# N368FE: 1971 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: 46606
- Year built: 1971
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: July 18, 2005
- Certificate issued: October 25, 1997
- Last registry action: June 3, 2023
- Mode S code: A42A86
- 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/N368FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=368FE
- Page: https://openairdocs.org/deregistered/N368FE-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 (116, newest 50)

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

- [SDR FDEA201912283324](https://openairdocs.org/sdr/FDEA201912283324), Dec 28, 2019: BULKHEAD. CRACKED. LH BULKHEAD IN NLG WHEEL WELL IS CRACKED. REPAIRED NOSE LANDING GEAR WHEEL WELL UPPER LEFT SIDE WEB STA 490 IN REF TO MD-10 SRM 53-30-00 FIG #6 VOL I
- [SDR FDEA2019123183324](https://openairdocs.org/sdr/FDEA2019123183324), Dec 28, 2019: BULKHEAD. CRACKED. LH BULKHEAD IN NLG WHEEL WELL IS CRACKED. REPAIRED NOSE LANDING GEAR WHEEL WELL UPPER LEFT SIDE WEB STA 490 IN REF TO MD-10 SRM 53-30-00 FIG #6 VOL I
- [SDR FDEA2019062751404](https://openairdocs.org/sdr/FDEA2019062751404), Jun 25, 2019: ROLLER. OUT OF ALIGNMENT. ON POST FLT CHECK, THE L1 DOOR WOULD NOT OPEN ELECTRICALLY. REALLIGNED L1 DOOR UPPER AFT BOGIE ROLLER ASSEMBLY INTO ITS TRACK, REINSTALLED LOWER DOOR LINER. PRE
- [SDR FDEA201806291601](https://openairdocs.org/sdr/FDEA201806291601), Jun 29, 2018: ADIRU. INOPERATIVE. DESCENDING BELOW 24K FEET, RECEIVED AN IAS COMPARATIVE FLAG ON THE PFD. HAD ABOUT A 5-8 KT DIFFERENCE BETWEEN FIRST OFFICER`S AND CAPTAIN'S AIRSPEED. DIFFERENCE
- [SDR FDEA201805181255](https://openairdocs.org/sdr/FDEA201805181255), May 18, 2018: WARNING MESSAGE. FALSE ACTIVATION. IGN OVD ON, ENG ANTI ICE ON, WING ANTI ICE ON, PACKS 1 & 3 ON, PACK 2 OFF. LVL III AIR MANIFOLD 1 FAIL ALERT, WING ANTI ICE 1 ALERT, LVL II AND LVL 1 AIR SYS 1 
- [SDR FDEA201801160170](https://openairdocs.org/sdr/FDEA201801160170), Jan 16, 2018: FITTING. CRACKED. NR 1 PYLON AFT BULKHEAD FITTING O/B FWD ATTACH HOLE COMMON TO UPPER SPAR WEB CRACKED. REMOVED & REPLACED NR 1 PYLON AFT BULKHEAD FITTING PER DWG AUB7025-13 & SR
- [SDR FDEA201801140328](https://openairdocs.org/sdr/FDEA201801140328), Jan 14, 2018: HINGE. CORRODED. CENTER CARGO DOOR AFT HINGE HALF SECTION ON DOOR SIDE CORRODED BEYOND LIMITS. REMOVED AND REPLACED HINGE HALF REF DAC DWG AFA3803 AND EA 8-5230-T0338044.
- [SDR FDEA201801140119](https://openairdocs.org/sdr/FDEA201801140119), Jan 14, 2018: SEAT TRACK. GOUGED. MAIN DECK SEAT TRACK, BS 755, LBL 47 GOUGED AT TWO PLACES. REPLACED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL 1, SRM 51-31-01, VOL. 2, AND SR10-53-002.
- [SDR FDEA201801110093](https://openairdocs.org/sdr/FDEA201801110093), Jan 11, 2018: HINGE. CORRODED. FWD CARGO DOOR HINGES ARE RUSTY. REMOVED SURFACE RUST, PRIMED AND PAINTED REF SRM 52-10-00 FIG 8 SHEET 1 VOL 2 AND SRM 51-21-02 PAGE 1-9 VOL 2.
