# N377FE: 1972 Mcdonnell Douglas MD-10-10F, registration cancelled 2024-03-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 2, 2024
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell Douglas MD-10-10F](https://openairdocs.org/model/mcdonnell-douglas-md-10-10f) (registry code 3022112)
- Engine: [GE CF6-6 series](https://openairdocs.org/engine/ge-cf6-6-series) (registry code 30020)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 47965
- Year built: 1972
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 11, 1998
- Certificate issued: October 25, 1997
- Last registry action: June 3, 2023
- Mode S code: A44E4E
- 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/N377FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=377FE
- Page: https://openairdocs.org/deregistered/N377FE-2024-03-02

From the FAA registry file of November 5, 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 Mcdonnell Douglas MD-10-10F: https://openairdocs.org/model/mcdonnell-douglas-md-10-10f.md

## Service difficulty reports (95, newest 50)

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

- [SDR FDEA201502200555](https://openairdocs.org/sdr/FDEA201502200555), Feb 20, 2015: LIMIT SWITCH. FAILED. R1 DOOR ARM & DISARM LEVER IS DIFFICULT TO MOVE IN EITHER DIRECTION. THE LEVER MUST BE PUSHED AGAINST THE STOP TO EXTINGUISH THE DISARM LIGHT. REMOVED AND REPLA
- [SDR FDEA201412114106](https://openairdocs.org/sdr/FDEA201412114106), Dec 11, 2014: LAMP. INOPERATIVE. L1 DOOR SLIDE LIGHT WILL NOT TEST. REMOVED & RE LAMPED L1 DOOR SLIDE PRESS INDICATION LIGHT ASSEMBLY & REINSTALLED. OPERATIONS CHECK IS GOOD.
- [SDR FDEA201408042330](https://openairdocs.org/sdr/FDEA201408042330), Aug 4, 2014: SKIN. CRACKED. RIGHT WING FOUND CRACK AT UPPER RT INBD CORNER OF TAI CUT OUT. FACTED IN ERROR WITH NO DEFECTS SEQ 225 WRI 57-10-4400. COMPLIED WITH EA 8-5720-T0310225 P1 BY RE
- [SDR FDEA201408042329](https://openairdocs.org/sdr/FDEA201408042329), Aug 4, 2014: SKIN. CRACKED. EVIDENCE OF CRACKING AT UPPER INBD CORNER OF LT WING TAI DUCT CUT OUT ON THE FIXED LE SKIN. COMPLIED WITH EA 8-5720-T0310221 P1 BY REPAIRING USING SRM 57-40-01 
- [SDR FDEA201405131044](https://openairdocs.org/sdr/FDEA201405131044), May 13, 2014: SKIN. CRACKED. POST FLIGHT WALK AROUND, FOUND POSSIBLE CRACK AT RT REFUELING DOOR INBD RADIUS ON WING. INSTALLED DOUBLER IAW SRM 57-10-00 & EA 8-5710-T0308147.
- [SDR FDEA201401050022](https://openairdocs.org/sdr/FDEA201401050022), Jan 5, 2014: SLIDE. FAULTY. L1 DOOR LOW BOTTLE PRESS INDICATOR LIGHT ILLUMINATED. REMOVED L1 DOOR SLIDE LOWER COVER & TROUBLESHOOT IAW ASM 25-61-0. FOUND CONTINUITY AT LIGHT ASSEMBLY JACK 
- [SDR FDEA201311242864](https://openairdocs.org/sdr/FDEA201311242864), Nov 24, 2013: SENSOR. FAULTY. ON CLIMB OUT LEVEL 3 BLED AIR 1 TEMP HI COMPLIED WITH QRH NO FURTHER INDICATION DURING RETURN. RELEASED FOR SERVICE IAW MEL 36-10-02-A. REMOVED AND REPLACED PNE
- [SDR FDEA201310152510](https://openairdocs.org/sdr/FDEA201310152510), Oct 15, 2013: SPAR. CORRODED. NR 1 PYLON UPPER SPAR CAP INBD LANDING IS CORRODED. CLEANED CORRISION AND BLENDED LANDING PER SRM 51-21-01 VOL II AND EA 8-5450-T0303216.
