# N124FE: 1967 Boeing 727-25C, registration cancelled 2004-08-26 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: August 26, 2004 - Status when cancelled: Triennial form not returned - Airframe: [Boeing 727-25C](https://openairdocs.org/model/boeing-727-25c) (registry code 138400H) - 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: 19360 - Year built: 1967 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-jet - Airworthiness: Standard - Certificate issued: January 8, 1982 - Last registry action: September 16, 2003 - Mode S code: A06310 - 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/N124FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=124FE - Page: https://openairdocs.org/deregistered/N124FE-2004-08-26 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 727-25C: https://openairdocs.org/model/boeing-727-25c.md ## Service difficulty reports (27) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 03FDEA01840](https://openairdocs.org/sdr/03FDEA01840), Oct 31, 2003: FRAME. DENTED. AFT CARGO BAY FRAME DENTED AT BS 1030 STR 26R. CUT OUT DAMAGED FRAME SECTION IN 1 X 2 INCH AREA. FABRICATED REPAIR PARTS, ALODINED, PRIMED, PAINTED AND INSTALLE - [SDR 03FDEA01841](https://openairdocs.org/sdr/03FDEA01841), Oct 31, 2003: FRAME. CRACKED. AFT CARGO BAY CRACK IN FRAME AT FASTENER HOLE BS 1090 STR 27L UNDER FLOOR TO SIDEWALL SUPPORT. SUPP INFO: AIRCRAFT IS BEING SCRAPPED AND WILL NOT BE LEAVING THI - [SDR 03FDEA00481](https://openairdocs.org/sdr/03FDEA00481), Apr 17, 2003: HANDLE. FAILED. LANDING GEAR HANDLE WOULD NOT RAISE AFTER TAKEOFF. PROCEEDED WITH LANDING GEAR LEVER LATCH FAILED TO RELEASE RED TAB CHECKLIST. AFTER PULLING AND RESETTING SAFE - [SDR 02FDEA00665](https://openairdocs.org/sdr/02FDEA00665), Sep 19, 2002: SEQUENCE VALVE. MALFUNCTIONED. UPON GEAR RETRACTION, GEAR DOORS LIGHT & RIGHT MAIN GEAR UNSAFE LIGHTS REMAINED ILLUMINATED. RED TAB PROCEDURES ACCOMPLISHED. WHEN INITIALLY MOVING, AND BEFORE - [SDR 02FDEA00651](https://openairdocs.org/sdr/02FDEA00651), Sep 14, 2002: DOWNLOCK SWITCH. LOOSE. ON TAKEOFF, UPON GEAR RETRACTION RED RT GROUND UNSAFE LIGHT AND RT MAIN GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED, FOLLOWED QRH PROCEDURES WITH GEAR HANDLE OFF, - [SDR 02FDEA00645](https://openairdocs.org/sdr/02FDEA00645), Sep 13, 2002: ACTUATOR. FAILED. ON TAKEOFF, UPON GEAR RETRACTION, THE RED DOORS LT, RED RIGHT GEAR UNSAFE LT, AND RT MAIN GEAR DOOR OPEN LIGHT REMAINED ILLUMINATED. FOLLOWED QRH PROCEDURES. WI - [SDR 02FDEA00523](https://openairdocs.org/sdr/02FDEA00523), Jul 26, 2002: ENGINE. MALFUNCTIONED. NR 3 ENGINE OIL TEMPERATURE WENT INTO YELLOW BAND APPROX 10 MINUTES AFTER T/O. STARTED 15 MINUTE TIMING & COMPLIED WITH RED TABS. WHEN THRUST LEVER WAS RETARDED - [SDR 01FDEA00274](https://openairdocs.org/sdr/01FDEA00274), Apr 12, 2001: FITTING. CORRODED. DURING ROUTINE INSP STRINGER 18L END FITTING AT BS 1183 FOUND CORRODED. *S/D* REMOVED AND REPLACED STR T-FITTING PER IAW BAC 