- [SDR FDEA201801110056](https://openairdocs.org/sdr/FDEA201801110056), Jan 11, 2018: BOLT. SHEARED. LEFT MLG WHEEL WELL, BS 1370, TRAPEZOID PANEL HORIZONTAL STRUCTURE BEAM HAS A SHEARED BOLT.
- [SDR FDEA201801090104](https://openairdocs.org/sdr/FDEA201801090104), Jan 9, 2018: SEAT TRACK. GOUGED. MAIN CABIN SEAT TRACK GOUGED AT LBL 27.5, BS 615 AND 621 ON THE UPPER SURFACES. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL 1.
- [SDR FDEA201801090100](https://openairdocs.org/sdr/FDEA201801090100), Jan 9, 2018: SEAT TRACK. DAMAGED. MAIN CARGO, BS 1135 - 1139 SEAT-TRACK GOUGED AT RBL 47.5. REPLACED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL 1, SRM 51-31-01, VOL 2, AND SR10-53-002
- [SDR FDEA201801090074](https://openairdocs.org/sdr/FDEA201801090074), Jan 9, 2018: SEAT TRACK. DAMAGED. MAIN DECK SEAT TRACK STA 1421, 8.5 LT DAMAGED. REMOVED DAMAGE AND INSTALLED PLUG REF SRM 53-70-00 FIG 2 SHEET 1, VOL 1.
- [SDR FDEA201801080092](https://openairdocs.org/sdr/FDEA201801080092), Jan 8, 2018: HINGE. CORRODED. FWD CARGO DOOR, RUST EMANATING FROM HINGE. REMOVED SURFACE RUST, PRIME AND PAINT REF SRM 52-10-00 FIG 8 SHEET 1 VOL 2 AND SRM 51-21-02 PAGE 1-9 VOL 2.
- [SDR FDEA201705241491](https://openairdocs.org/sdr/FDEA201705241491), May 24, 2017: GIRT BAR. DETACHED. FOUND THE L1 GIRT BAR HANGING FROM OPEN DOOR. REINSTALLED GIRT BAR BACK INTO HOLDONG CLIPS ON THE L1 DOOR IAW AMM 25-61-01-2, OK FOR CONTINUED USE AT THIS TIME.
- [SDR FDEA201703230983](https://openairdocs.org/sdr/FDEA201703230983), Mar 23, 2017: WIRE HARNESS. DAMAGED. AFTER TAKEOFF, WHEN GEAR HANDLE SELECTED UP. RECEIVED AN UNSAFE LEFT MAIN GEAR ON BOTH PRIMARY & SECONDARY. REVIEWED QRH RESULTING IN PUTTING GEAR HANDLE DOWN A
- [SDR FDEA201701190226](https://openairdocs.org/sdr/FDEA201701190226), Jan 19, 2017: DOOR. OUT OF ADJUST. CANNOT ARM L1 DOOR. PERFORMED ADJUSTMENT TEST OF THE 1L DOOR IAW AMM 25-61-02-5. OPS CHECKED GOOD.
- [SDR FDEA201609033113](https://openairdocs.org/sdr/FDEA201609033113), Sep 3, 2016: PRESSURE SWITCH. FAILED. APPROXIMATELY 2 AT 15 AFTER TAKEOFF FL 350 GOT AIR MFG NR 1 FAIL, LEVEL 3 ALERT. 1 THROTTLE TO IDLE IAW QRH. NR 1 AIR SYSTEM TEMP AND AIR PRESSURE DECREASED, DI
- [SDR FDEA201602240682](https://openairdocs.org/sdr/FDEA201602240682), Feb 24, 2016: DOOR. CRACKED. R4 LOWER CORNER HAS CRACK. REMOVED CRACK & INSTALLED DOUBLER.
- [SDR FDEA201602220673](https://openairdocs.org/sdr/FDEA201602220673), Feb 22, 2016: TEE FITTING. CRACKED. STATION 595, BULKHEAD T CAP VERTICAL LEG, AT LONGERON 36L HAS A 1.0 INCH CRACK. REPAIRED IAW EA 8-5310-T0323068.