- [SDR FDEA201310152512](https://openairdocs.org/sdr/FDEA201310152512), Oct 15, 2013: CHANNEL. CRACKED. NR 1 PYLON, BRACKET BETWEEN LT AND RT LOWER SPARS CRACKED APPROXIMATELY 3 INCHES LONG. REMOVED CRACKED CHANNEL, FABRICATED NEW CHANNEL, IAW DWG AUB7009. INSTALL
- [SDR FDEA201309252314](https://openairdocs.org/sdr/FDEA201309252314), Sep 25, 2013: BULKHEAD. CRACKED. NLG WHEEL WELL, RT BULKHEAD WEB CRACKED. ABOUT 3.5 INCHES LONG, AT BS 480, X= -6. INSTALLED FILLER SHIM AND DOUBLER IAW SRM 53-30-30 VOL.1 FIG.6.
- [SDR FDEA201303050497](https://openairdocs.org/sdr/FDEA201303050497), Mar 5, 2013: PROXIMITY SENSOR. MISINSTALLED. AFTER TAKEOFF, RAISED LANDING GEAR; RT MAIN INDICATED UNSAFE (RED) ON FWD PANEL AND SYNOPTIC. FOLLOWED QRH PROCEDURE, SLOWED AND CYCLED GEAR AFTER SECOND RETRAC
- [SDR FDEA201302260462](https://openairdocs.org/sdr/FDEA201302260462), Feb 26, 2013: WIRE. BURNED. WIRE B9502-108-16 HAS BURN SIGNS, LOCATED BELOW THE RT OBSERVER CONSOLE THRU ACCESS PANEL ABN7643-139. REPAIRED WIRE B9502-108-16 IAW SWP 20-10-03, SECTION 7D. 
- [SDR FDEA201302070293](https://openairdocs.org/sdr/FDEA201302070293), Feb 7, 2013: CONTROL UNIT. FAILED. ANTI-SKID LT FAIL ALERT DURING PREFLIGHT CLEARED AFTER SUBSEQUENT SELF TEST. EXTENDED GEAR AND ANTI-SKID LT FAILED AGAIN. COMPLETED CHECKLIST AND DECLEARED EMER
- [SDR FDEA201210053570](https://openairdocs.org/sdr/FDEA201210053570), Oct 5, 2012: ANTI-SKID SYS. MALFUNCTIONED. LEFT ANTI-SKID FAIL GO AROUND, RAN QRH ON SECOND GEAR EXTENSION NO ANTI-SKID FAIL. PERFORMED RTS ON VIA 1 ALL CHECKS GOOD. PERFORMED BITE TEST ON ANTI SKID CONT
- [SDR FDEA201209183349](https://openairdocs.org/sdr/FDEA201209183349), Sep 18, 2012: TEE FITTING. CRACKED. LEFT SIDEWALL TO SPAR ATTACH TEE FITTING HAS A THREE INCH CRACK 1.5" DOWN FROM SPAR CAP. REMOVED TEE FITTING IAW SRM 51-35-01. FABRICATED PART APB 7078-1 IAW DW
- [SDR FDEA201204041253](https://openairdocs.org/sdr/FDEA201204041253), Apr 4, 2012: SENSOR. FAILED. RIGHT MLG INTERMITTENT RED UNSAFE UP & LOCKED. BOTH PRIMARY & SECONDARY, QRH FOLLOWED. REMOVED RT MLG DOWNLOCK SENSOR D1-43. REPLACED PINS AND CONNECTOR ON NEW 
- [SDR FDEA201108253479](https://openairdocs.org/sdr/FDEA201108253479), Aug 25, 2011: POWER SUPPLY. FAILED. WHILE PREPPING ACFT FOR DEPARTURE, EMERGENCY LIGHT TEST FAIL. INDICATED EMERGENY LIGHT BATTERY 1 LOW. FOUND EMERGENCY LIGHT BATTERY POWER SUPPLY FAULTY. R & R E