727 SRM 51-30-2. - [SDR 01FDEA00275](https://openairdocs.org/sdr/01FDEA00275), Apr 12, 2001: FITTING. CORRODED. DURING ROUTINE INSP, STR 18R END FITTING AT BS 1183 FOUND CORRODED. *S/D* REMOVED AND REPLACED STR T-FITTING PER IAW BAC 727 SRM 51-30-2. - [SDR 01FDEA00272](https://openairdocs.org/sdr/01FDEA00272), Apr 12, 2001: FITTING. CRACKED. DURING ROUTINE INSP, RT MAIN GEAR DOOR TO WING FAIRING ROLLER FITTING FOUND CRACKED. ** S/D ** R&R FITTING PER IAW BAC 727 SRM 51-30-2. - [SDR 01FDEA00258](https://openairdocs.org/sdr/01FDEA00258), Apr 6, 2001: SKIN. CRACKED. DURING ROUTINE INSP, RT WING UPPER SKIN LEAD EDGE FOUND CRACKED AT WS 46, 8 INCHES FWD OF THE FWD WING SPAR.** S/D ** FAB & REPAIR PER IAW BAC 727 SRM 57-30-4 & - [SDR 01FDEA00266](https://openairdocs.org/sdr/01FDEA00266), Apr 6, 2001: SPAR. CORRODED. DURING ROUTINE INSP, FWD FACE OF THE BS 870 BULKHEAD BL 0 UP 9 INCHES FROM OPEN FOR HOT AIR DUCT IN KEELBEAM FOUND CORRODED. *S/D* REPAIRED REAR SPAR WEB PER IA - [SDR 01FDEA00265](https://openairdocs.org/sdr/01FDEA00265), Apr 6, 2001: SEAT TRACK. CORRODED. DURING ROUTINE INSP, NR 2 SEAT TRACK FOUND CORRODED BS 610. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5. - [SDR 01FDEA00264](https://openairdocs.org/sdr/01FDEA00264), Apr 6, 2001: SEAT TRACK. CORRODED. DURING ROUTINE INSP, NR 3 SEAT TRACK FOUND CORRODED FROM BS 640-740. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 53-10-5. - [SDR 01FDEA00263](https://openairdocs.org/sdr/01FDEA00263), Apr 6, 2001: PLATE. CRACKED. DURING ROUTINE INSP, RT ELEVATOR REAR SPAR NR 4 SHEAR PLATE FOUND CRACKED. REMOVED, REPLACED AND FAB PER IAW BAC 727 SRM 51-20-2, 51-30-2. - [SDR 01FDEA00247](https://openairdocs.org/sdr/01FDEA00247), Mar 31, 2001: SKIN. CRACKED. DURING INSP FUSELAGE SKIN AT BS 249, WL 245 WAS FOUND CRACKED AT FASTENER HOLE BENEATH THE PILOTS NR 3 WINDOW. *S/D* REPAIRED SKIN PER IAW FEDEX EA 7-5330-57216 - [SDR 01FDEA00244](https://openairdocs.org/sdr/01FDEA00244), Mar 31, 2001: SPAR. CORRODED. DURING ROUTINE INSP, THE AFT FACE OF THE CENTER WING TANK FOUND CORRODED 9 INCHES UP FROM BOTTOM OF THE TANK AT RBL 9. *S/D* REPAIRED REAR SPAR PER IAW FEDEX EA - [SDR 01FDEA00246](https://openairdocs.org/sdr/01FDEA00246), Mar 31, 2001: SPAR. CORRODED. DURING ROUTINE INSP, THE CTR FUEL TANK AFT WEB FOUND CORRODED ON THE AFT FACE FROM LBL 15 TO LBL 18, 6-8 IN UP FROM BOTTOM OF TANK. *S/D* REPAIRED REAR SPAR WEB - [SDR 01FDEA00245](https://openairdocs.org/sdr/01FDEA00245), Mar 31, 2001: STIFFENER. CORRODED. DURING ROUTINE INSP THE VERTICAL STIFFENER AT LBL 14 ON THE AFT SIDE OF THE CTR WING TANK FOUND CORRODED 2 IN FROM TOP OF THE STIFFENER. - [SDR 01FDEA00199](https://openairdocs.org/sdr/01FDEA00199), Mar 15, 2001: DOOR. UNLATCHED. AFT CARGO LIGHT ON AT 14,000. BOTH PACKS WERE ON AND PRESS WAS STABLE. NO YAW PROBLEMS NOTED. FOUND AFT FAIRING DOOR UNLATCHED. SECURED LATCH. OPS NORMAL. OK FO - [SDR 00FDEA00790](https://openairdocs.org/sdr/00FDEA00790), Nov 25, 