# N68054: 1975 Mcdonnell Douglas MD-10-10F, registration cancelled 2024-02-03

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 3, 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: 47808
- Year built: 1975
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 16, 2006
- Certificate issued: April 10, 1980
- Last registry action: October 20, 2023
- Mode S code: A9065B
- 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/N68054
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=68054
- Page: https://openairdocs.org/deregistered/N68054-2024-02-03

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 (186, newest 50)

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

- [SDR FDEA201406081356](https://openairdocs.org/sdr/FDEA201406081356), Jun 8, 2014: SKIN. CRACKED. FOUND RT WING CRACKED JUST ABOVE ANTI-ICE TELESCOPING DUCT CUT OUT. ACCOMPLISH HFEC IAW NTM PT6 20-30-00. REPAIRED IAW EA 8-5710-T0308735 P1 AND SRM 57-40-01 RE
- [SDR FDEA201406081357](https://openairdocs.org/sdr/FDEA201406081357), Jun 8, 2014: SKIN. CRACKED. RIGHT WING FUEL PNL DOOR CUT OUT HAS A 1"X1/8" STRIP OF PAINT MISSING & LOOKS LIKE A POSSIBLE CRACK. REQUESTED NDT VERIFY. CONFIRMED & MARKED END CRACK LOCATED 
- [SDR FDEA201212134289](https://openairdocs.org/sdr/FDEA201212134289), Dec 13, 2012: LIGHT. INOPERATIVE. R1 DOOR SLIDE TEST LIGHT INOPERATIVE. REMOVED AND REPLACED PRESSURE INDICATION LIGHT ASSY IAW AMM 25-61-03-2, OPS CHECKED GOOD. OK FOR SERVICE.
- [SDR FDEA201206072130](https://openairdocs.org/sdr/FDEA201206072130), Jun 7, 2012: COALESCER BAG. ODOR. PACK ODOR LIKE DIRTY SOCK. R & R NR 2 AND NR 3 COALESCER BAGS IAW MM 21-54-03-2, RAN PACKS FOR 20 MIN AT FULL HOT, FOUND NO FOUL ODOR IN ACFT AT THIS TIME, OK T
- [SDR FDEA201206072129](https://openairdocs.org/sdr/FDEA201206072129), Jun 7, 2012: UNKNOWN. ODOR. PACK ONE HAS STRONG ODOR. NR 1 COALESCER ALREADY REPLACED, RAN PACKS, NO ODOR AT THIS TIME IAW M/M 21-54-03-2.
- [SDR FDEA201110254643](https://openairdocs.org/sdr/FDEA201110254643), Oct 25, 2011: SPAR CAP. CRACKED. RT WING REAR SPAR LOWER CAP EO 8-5710-7-5007, PT 2 INSP FOUND CRACK AT FWD, OTBD HOLE COMPLIED WITH EA 8-5710-156726 FOR RT WING REAR SPAR LOWER CAP REPAIR OF F
- [SDR FDEA201110254641](https://openairdocs.org/sdr/FDEA201110254641), Oct 25, 2011: DOOR FRAME. CORRODED. AFT CARGO COMPARTMENT DOOR SILL HAS CORROSION AT NUTPLATE HOLES AS MARKED. REMOVED CORROSION AT 12 EA HOLES IAW SRM 51-21-01, 12 EA AREAS ARE WITHIN LIMITS IAW 
- [SDR FDEA201110214618](https://openairdocs.org/sdr/FDEA201110214618), Oct 21, 2011: SKIN. CRACKED. AFT FUSELAGE OUTER SKIN IS CRACKED APPROX. 3" AT BS 2132 BETWEEN L4R AND L5R. REMOVED DAMAGE IAW SRM 53-00-01, NDT HFEC CHECKED GOOD IAW NTSPM 06-10-01, FABRICA
- [SDR FDEA201110214614](https://openairdocs.org/sdr/FDEA201110214614), Oct 21, 2011: SKIN. CRACKED. RT WING OTBD FLAP UPPER SURFACE 21" FROM THE OTBD EDGE HAS 3EA CRACKS AROUND FASTENER HOLES. REPAIRED RT WING OTBD FLAP UPPER SURFACE CRACKS AT 21" FROM OTBD ED
