# N373FE: 1972 Mcdonnell Douglas MD-10-10F, registration cancelled 2024-01-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 29, 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 CF6-6D](https://openairdocs.org/engine/ge-cf6-6d) (registry code 30076)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 46611
- Year built: 1972
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 3, 2007
- Certificate issued: January 8, 1998
- Last registry action: August 4, 2023
- Mode S code: A43F72
- 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/N373FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=373FE
- Page: https://openairdocs.org/deregistered/N373FE-2024-01-29

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 Mcdonnell Douglas MD-10-10F: https://openairdocs.org/model/mcdonnell-douglas-md-10-10f.md

## Service difficulty reports (135, newest 50)

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

- [SDR FDEA201604131201](https://openairdocs.org/sdr/FDEA201604131201), Apr 13, 2016: COMPUTER. FAILED. STAB TRIM WAS SET AT 6.2 FOR TAKEOFF WHICH WAS IN THE MIDDLE OF THE GREEN BOX. AT 80KTS STAB FLICKERED TO 6.2, WENT AMBER, STAB TRIM AURAL WARNING WENT OFF TWIC
- [SDR FDEA201511283811](https://openairdocs.org/sdr/FDEA201511283811), Nov 28, 2015: FAIRING. SEPARATED. ELP MX REPORTED PART FOUND ON RUNWAY AFTER TAKEOFF. INSPECTED ACFT FOUND THE NR 2 ENG LT SIDE TAIL PYLON & FAN DUCT RAMP FAIRING. IPC 54-22-15-01 ITEM 720, MISS
- [SDR FDEA201502180540](https://openairdocs.org/sdr/FDEA201502180540), Feb 18, 2015: LIGHT. INOPERATIVE. L1 DOOR SLIDE FAILS PRESS TO TEST. RELAMPED L1 DOOR EMER ESCAPE SLIDE PRESSURE, PRESS TO TEST, INDICATOR LAMP AS REQUIRED. OPERATIONS CHECKED NORMAL IAW AMM 25-
- [SDR FDEA201412244167](https://openairdocs.org/sdr/FDEA201412244167), Dec 24, 2014: WIRE HARNESS. DAMAGED. DURING INITIAL CLIMB, NR 1 ENGINE EXCEEDED 1051 DEGREES EGT. NO FIRE INDICATIONS, NO ABNORMAL AIRFRAME MOVEMENTS. RAN QRH SHUTDOWN THE ENGINE. TROUBLESHOT IAW S
- [SDR FDEA201410163186](https://openairdocs.org/sdr/FDEA201410163186), Oct 16, 2014: ATTACH ANGLE. CRACKED. DURING HIGH FREQUENCY EDDY CURRENT INSPECTION, FOUND A CRACK AT RT WING STRINGER BUTTERFLY CLIP AT XORS 402 STRINGER 39, APPROX 0.5 INCHES IN LENGTH. REMOVED AN
- [SDR FDEA201410113110](https://openairdocs.org/sdr/FDEA201410113110), Oct 11, 2014: BRACKET. CORRODED. RIGHT WING INBD FLAP ASSEMBLY AFT HINGE OTBD PIVOT BORE HAS SURFACE CORROSION. REWORKED AND FOUND OUT OF LIMITS IAW CMM 57- 52-01. REPAIRED PER EA 8-5750-T03122
- [SDR FDEA201410083008](https://openairdocs.org/sdr/FDEA201410083008), Oct 8, 2014: SUPPORT FITTING. CORRODED. AFTER REMOVAL OF CENTER WING TANK, TOP SURFACE SUPPORT FITTING FOUND CORRODED BS 1361 X = 31. SUPPORT FITTING REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II. R
- [SDR FDEA201410062986](https://openairdocs.org/sdr/FDEA201410062986), Oct 6, 2014: FLOORBEAM. CORRODED. FORWARD CARGO BAY SUMP AREA BS 959 RBL 7 FLOORBEAM FOUND CORRODED. FLOORBEAM REMOVED AND REPLACED IAW SRM 51-31-01 VOLUME II. FLOORBEAM REWORKED IAW DRAWING ADA