- [SDR FDEA201602190629](https://openairdocs.org/sdr/FDEA201602190629), Feb 19, 2016: SEAT TRACK. DAMAGED. DAMAGED SEAT TRACK. REPLACED DAMAGED SEAT TRACK.
- [SDR FDEA201602190628](https://openairdocs.org/sdr/FDEA201602190628), Feb 19, 2016: SEAT TRACK. DAMAGED. DAMAGED SEAT TRACK. REPLACED DAMAGED SEAT TRACK.
- [SDR FDEA201602160589](https://openairdocs.org/sdr/FDEA201602160589), Feb 16, 2016: TEE FITTING. CRACKED. LEFT LOWER BS 595, BULKHEAD T CAP VERTICAL LEG AT LONGERON 39L, HAS A TWO INCH CRACK. REPAIRED IAW EA 8-5310-T0323068.
- [SDR FDEA201602160588](https://openairdocs.org/sdr/FDEA201602160588), Feb 16, 2016: TEE FITTING. CRACKED. LEFT LOWER BS 595, BULKHEAD TED CAP VERTICAL LEG AT LONGERON 39L, HAS A TWO INCH CRACK. REPAIRED THE TEE IAW EA 8-5310-T0323068.
- [SDR FDEA201602160587](https://openairdocs.org/sdr/FDEA201602160587), Feb 16, 2016: BULKHEAD. CRACKED. LEFT SIDE STATION 595, BULKHEAD WEB AT LONGERON 36L HAS A .300 INCH CRACK. NDT AREA FABRICATED & INSTALLED DOUBLERS & FILLER IAW SRM 53-40-00 VOL 1.
- [SDR FDEA201602100498](https://openairdocs.org/sdr/FDEA201602100498), Feb 10, 2016: SKIN. CRACKED. LEFT FWD PAX DOOR, AFT LOWER CORNER, HAS A CRACK INDICATION AT THE LOWER FASTENER IN THE RADIUS. CUT OUT DAMAGED AREA & INSTALLED THREE DOUBLERS IAW EA 8-5330-T
- [SDR FDEA201602100496](https://openairdocs.org/sdr/FDEA201602100496), Feb 10, 2016: SKIN. CRACKED. RIGHT AFT PAX DOOR, FWD LOWER CORNER HAS A CRACK INDICATION AT THE LOWER FASTENER IN THE RADIUS. REMOVED CRACK & INSTALLED DOUBLER IAW DWG SR10530084.
- [SDR FDEA201602090491](https://openairdocs.org/sdr/FDEA201602090491), Feb 9, 2016: CAP. CRACKED. FORWARD CARGO, STATION 595 BULKHEAD T CAP VERTICAL LEG AT LONGERON 39R HAS A .300 INCH CRACK AT THE LOWER FASTENER. REPAIRED T CAP IAW EA 8-5310-T0323071 P1.
- [SDR FDEA201602080488](https://openairdocs.org/sdr/FDEA201602080488), Feb 8, 2016: BEAM. CRACKED. FORWARD CARGO, STATION 595 BULKHEAD, LOWER HORIZONTAL BEAM Z = -80, UPPER & LOWER SURFACE, CTR AREA, IS CRACKED. INSTALLED REPAIRED DOUBLERS IAW SRM 53-40-00 FI
- [SDR FDEA201602020419](https://openairdocs.org/sdr/FDEA201602020419), Feb 2, 2016: SKIN. CRACKED. LEFT WING LE LOWER SURFACE, FUELING PANEL 519CB CUT OUT, FWD INBD CORNER IS CRACKED. REPAIRED REF SRM 57-10-00 VOL 1 REPAIR 100. REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201509242932](https://openairdocs.org/sdr/FDEA201509242932), Sep 24, 2015: HARNESS. FAILED. AT CRUISE GOT, ENG 2 EXCEEDANCE, EGT 960. AFTER ENG SHUTDOWN GAUGE FLOATED BETWEEN 0 - 600. COMPLIED WITH TSI 77-20/5735. R&R 4(EA) EGT THERMOCOUPLE LEADS PER M
- [SDR FDEA201508132544](https://openairdocs.org/sdr/FDEA201508132544), Aug 13, 2015: DOOR. OUT OF ADJUST. L1 DOOR APPEARS TO BIND WHEN CLOSING SHUTTERS & SHAKES. NORMAL OPERATION WHEN OPENING. REMOVED L1 DOOR AFT SPROCKET DRIVE CABLE ASSEMBLY IAW AMM 52-11-09-2. INS
- [SDR FDEA201506262095](https://openairdocs.org/sdr/FDEA201506262095), Jun 26, 2015: INDICATOR. DEFECTIVE. DOOR 1R PRESS TO TEST LIGHT DOES NOT TEST PROPERLY. AMM 25-61-03-2-0 R & R SLIDE PACK INDICATOR ASSEMBLY. CHECKED OK.