- [SDR FDEA201110214613](https://openairdocs.org/sdr/FDEA201110214613), Oct 21, 2011: SKIN. CRACKED. RT WING OTBD FLAP UPPER SURFACE STA XORS 587 HAS 2 EA CRACKS AROUND FASTENER HOLES. REPAIRED RT WING OTBD FLAP UPPER SURFACE AT STA XORS 587 IAW SRM 57-10-00 VO
- [SDR FDEA201110174551](https://openairdocs.org/sdr/FDEA201110174551), Oct 17, 2011: DOUBLER. WORN. AFT FUSELAGE ACCESS DOOR 311AB CUTOUT DOUBLER WORN AND RT SIDE IS ALMOST KNIFE EDGE. REPAIRED IAW EA8-5310-150998
- [SDR FDEA201110164540](https://openairdocs.org/sdr/FDEA201110164540), Oct 16, 2011: CARGO TRACK. CORRODED. AFT CARGO COMPARTMENT SEAT TRACK, RBL 25 BETWEEN FS 1940 TO FS 1964, GOUGED AND CORRODED. R & R AFT CARGO COMPARTMENT SEAT TRACK AT IAW SRM 51-31-01, MAJOR REPA
- [SDR FDEA201110164539](https://openairdocs.org/sdr/FDEA201110164539), Oct 16, 2011: CARGO TRACK. CORRODED. AFT CARGO COMPARTMENT SEAT TRACK AT RBL 25 BETWEEN FS 1800 TO 1920, HAS GOUGED AND CORRODED. R & R AFT CARGO COMPARTMENT SEAT TRACK IAW SRM 51-31-01, MAJOR REPA
- [SDR FDEA201110154528](https://openairdocs.org/sdr/FDEA201110154528), Oct 15, 2011: CARGO TRACK. GOUGED. AFT CARGO BAY CARGO TRACK, LBL 25 BETWEEN BS 1920-1964 GOUGED AND CORRODED. REMOVED, AND FABRICATED, REPAIR SPLICES AND PLATES AND REPLACED CARGO TRACK IAW SRM 
- [SDR FDEA201110154530](https://openairdocs.org/sdr/FDEA201110154530), Oct 15, 2011: FLOORBEAM. CORRODED. AFT CARGO COMPARTMENT FLOORBEAM BS 1902 IS CORRODED FROM RBL15 TO LBL15. REMOVED DAMAGE IAWSRM 53-00-01 FIG.8 AND SRM 51-31-01. FABRICATED REPAIR ANGLE AND FILL
- [SDR FDEA201110144503](https://openairdocs.org/sdr/FDEA201110144503), Oct 14, 2011: SKIN. PUNCTURED. LEFT WING, INBD FLAP, LOWER OTBD SKIN PUNCTURED. TRIMMED OUT DAMAGE IAW 57-00-01, HFEC IAW NTSPM 06-10-01. NO CRACKS NOTED. FABRICATED SKIN DOUBLER, TEE DOUBLER
- [SDR FDEA201110124454](https://openairdocs.org/sdr/FDEA201110124454), Oct 12, 2011: PULLEY. WORN. L1 DOOR FWD DRIVE TRACK, UPPER FORWARD PULLEY WORN. FURTHER INSPECTION FOUND PULLEY TO BE SPLIT. MINOR REPAIR R & R L1 DOOR UPPER FWD DRIVE PULLEY IAW SRM 51-31
- [SDR FDEA201110114424](https://openairdocs.org/sdr/FDEA201110114424), Oct 11, 2011: SHEAR TIE. CRACKED. MCD CABIN RT SIDEWALL AT STA 1800 AT L-18 SHEAR TIE CRACKED. REMOVED AND REPLACED DAMAGED SECTION OF SHEAR TIE IAW SRM 53-30-00 FIG 10, SRM 51-31-01 AND SRM 51-
- [SDR FDEA201110104409](https://openairdocs.org/sdr/FDEA201110104409), Oct 10, 2011: SEAT TRACK. DAMAGED. SEAT TRACK AT RBL 45.5 BETWEEN FS 1821 AND FS 1841 UPPER LOBE HAS ELONGATED HOLE. REPLACEMENT ACCOMPLISHED ON NON-ROUTINE N00471 AND IS CLASSIFIED AS MAJOR REPA
- [SDR FDEA201110104408](https://openairdocs.org/sdr/FDEA201110104408), Oct 10, 2011: SEAT TRACK. DAMAGED. SEAT TRACK AT RBL 45.5 BETWEEN FS 1801 AND FS 1821 UPPER LOBE HAS ELONGATED HOLES. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 53-70-00 FIG 1. FABRICATED SEAT TR