2000: SWITCH. DIRTY. WHEN PUTTING GEAR HANDLE OFF POSITION RED DOOR LIGHT AND RIGHT MAIN GEAR DOOR LIGHT ILLUM. CLEANED RM GEAR DOOR SWITCH PER STANDARD MAINTENANCE PRACTICES. ALL I - [SDR 00FDEA00781](https://openairdocs.org/sdr/00FDEA00781), Nov 18, 2000: UPLOCK. FAILED. WHEN CAPT PLACED GEAR HANDLE IN OFF POS RT MLG RED LIGHT AND RT MLG DOOR OPEN LIGHT ILLUM. C/W RED TABS AND RETURN TO UP POS. REPEAT DISCREPANCY. *S/D* REMOVED - [SDR 99FDEA00010](https://openairdocs.org/sdr/99FDEA00010), Jan 14, 1999: SWITCH. OUT OF ADJUST. 99-0010 - RED DOOR LIGHT ON WHEN GEAR IS OFF. GEAR RECYCLED PER RED TABS. LIGHT WENT OUT AND GEAR LEVER LEFT UP POSITION. INSTALL MAIN AND NOSE GEAR PINS 1-14-9 - [SDR 97FDEA00543](https://openairdocs.org/sdr/97FDEA00543), Aug 15, 1997: LATCH. NOT LATCHED. 97-0158 - AFT CARGO LIGHT ILLUMINATED AFTER TAKEOFF AT 3000 MSL. FOUND AFT CARGO DOOR OUTER FAIRING BOTTOM LATCH NOT POSITIONED PROPERLY. RELATCHED DOOR. OPERAT - [SDR 96FDEA00915](https://openairdocs.org/sdr/96FDEA00915), May 6, 1996: GUSSET. CRACKED. CABIN INTERIOR STA FS 600 RIB GUSSET IS CRACKED IN TWO AT STR 2L AREA. REPLACED GUSSET WITH 7075-T6 X.063 DOUBLER AS SHOWN IN FIG NR 1 AS PER EA 7-5330-28637 DA - [SDR 96FDEA00912](https://openairdocs.org/sdr/96FDEA00912), May 2, 1996: WEB. CRACKED. LT STA 870 LOWER INTEGRAL WEB IS CRACKED. FABRICATED A MACHINED BATHTUB FITTING. MATERIAL TO BE 4130 TREATED TO SPECIFICATION 180 TO 200 KSI CAD PLATE, PRIME AS - [SDR 96FDEA00810](https://openairdocs.org/sdr/96FDEA00810), Apr 16, 1996: FRAME. CRACKED. NRO232, STA 804 ABOVE CUSP, FRAME CRACKED FROM I/B LIP TO FASTENER HOLE IN CENTER OF FRAME. *S/D* FABRICATED REPAIR PARTS IAW SRM 51-40-3 AND INSTALLED DOUBLER ## FAA accident and incident reports (4) 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 19970326009069I](https://openairdocs.org/incident/19970326009069I), Mar 26, 1997: Boeing 72725C (N124FE), Knoxville, TN, Minor damage. Narrative: the marshaller did not determine that a tug/trailer/container was parked inside the painted object free line. During a heavy rain during aircraft… - [Incident 19920327008949I](https://openairdocs.org/incident/19920327008949I), Mar 27, 1992: Boeing 72725C (N124FE), Memphis, TN. NR1 engine fire warning. Engine shut down. Landed at destination. Found an eight stage duct blown. Caused warning. - [Incident 19900802040129I](https://openairdocs.org/incident/19900802040129I), Aug 2, 1990: Boeing 72725C (N124FE), Memphis, TN. APU on fire on pushback. Crew shut down APU and fired bottle. Deployed slide and evacuated. - [Incident 19880719044319I](https://openairdocs.org/incident/19880719044319I), Jul 19, 1988: Boeing 72725C (N124FE), Memphis, TN. On takeoff,cockpit filled with burning oily odor. Returned. Maintenance replaced air conditioning sock. ## Other aircraft with N124FE - [Registered now](https://openairdocs.org/aircraft/N124FE): Boeing 767-3S2F, S/N 43546, 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.