- [SDR FDEA201410062985](https://openairdocs.org/sdr/FDEA201410062985), Oct 6, 2014: TEE FITTING. CORRODED. LEFT WW FWD BULKHEAD SLAT PANEL ATTACH TEE FITTING INBD SIDE FOUND WITH CORROSION. REMOVED AND REPLACED IAW AMM 20-50-02 AND DRAWING NPB6072 REVISION AL. REPAIR
- [SDR FDEA201410062984](https://openairdocs.org/sdr/FDEA201410062984), Oct 6, 2014: SKIN. CRACKED. LOWER FUSELAGE SKIN AT BS 1156 CRACKED. REPAIR IAW EA 8-5310-T0312350 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201410062983](https://openairdocs.org/sdr/FDEA201410062983), Oct 6, 2014: SKIN. CRACKED. LEFT WING DROOP LE AFT SURFACE FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 55 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201410062982](https://openairdocs.org/sdr/FDEA201410062982), Oct 6, 2014: SKIN. CRACKED. RIGHT WING DROOP LE AFT UPPER SURFACE FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 55 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201410062981](https://openairdocs.org/sdr/FDEA201410062981), Oct 6, 2014: SKIN. CHAFED. RIGHT WING DROP LE OTBD UPPER SURFACE AT XDLE 328 FOUND WITH CHAFED. REPAIRED IAW SRM 57-10-00 FIGURE 97 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201410062977](https://openairdocs.org/sdr/FDEA201410062977), Oct 6, 2014: FORMER. CRACKED. RIGHT WING LE COMPARTMENT FIXED LE RIB ATTACHED FORMER AT XOS 584 FOUND CRACKED. CRACKED FORMER REMOVED AND REPLACED IAW DRAWING ARB1162 REVISION S AND SRM 51-3
- [SDR FDEA201410062976](https://openairdocs.org/sdr/FDEA201410062976), Oct 6, 2014: ATTACH FITTING. CORRODED. LEFT WHEEL WELL FWD BULKHEAD PANEL INBD ATTACHMENT FITTING FOUND CORRODED. FITTING REMOVED AND REPLACED IAW SRM 51-31-01 VOLUME II. REPAIR CLASSIFIED AS MAJOR I
- [SDR FDEA201410062975](https://openairdocs.org/sdr/FDEA201410062975), Oct 6, 2014: DOUBLER. CRACKED. RIGHT WING INBD FLAP ASSEMBLY, ENCLOSURE AREA SIDE LOAD FITTING CUT OUT DOUBLER CRACKED. REPAIRED IAW EA 8-5340-T0312333 PART 1. REPAIR CLASSIFIED AS MAJOR IAW 
- [SDR FDEA201410062980](https://openairdocs.org/sdr/FDEA201410062980), Oct 6, 2014: DOUBLER. CRACKED. RIGHT WING LE BEADED DOUBLER AT XOS 587 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201410062979](https://openairdocs.org/sdr/FDEA201410062979), Oct 6, 2014: DOUBLER. CRACKED. RIGHT WING LE BEADED DOUBLER AT XOS 908 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201410062978](https://openairdocs.org/sdr/FDEA201410062978), Oct 6, 2014: DOUBLER. CRACKED. RIGHT WING LE BEADED DOUBLER AT STATION XOS 665 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201410042957](https://openairdocs.org/sdr/FDEA201410042957), Oct 4, 2014: LONGERON. CORRODED. FORWARD CARGO BILGE AREA FOUND LONGERON 52 CORRODED BETWEEN BS 780 & 790. REMOVED AND REPLACED THE LONGERON IAW SRM 51-31-01 VOLUME II AND DRAWING ADA8098. REPA
- [SDR FDEA201410042956](https://openairdocs.org/sdr/FDEA201410042956), Oct 4, 2014: SEAT TRACK. CRACKED. BS 1471 LBL 27.5 SEAT TRACK FOUND CRACKED. REPAIRED IAW SRM 53-70- 00 FIGURE 1 VOLUME I. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201410042954](https://openairdocs.org/sdr/FDEA201410042954), Oct 4, 2014: SKIN. CRACKED. LEFT WING NR 3 SLAT LOWER SURFACE AT STATION XOS 418 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 43 VOLUME I AND EA 8-5750-T0312515 PART 1. REPAIR CLASSIFIE
