. CORRODED. DURING ROUTINE INSP, THE FUSELAGE SKIN FOUND CORRODED BEYOND ALLOWED LIMITS BETWEEN SKIN LAP AT BS 1338, STR 10L. REMOVED AND REPLACED, FAB DOUBLER AND FILLER P - [SDR 00FDEA00639](https://openairdocs.org/sdr/00FDEA00639), Sep 6, 2000: STIFFENER. CRACKED. DURING ROUTINE INSP, A VERTICAL STIFFENER FOUND CRACKED AT BS 1070, BETWEEN STR 28R AND 29R. REMOVED, FAB AND INSTALLED PER IAW B727 SRM 51-20-1, 51-30-2. - [SDR 00FDEA00637](https://openairdocs.org/sdr/00FDEA00637), Sep 6, 2000: WIRE. BROKEN. DURING ROUTINE INSP, THE EMERGENCY ESCAPE SLIDE LIGHT WIRE WAS FOUND BROKEN BETWEEN THE BATTERY AND LIGHT. REPAIRED BROKEN WIRE PER IAW WDM 33-51-02. - [SDR 97FDEA00829](https://openairdocs.org/sdr/97FDEA00829), Nov 13, 1997: SWITCH. INOPERATIVE. EQUIPMENT ACCESS DOOR LIGHT INOPERATIVE. AIRCRAFT TOOK OFF WITH ELECTRICAL EQUIPMENT COMPARTMENT OPEN. RAMP ACCOMPLISHED PUSH BACK, INSPECTED ELECTRICAL EQUIPME - [SDR 96FDEA00331](https://openairdocs.org/sdr/96FDEA00331), Feb 28, 1996: TRIM MOTOR. FAILED. AFTER TAKEOFF, MAIN STABILIZER TRIM FAILED. RESET CIRCUIT BREAKER TO NO AVAIL, CRUISE TRIM WORKED NORMALLY. REPLACED MAIN ELECTRIC STABILIZER TRIM MOTOR PER MM - [SDR 95FDEA01315](https://openairdocs.org/sdr/95FDEA01315), Sep 12, 1995: SKIN. CORRODED. STR 9R STA 1352 TO 1420 PILLOWING SKIN. REMOVED AND REPLACED 30 INCHES OF SKIN AND REPAIRED SKINS BOTH FWD AND AFT OF STA 1365.5 STR 9R, PER FEDEX SRM 53-30-3, - [SDR 95FDEA01313](https://openairdocs.org/sdr/95FDEA01313), Sep 12, 1995: CHORD. CORRODED. CORROSION ON REINFORCEMENT CHORD STA 1176.9 RBL 55 WL 208. REMOVED PARTS, SECONDARY STRUCTURE AND REMOVED CORRODED REINFORCEMENT CHORD. INSTALLED NEW CHORD AND - [SDR 95FDEA01312](https://openairdocs.org/sdr/95FDEA01312), Sep 12, 1995: CHORD. CORRODED. CORROSION FOUND ON HORIZONTAL CHORD AT RBL 16.5 TO 20 WL 191.5. REPAIRED CORRODED AREA PER EA 7-5310-25687. - [SDR 95FDEA01316](https://openairdocs.org/sdr/95FDEA01316), Sep 8, 1995: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT FLANGE AT STA 840 LBL 24 WL 208 HAS INTERGRANULAR CORROSION THAT IS OUT OF LIMITS. FABRICATED REINFORCEMENT STRAP PER EWO NO 95-3069. - [SDR 95FDEA01314](https://openairdocs.org/sdr/95FDEA01314), Sep 8, 1995: SKIN. CORRODED. STRINGER 9L STA 1372 TO 1389 PILLOWING SKIN. REMOVED DAMAGE SECTION OF SKIN AND REPAIRED IAW FEDEX SRM 53-30-3, 51-30-2. - [SDR 95FDEA01272](https://openairdocs.org/sdr/95FDEA01272), Sep 7, 1995: STIFFENER. GOUGED. GOUGE IN FLOORBEAM VERTICAL STIFFENER STA 312 RBL 52 WL 207. REMOVED AND FABRICATED FLOORBEAM VERTICAL STIFFENER. ALL WORK DONE IAW FEDEX SRM 53-20-1. - [SDR 95FDEA01271](https://openairdocs.org/sdr/95FDEA01271), Sep 7, 1995: SEAT TRACK. CORRODED. CORRODED SEAT TRACK AND FASTENERS AT STA 760 TO 850 LBL 25. REMOVED AND REPLACED SEAT TRACK. ALL WORK DONE IAW FEDEX SRM 53-10-1 AND FEDEX MM 53-20-12. ## FAA accident and incident reports (1) 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 19930423018149I](https://openairdocs.org/incident/19930423018149I), Apr 23, 1993: Boeing 72722 (N147FE), Cleveland, OH, Minor damage. Blew NR1 and NR4 tires on landing rollout. Found NR4 main anti-skid spider was broken. ## Other aircraft with N147FE - [Registered now](https://openairdocs.org/aircraft/N147FE): Boeing 767-300F, S/N 63094, built 2017 --- 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.