- [SDR FDEA201506231959](https://openairdocs.org/sdr/FDEA201506231959), Jun 23, 2015: INDICATOR. INOPERATIVE. DURING PREFLIGHT CHECK R1 DOOR SLIDE DISARM LIGHT INOPERATIVE. REMOVED AND REPLACED SLIDE PACK INDICATOR ASSY. CHECKS OK
- [SDR FDEA201407171842](https://openairdocs.org/sdr/FDEA201407171842), Jul 17, 2014: FLAP. CHAFED. RIGHT WING INBD TE FLAP LE ABOVE FLAP FAIRING FWD END HAVE DEEP CHAFED MARK. REPAIRED RT WING INBD TE FLAP LE IAW SRM 57-10-00 FIG 86. TRACKED ON EA 8-5710-T030
- [SDR FDEA201407171838](https://openairdocs.org/sdr/FDEA201407171838), Jul 17, 2014: SKIN. DAMAGED. FLIGHT CONTROLS LT INBD AILERON LOWER SKIN DAMAGE. COMPLY WITH EA 8-2710-T0308548 REV NO POS P3. THIS WRITE UP IS A WORK RELEASE ITEM SEQ 000669 WRI 27104334. N
- [SDR FDEA201407171829](https://openairdocs.org/sdr/FDEA201407171829), Jul 17, 2014: SUPPORT ANGLE. CRACKED. AFT CARGO DOOR AFT LOWER CUT OUT CORNER WEB SUPPORT ANGLE IS CRACKED. REMOVED & INSTALLED NEW T BRACKET PN AFA 3933-1 BATCH 0002646676 IAW SRM 51-31-01. REMOVED
- [SDR FDEA201407051635](https://openairdocs.org/sdr/FDEA201407051635), Jul 5, 2014: SEAT TRACK. CORRODED. AFT CARGO COMPARTMENT BETWEEN STATION 1787 & 1841 SEAT TRACK X= 52.70 CORRODED. FOUND TO BE OUT OF LIMITS IAW SRM DC-1053-42-01 & SRM 53-00-01 FIG 1A. MATERIAL 
- [SDR FDEA201405030920](https://openairdocs.org/sdr/FDEA201405030920), May 3, 2014: ACCESS PANEL. MISSING. DURING WALK AROUND AFTER ACFT ARRIVED, FOUND NR 1 ENGINE PYLON INSPECTION PANEL 437JL BROKEN OFF & MISSING. REPAIRED IAW E.A 8-5480-T0307890 REV.