- [SDR FDEA201410042955](https://openairdocs.org/sdr/FDEA201410042955), Oct 4, 2014: DOUBLER. CRACKED. LEFT WING LE BEADED DOUBLER AT XOS 545 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201410022919](https://openairdocs.org/sdr/FDEA201410022919), Oct 2, 2014: STRINGER. CRACKED. RIGHT WING LE STRINGER AT XOS 666 FOUND CRACKED. REPAIRED IAW EA 8-5710-T0312188 PART 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201410022918](https://openairdocs.org/sdr/FDEA201410022918), Oct 2, 2014: STRINGER. CRACKED. LEFT WING LE STRINGER AT XOS 666 FOUND CRACKED. REPAIRED IAW EA 8-5710-T0312186 PART 1. . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201410022917](https://openairdocs.org/sdr/FDEA201410022917), Oct 2, 2014: RIB. CRACKED. LEFT WING LE RIB DOUBLER AT XOS 667 FOUND CRACKED. RIB REMOVED AND REPLACED IAW SRM 51-33-01 VOLUME II. NEW RIB DOUBLER FABRICATED IAW DRAWING ARB1249 REVISION 
- [SDR FDEA201410022920](https://openairdocs.org/sdr/FDEA201410022920), Oct 2, 2014: DOUBLER. CRACKED. RIGHT WING LE BEADED DOUBLER AT XOS 668 FOUND CRACKED. REPAIRED IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASIFIED MAJOR IAW GMM 6-2-100..
- [SDR FDEA201410022916](https://openairdocs.org/sdr/FDEA201410022916), Oct 2, 2014: DOUBLER. CRACKED. LEFT WING LE BEADED DOUBLER AT XOS 668 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201410022915](https://openairdocs.org/sdr/FDEA201410022915), Oct 2, 2014: DOUBLER. CRACKED. LEFT WING LE BEADED DOUBLER AT XOS 666 FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-10-00 FIGURE 71 VOLUME I. REPAIR CLASIFIED MAJOR IAW GMM 6-2-100.
- [SDR FDEA201408162190](https://openairdocs.org/sdr/FDEA201408162190), Aug 16, 2014: CONNECTOR. LOOSE. ON FIGHT CREW PREFLIGHT FOUND EMER LIGHTING SYS INOPERATIVE. FOUND CONNECTOR P1-203 PARTIALLY DISCONNECTED. RECONNECTED P1-203 IAW SWPM. EMER LIGHTS OPERATIONS 
- [SDR FDEA201405291229](https://openairdocs.org/sdr/FDEA201405291229), May 29, 2014: PROXIMITY SENSOR. DEFECTIVE. PASSING 25K' NOSE GEAR RED UNSAFE CYCLED ON & OFF SEVERAL TIMES THEN HELD STEADY. SLOWED & DESCENDED TO CYCLE GEAR. NOSE UP & LOCKED, BUT MAINS WOULD NOT. SLOWE
- [SDR FDEA201405231148](https://openairdocs.org/sdr/FDEA201405231148), May 23, 2014: SENSOR. MALFUNCTIONED. CLIMBING THROUGH 5000 FT, RECEIVED AN INTERMITTENT, THEN STEADY UNSAFE NLG ON BOTH THE SYNOPTIC & GEAR HANDLE LIGHT. CYCLED GEAR IAW QRH & NLG INDICATED SAFE. R
- [SDR FDEA201309122200](https://openairdocs.org/sdr/FDEA201309122200), Sep 12, 2013: INDICATOR. INOPERATIVE. DURING PREFLIGHT, FOUND LEFT ENTRY DOOR EVACUATION SLIDE REMOTE PRESSURE PRESS-TO-TEST INDICATING SYS LIGHT INOPERATIVE. REMOVED AND REPLACED THE L1 DOOR PRESSU
- [SDR FDEA201307201602](https://openairdocs.org/sdr/FDEA201307201602), Jul 20, 2013: PUMP. FAILED. REJECTED TAKEOFF DUE TO NR 1 ENGINE ROLL BACK AT 95 KTS. R & R THE MEC AND FUEL PUMP.