- [SDR FDEA201102100521](https://openairdocs.org/sdr/FDEA201102100521), Feb 10, 2011: BULB. WRONG PART. L1 DOOR SLIDE PRESSURE, PRESS TO TEST LIGHT INOPERATIVE. FOUND WRONG BULBS INSTALLED IN LIGHT SOCKET, INSTALLED PROPER BULBS PER STANDARD MAINT. PRACTICES, OPS 
- [SDR FDEA201012264753](https://openairdocs.org/sdr/FDEA201012264753), Dec 26, 2010: PRESSURE SWITCH. INOPERATIVE. ON DESCENT TURNED ON ENG - WING ANTI-ICE RECEIVED "A WING A-ICE L DISAG ALERT SHORTLY AFTER RECEIVED AN AIR MANF 1 FAIL" COMPLIED WITH QRH AND DIVERTED, WITHOUT
- [SDR FDEA200912024335](https://openairdocs.org/sdr/FDEA200912024335), Dec 2, 2009: FRAME. CRACKED. MAIN CARGO STA 1721, RT LONGERON NR 13, FRAME CRACKED N1080 WAS GENERATED TO REPAIR ALL AFFECTED AREAS. THIS CRACKED FRAME SECTION AT THE ABOVE STA AND LONGERON
- [SDR FDEA200912024334](https://openairdocs.org/sdr/FDEA200912024334), Dec 2, 2009: FRAME. CRACKED. MAIN CARGO, STA 1741, RT, LONGERON NR 13, FRAME CRACKED N1079 WAS GENERATED TO REPAIR ALL AFFECTED AREAS. THIS CRACKED FRAME SECTION AT THE ABOVE STA AND LONGER
- [SDR FDEA200912024333](https://openairdocs.org/sdr/FDEA200912024333), Dec 2, 2009: FRAME. CRACKED. MAIN CARGO, STA NR 1781, LT LONGERON NR 13, FRAME CRACKED N1078 WAS GENERATED TO REPAIR ALL AFFECTED AREAS. THIS CRACKED FRAME SECTION AT THE ABOVE STA AND LONG
- [SDR FDEA200912024332](https://openairdocs.org/sdr/FDEA200912024332), Dec 2, 2009: FRAME. CRACKED. MAIN CARGO, STA NR 1761, LT LONGERON NR 13 FRAME CRACKED. N1076 WAS GENERATED TO REPAIR ALL AFFECTED AREAS. THIS CRACKED FRAME SECTION AT THE ABOVE STA AND LONG
- [SDR 08FDEA02166](https://openairdocs.org/sdr/08FDEA02166), Jun 5, 2008: NONE. NONE. REJECTED TAKEOFF AT IND AT 100 KTS OAT 31C WEIGHT 386,200. REJECTED FOR PREDICITIVE WINDSHEAR ALERT. NO OBSERVED OR REPORTED WINDSHEAR. PERFORMED BRAKE INSPECTI
- [SDR 07FDEA05144](https://openairdocs.org/sdr/07FDEA05144), Dec 27, 2007: BOLT. SHEARED. NR 3 PYLON, TOMBSTONE LOWER SPHERICAL BEARING ATTACH BOLT SHEARED AT 6 O'CLOCK POSITION, DOT NR 1. REMOVED AND REPLACED 6 BOLTS, P/N 77711-9-105, PLATE -P/N AUB
- [SDR 07FDEA02439](https://openairdocs.org/sdr/07FDEA02439), Jul 10, 2007: MEC. FAILED. NR 1 ENGINE FLAMED OUT ON ROLLOUT. FIRST INDICATION WAS GEN 1 OFF FOLLOWED BY AIR SYS 1 LOW PRESS. REMOVED AND REPLACED FUEL PUMP AND MEC.