- [SDR FDEA201208283196](https://openairdocs.org/sdr/FDEA201208283196), Aug 28, 2012: WIRE. FAILED. ONE HOUR INTO FLIGHT NOTICED TANK 2 QTY 8000 LBS LESS THAN TANKS 1&3. TROUBLESHOT PER FIM 28-41 AND FOUND NR 2 TANK RT COMPENSATOR PROBE WIRE WAS LOOSE AT RIVET
- [SDR FDEA201208243184](https://openairdocs.org/sdr/FDEA201208243184), Aug 24, 2012: FUEL CELL. LEAKING. "TANK 2 PUMP OFF" FOLLOWED BY " NR 2 CROSSFEED" ABOUT 1 HOUR INTO FLIGHT. NR 2 QTY INDICATED ALMOST 5000 POUNDS LESS THAN 1 AND 3. FOLLOWED QRH AND IN MANUAL AL
- [SDR FDEA201207202629](https://openairdocs.org/sdr/FDEA201207202629), Jul 20, 2012: SENSOR. OBSTRUCTED. UNSAFE UP LEFT GEAR ON BOTH GEAR HANDLE DISPLAY AND ON CONFIGURATION PAGE. SAFE DOWN INDICATION. FOUND CONDUIT FOR THE UP AND LOCKED SENSOR ROUTED INCORRECTLY A
- [SDR FDEA201207172596](https://openairdocs.org/sdr/FDEA201207172596), Jul 17, 2012: BULKHEAD. CRACKED. CENTER WHEEL WELL HAS ONE CRACK ON LT SIDEWALL 32" FWD OF STA Y1521 AND 19" DOWN FROM UPPER BULKHEAD. REPAIRED LT WHEEL WELL SIDEWALL IAW EA 8-5310-157347.
- [SDR FDEA201207112595](https://openairdocs.org/sdr/FDEA201207112595), Jul 11, 2012: BULKHEAD. CRACKED. CENTER WHEEL WELL HAS THREE CRACKS ON LT SIDEWALL 16" AFT OF STA Y1381 AND 5" DOWN FROM UPPER BULKHEDD. REPAIRED IAW EA 8-5310-157348, SEQ NR 240.
- [SDR FDEA201206062105](https://openairdocs.org/sdr/FDEA201206062105), Jun 6, 2012: SKIN. MISREPAIRED. SKIN MISREPAIRED AT BS 1907 BETWEEN LONGERON 19 AND 20 RIGHT. REPAIR CARRIED OUT IAW SRM 53-20-00, FIG 6, VOL I, REV 98. EO 8-5100-7-5000 A4, PART 2. REPAIR CLA
- [SDR FDEA201205292001](https://openairdocs.org/sdr/FDEA201205292001), May 29, 2012: RAIL. CRACKED. RAIL CRACKED. REPAIRED IAW EA 8-5330-159845, PART 1C AND 1D. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
- [SDR FDEA201205181872](https://openairdocs.org/sdr/FDEA201205181872), May 18, 2012: SKIN. MISREPAIRED. FUSELAGE SKIN BS 1079, LONGERON 52 LEFT MISREPAIRED. REPAIR CARRIED OUT IAW SRM 53-20-00, FIG 7, VOL I, REV 98. EO E8-5100-7-5000 A4, PART 2. REPAIR CLASSIFIED 
- [SDR FDEA201205181871](https://openairdocs.org/sdr/FDEA201205181871), May 18, 2012: SKIN. MISREPAIRED. FUSELAGE SKIN BS 715 BETWEEN LONGERON 39 AND 40 LT MISREPAIRED. REPAIRED IAW SRM 53-20-00, FIG 6, VOL I, REV 98. EO E8-5100-7-5000 A4, PART 2. REPAIR CLASSIFIED
- [SDR FDEA201205181869](https://openairdocs.org/sdr/FDEA201205181869), May 18, 2012: SKIN. MISREPAIRED. FUSELAGE SKIN BS 840, LONGERON 43 RT MISREPAIRED. REPAIR CARRIED OUT IAW EA 8-5330-159845, PART 1A AND 1B. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114.
- [SDR FDEA201205181868](https://openairdocs.org/sdr/FDEA201205181868), May 18, 2012: SKIN. MISREPAIRED. CARGO DOOR CUT-OUT FWD SKIN AT STA 879 BETWEEN LONGERON 41 RT AND LONGERON 43 RT MISREPAIRED. CARRIED OUT REPAIR IAW EA 8-5330-160619 PART 1. REPAIR CLASSIFIED 

All 116: https://openairdocs.org/deregistered/N368FE-2024-03-02/reports.md

## 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 20030524009299I](https://openairdocs.org/incident/20030524009299I), May 24, 2003: Doug DC1010F (N368FE), Oakland, CA, Substantial damage. (-23) Federal express aircraft N368FE, DC-10-10/87 serial number 46606, departed Oakland international at 0602PDT on 05/24/2003 for flt 3103 enroute to fort…

---
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.