- [SDR FDEA201307181583](https://openairdocs.org/sdr/FDEA201307181583), Jul 18, 2013: SWITCH. INOPERATIVE. L1 DOOR BOTTLE PRESSURE LIGHT DOESN`T TEST. R & R L1 DOOR PRESSURE INDICATOR SWITCH. OPS CHECKED GOOD.
- [SDR FDEA201307011429](https://openairdocs.org/sdr/FDEA201307011429), Jul 1, 2013: BOTTLE. NO TEST. LIFE RAFT BOTTLE FAILED TEST, DURING PREFLT TEST. INSTALLED CORRECT BULBS,PERFORMED OPS CHECK PER MM 25-61-01-2. SLIDE LIGHT OPS CHECKED GOOD.
- [SDR FDEA201306261403](https://openairdocs.org/sdr/FDEA201306261403), Jun 26, 2013: SMOKE DETECTOR. FALSE ACTIVATION. CLIMBING THROUGH 18000' TRI-TONE WARNING ANNUNCIATING A "CARGO FIRE LOWER" OCCURED FOR APPROX 5 SECONDS (2 CYCLES OF THE TRI-TONE). HAPPENED FOUR TIMES. INITIAT
- [SDR FDEA201301250177](https://openairdocs.org/sdr/FDEA201301250177), Jan 25, 2013: CONTROLLER. MALFUNCTIONED. CABIN PRESSURE UNCONTROLLABLE AFTER TAKEOFF, RTB. R & R CABIN OUTFLOW ACTUATOR, RIG & FUNCTIONAL CHECK GOOD IAW REF MM 21-31-20-4, MM 21-31-01/501. PERFORMED RT
- [SDR FDEA201210273763](https://openairdocs.org/sdr/FDEA201210273763), Oct 27, 2012: WIRE. BROKEN. LT DOOR SLIDE INDICATION SYS INOPERATIVE. REMOVED BROKEN PRESS TO TEST LAMP AND PULLED PLUG FROM TEST LIGHT JACK IN L1 DOOR. FOUND BROKEN WIRE ON POWER UNIT ASS
- [SDR FDEA201107293032](https://openairdocs.org/sdr/FDEA201107293032), Jul 29, 2011: POWER SUPPLY. INOPERATIVE. DURING COCKPIT SET UP, EMERGENCY LIGHTS TEST RECEIVED A LEVEL ONE ALERT. EMERGENCY LIGHT TEST FUNCTION - INOP. R & R EMERGENCY POWER SUPPLY IAW MM 33-51-4-0. OP
- [SDR FDEA201107283008](https://openairdocs.org/sdr/FDEA201107283008), Jul 28, 2011: POWER SUPPLY. FAILED. DURING COCKPIT SET UP, EMERGENCY LIGHTS TEST RECEIVED A LEVEL ONE ALERT: EMERGENCY LIGHT BATTERY ONE LOW. REMOVED AND REPLACED EMERGENCY POWER SUPPLY AS PER MM 
- [SDR FDEA201106052128](https://openairdocs.org/sdr/FDEA201106052128), Jun 5, 2011: RELAY. MALFUNCTIONED. ATTEMPTED TO DUMP FUEL FOR RTB MEM AT APPROX 35K AT START OF DUMP, COULD NOT GET NORMAL DUMP TO OCCUR, EVEN AFTER SELECTING DUMP A SECOND TIME. GOT FUEL DUMP VA