- [SDR 06FDEA2000](https://openairdocs.org/sdr/06FDEA2000), May 23, 2006: SPAR. CORRODED. LT WHEEL WELL STA 1370 JUST ABOVE REAR SPAR, HAS AREA OF CORROSION. REMOVED CORROSION AT EDGE MEMBER, OUT OF LIMITS IAW DC10 SRM 51-21-01-VOL II AND DC10 SRM 53
- [SDR 06FDEA1912](https://openairdocs.org/sdr/06FDEA1912), May 13, 2006: DOUBLER. CRACKED. LEFT OUTER WING TO CENTER WING LOWER SURFACE SPLICE DOUBLER HAS A CRACK STARTING AT FASTENER HOLE ON AFT END, XFS 145 AND FS 1370. REPAIRED IAW FEDEX EA 8-5710-
- [SDR 06FDEA1787](https://openairdocs.org/sdr/06FDEA1787), May 11, 2006: REPAIR. UNKNOWN. REPAIR EVALUATION AGING AIRPLANE PROGRAM EXISTING REPAIR AT STA 304-328 LONGERON 26L-38L. OPS 1401/ T 8-5330-86848 COMPLIED WITH CARD T-8-5330-83848-FUSELAGE-RE
- [SDR 04FDEA03454](https://openairdocs.org/sdr/04FDEA03454), Dec 21, 2004: VALVE. MALFUNCTIONED. AFTER GEAR EXTENSION, RECEIVED LVL 2 LT ANTI SKID FAIL. EXECUTED GO-AROUND, FOLLOWED QRH PROCEDURES. ALERT MOMENTARILY EXTINGUISHED AFTER CYCLING ANTI SKID SWIT
- [SDR 04FDEA03386](https://openairdocs.org/sdr/04FDEA03386), Dec 7, 2004: HINGE BRACKET. GOUGED. VERTICAL STABILIZER REAR SPAR, UPPER RUDDER HINGE FITTING BENT AND GOUGED. REMOVED AND REPLACED UPPER RUDDER HINGE SUPPORT BRACKET IAW MD10-10 MM 55-53-01-2 AND
- [SDR 04FDEA03329](https://openairdocs.org/sdr/04FDEA03329), Dec 2, 2004: SKIN. DAMAGED. AFT REPAIR AT STATION 966 TO 1001, LONGERON 37 RIGHT TO 42 RIGHT NEEDS EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WITH F
- [SDR 04FDEA03272](https://openairdocs.org/sdr/04FDEA03272), Nov 30, 2004: SKIN. CORRODED. REPAIR AT STATION 1957 TO 1993 LONGERON 49 LEFT TO 49 RIGHT NEED ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE 
- [SDR 04FDEA03270](https://openairdocs.org/sdr/04FDEA03270), Nov 30, 2004: SKIN. DAMAGED. REPAIR AT STATION 304 TO 328 LONGERON 26 LEFT AND 38 LEFT NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIRS IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE 
- [SDR 04FDEA03269](https://openairdocs.org/sdr/04FDEA03269), Nov 30, 2004: SKIN. DAMAGED. REPAIR AT STATION 330 BETWEEN LONGERONS 37 RIGHT TO 38 RIGHT NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANC
- [SDR 04FDEA03268](https://openairdocs.org/sdr/04FDEA03268), Nov 30, 2004: SKIN. DAMAGED. EXTERNAL DOUBLER ON LEFT HAND LOWER FUSELAGE SKIN STATION 470 TO 475 BETWEEN LONGERON 30 LEFT AND 31 LEFT APPEARS NOT TO BE PER THE SRM. REMOVED OLD REPAIR IAW 
- [SDR 04FDEA03267](https://openairdocs.org/sdr/04FDEA03267), Nov 30, 2004: SKIN. DAMAGED. REPAIR AT STATION 470-475 LONGERON 30 RIGHT TO 30 LEFT, NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF REPAIR IS IN ACCORDANCE WIT
- [SDR 04FDEA03266](https://openairdocs.org/sdr/04FDEA03266), Nov 30, 2004: SKIN. DAMAGED. REPAIR AT STATION 1942 LONGERON 50 RIGHT TO 51 RIGHT NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MINOR OR MAJOR AND IF REPAIR IS IN ACCORDANCE WITH F
- [SDR 04FDEA03265](https://openairdocs.org/sdr/04FDEA03265), Nov 29, 2004: PANEL. DELAMINATED. RIGHT WING PANEL ARC0613-502, UPPER TRAILING EDGE PANEL AT INBOARD END OF OUTBOARD FLAP DELAMINATED. RIGHT WING PANEL ARC0613-502 REPAIRED BY FABRICATING AND BO
- [SDR 04FDEA03264](https://openairdocs.org/sdr/04FDEA03264), Nov 29, 2004: MANIFOLD. WORN. NR 1 ENGINE OUTBOARD THRUST REVERSER UPPER COOLING DUCT IS CHAFED IN SEVERAL AREAS. REMOVED COOLING DUCT IAW DC10 SRM 51-31-01 VOL 2. WELD REPAIRED COOLING MANI
- [SDR 04FDEA03263](https://openairdocs.org/sdr/04FDEA03263), Nov 29, 2004: ROLLER. LOOSE. RIGHT WING LOWER FORWARD INBOARD FLAP LOAD ROLLER HAS EXCESSIVE LATERAL PLAY. REMOVED AND REPLACED RIGHT HAND INBOARD FLAP INBOARD TRACK LOWER ROLLER IAW FEDEX 
- [SDR 04FDEA03262](https://openairdocs.org/sdr/04FDEA03262), Nov 29, 2004: ROLLER. WORN. RIGHT WING LOWER AFT LOAD ROLLER HAS WORN BEARING SURFACE, CHROME WORN ON INBOARD FLAP TRACK ATTACHMENT AREA. REMOVED AND REPLACED RIGHT HAND INBOARD FLAP INBOA
- [SDR 04FDEA03261](https://openairdocs.org/sdr/04FDEA03261), Nov 29, 2004: SKIN. DAMAGED. REPAIR AT STATION 1140 TO 1151 AT LONGERON 39 LEFT TO 41 LEFT NEEDS ENGINEERING EVALUATION TO DETERMINE MAJOR OR MINOR AND IF DATA AND REPETITIVE INSPECTION REQ
- [SDR 04FDEA03260](https://openairdocs.org/sdr/04FDEA03260), Nov 29, 2004: DOOR. DELAMINATED. LEFT HAND WING REFUEL PANEL NEEDS REWORK DUE TO SHIFT OF INNER DOUBLER DURING AUTO-CLAVE CURE AND LACK OF TIMCO ROUTING SHEET BEING ASSIGNED. REPAIRED, REWORKED
- [SDR 04FDEA03259](https://openairdocs.org/sdr/04FDEA03259), Nov 29, 2004: DOOR. DELAMINATED. LEFT WING REFUEL PANEL, DELAMINATED ON EDGES ADJACENT TO HINGE, AS MARKED. LOWER SKIN, CORE AND BLOCKS BONDED IAW TPS 1001 REV E, DAC DWG ARB1011 AND FEDEX EA 8
- [SDR 04FDEA03258](https://openairdocs.org/sdr/04FDEA03258), Nov 29, 2004: PRESSURE BLKHD. DAMAGED. REPAIR UNDER RADAR ON PRESSURE BULKHEAD NEEDS ENGINEERING EVALUATION TO DETERMINE IF REPAIR IS MAJOR OR MINOR AND IF IS IN ACCORDANCE WITH FAA APPROVED DATA AND
- [SDR 04FDEA03257](https://openairdocs.org/sdr/04FDEA03257), Nov 29, 2004: PANEL. DELAMINATED. LEFT WING PANEL OVER AFT TRUNNION HAS MANY AREAS OF DELAMINATION. REPAIRED AFT TRUNNION PANEL ARC0269-503 BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND COR
- [SDR 04FDEA03256](https://openairdocs.org/sdr/04FDEA03256), Nov 29, 2004: PANEL. DENTED. LEFT HAND WING UPPER TRAILING EDGE PANEL JUST OUTBOARD OF MAIN LANDING GEAR UPPER SURFACE HAS SEVERAL DENTS. REPAIRED PANEL PART NUMBER ARC0263, BY FABRICATING 
- [SDR 04FDEA03254](https://openairdocs.org/sdr/04FDEA03254), Nov 29, 2004: HINGE BRACKET. CORRODED. LEFT AND INBOARD FLAP OUTBOARD HINGE BOLT HOLE HAS AREA OF CORROSION. BOLT HOLE IS REPLACEMENT BOLT PART NUMBER 3D0031-8-90 STEP 23 OF FEDEX WIC E 8-5710-7-5005
- [SDR 04FDEA03253](https://openairdocs.org/sdr/04FDEA03253), Nov 29, 2004: PANEL. DELAMINATED. RIGHT WING INBOARD FLAP AREA LEFT HAND FALSE SPAR CEILING PANEL INBOARD OF MAIN LANDING GEAR STRUT DELAMINATED/DENTED. REMOVED FILLET PANELS 152FT, 152ET AND SM

All 95: https://openairdocs.org/deregistered/N377FE-2024-03-02/reports.md

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