- [SDR FDEA201103221110](https://openairdocs.org/sdr/FDEA201103221110), Mar 22, 2011: CONTROL CABLE. BINDING. NR 2 THROTTLE JAMMED AT CRUISE POWER SETTING. UNABLE TO CONTROL THROTTLE POSITION DURING DESCENT AND APPROACH. SHUTDOWN NR 2 ENG IAW QRH. AFTER LANDING DURING T
- [SDR FDEA201011274498](https://openairdocs.org/sdr/FDEA201011274498), Nov 27, 2010: LANDING GEAR. MALFUNCTIONED. DURING LANDING GEAR RETRACTION, THE LT MLG PRIMARY AND SECONDARY INDICATIONS, INDICATED UNSAFE. CHECK LIST WAS ACCOMPLISHED. GEAR WAS EXTENDED AND RETRACTED. AL
- [SDR FDEA201011204434](https://openairdocs.org/sdr/FDEA201011204434), Nov 20, 2010: SKIN. CRACKED. LT WING REAR SPAR LOWER CAP AT XORS 345, HFEC OPEN HOLE INSP. FOUND 01EA FASTENER HOLE WITH CRACKED INDICATION. LEFT HAND WING REAR SPAR LOWER CAP AT XORS 345, 
- [SDR FDEA201011104303](https://openairdocs.org/sdr/FDEA201011104303), Nov 10, 2010: SKIN. CRACKED. RT WING ANTI ICE TELESCOPIC DUCT CUTOUT FOUND CRACKED. RT WING ANTI ICE TELESCOPIC DUCT CUTOUT CARRIED OUT REPAIR IAW NR 8-5710-143471, REPAIR CLASSIFIED AS MAJ
- [SDR FDEA201011104302](https://openairdocs.org/sdr/FDEA201011104302), Nov 10, 2010: SKIN. CRACKED. LT WING ANTI ICE TELESCOPIC DUCT CUTOUT FOUND CRACKED. LT WING ANTI ICE TELESCOPIC DUCT CUTOUT CARRIED OUT REPAIR IAW EA NR 8-5710-143470, REPAIR CLASSIFIED AS 
- [SDR FDEA201011034235](https://openairdocs.org/sdr/FDEA201011034235), Nov 3, 2010: SKIN. CHAFED. LT WING SLAT NR 4 UPPER SURFACE FOUND CHAFED. REMOVED AND CLEANED AS PER SRM 57-00-01 FIGURE 1A, VOLUME I, REVISION 96. REPAIR CLASSIFIED AS MINOR PER GMM 6-2-1
- [SDR FDEA201011024228](https://openairdocs.org/sdr/FDEA201011024228), Nov 2, 2010: SKIN. CRACKED. LT WING FIXED L/E FWD INBD SIDE OF PRESSURE REFUEL PANEL CUTOUT FOUND REPAIR DOUBLER CRACKED. CARRIED OUT RECTIFICATION AS PER E.A. 8-5730-143796, REPAIR CLASSI
- [SDR FDEA201011024227](https://openairdocs.org/sdr/FDEA201011024227), Nov 2, 2010: SKIN. CRACKED. WHILE CARRYING OUT WALK AROUND CHECK FOUND RT WING FUEL DUMP ISLAND UPPER SURFACE OTBD AREA EDGE WITH CRACK APPROX .5". REPAIRED AS PER EA 8-5750-143479, REPAIR

All 135: https://openairdocs.org/deregistered/N373FE-2024-01-29/reports.md

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