- [SDR FDEA201110044289](https://openairdocs.org/sdr/FDEA201110044289), Oct 4, 2011: SEAT TRACK. DAMAGED. SEAT TRACK AT LBL45.5 BETWEEN FS 1621 AND 1641 UPPER LOBE HAS ELONGATED HOLE. REMOVED DAMAGED SEAT TRACK SECTION , FABRICATED TRACK, REPAIR SPLICES AND PLATES I
- [SDR FDEA201110044288](https://openairdocs.org/sdr/FDEA201110044288), Oct 4, 2011: SEAT TRACK. GOUGED. SEAT TRACK AT LBL 45.5 BETWEEN FS 1721 AND FS1741 LOBE IS GOUGED. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED TRACK , REPAIR SPLICES AND PLATES IAW SRM 53-70
- [SDR FDEA201110044290](https://openairdocs.org/sdr/FDEA201110044290), Oct 4, 2011: SEAT TRACK. GOUGED. SEAT TRACK AT LBL 45.5 BETWEEN FS 1621 AND FS 1641 UPPER SURFACE IS GOUGED. REMOVED DAMAGED SEAT TRACK SECTION IAW SRM 53-70-00 FIG.1 FABRICATED REPAIR SLICES A
- [SDR FDEA201110044291](https://openairdocs.org/sdr/FDEA201110044291), Oct 4, 2011: SEAT TRACK. DAMAGED. SEAT TRACK AT LBL 45.5, FS 1721-1741 UPPER LOBE HAS ELONGATED HOLES. REMOVED DAMAGED SEAT TRACK SECTION, FABRICATED REPAIR SLICES AND PLATES AND INSTALLED IAW S
- [SDR FDEA201102260785](https://openairdocs.org/sdr/FDEA201102260785), Feb 26, 2011: OXYGEN MASK. LEAKING. AFTER O2 MASK WERE USED IN FLIGHT ALL 3 O2 BOTTLES DROPPED TO 0 PSI. SERVICED ALL 3, CREW O2 BOTTLES PER AMM 12-14-35. CHECKED ALL BOTTLES AND MASK SYSTEMS FOR 
- [SDR FDEA201010284183](https://openairdocs.org/sdr/FDEA201010284183), Oct 28, 2010: BUNGEE CYLINDER. DAMAGED. AFTER T/O, LT MAIN REMAINED UNSAFE FOLLOWED QRH CYCLED NO CHANGE. GEAR APPEARED TO BE DOWN ENTIRE TIME. UNEVENTFUL LANDING. REMOVED & REPLACED L/H MLG BUNGEE CY
- [SDR 07FDEA05029](https://openairdocs.org/sdr/07FDEA05029), Dec 11, 2007: SEAT TRACK. DAMAGED. MAIN CABIN, BS 1240, LBL 48, SEAT TRACK SCALLOP CHIPPED AND WORN RE-EVALUATED TRACK. TRACK HAS CHIPPED/BROKEN AREAS. OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 V
- [SDR 07FDEA05016](https://openairdocs.org/sdr/07FDEA05016), Dec 7, 2007: DOOR FRAME. CORRODED. MAIN CARGO DOOR JAMB TOP SURFACE UNDER NR 5 SPOOL FITTING HAS EXFOLIATION, STA 712. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IN REF TO MD/DC10-10 SRM 53-
- [SDR 07FDEA05015](https://openairdocs.org/sdr/07FDEA05015), Dec 7, 2007: DOOR FRAME. CORRODED. MAIN CARGO DOOR LOWER JAMB TOP SURFACE MOST AFT PART OF JAMB AT STA 766 HAS SURFACE CORROSION. REMOVED CORROSION AND FOUND TO BE OUT OF LIMITS IN REF TO MD/DC10
- [SDR 07FDEA04989](https://openairdocs.org/sdr/07FDEA04989), Dec 3, 2007: SEAT TRACK. DAMAGED. MAIN CABIN APPROX AT STA 1256 AND STA 1264 SEAT TRACK SCALLOPS (3EA) ELONGATED (N7513) AT LBL 48 EVALUATED SEAT TRACK FOUND TO BE OUT OF LIMITS IAW DC/MD10 SRM 
- [SDR 07FDEA04988](https://openairdocs.org/sdr/07FDEA04988), Dec 3, 2007: SEAT TRACK. DAMAGED. CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 1139 LBL 48 EVALUATED SEAT TRACK, FOUND BROKEN SCALLOP, OUT OF LIMITS IAW DC/MD10 SRM 53-70-00 VOL I PG 21 AND 22. R
- [SDR 07FDEA04987](https://openairdocs.org/sdr/07FDEA04987), Dec 3, 2007: SEAT TRACK. CORRODED. MAIN CABIN APPROX AT STA 1531 LBL 27 SEAT TRACK HAS CORROSION. REMOVED AND REPLACED SEAT TRACK AT STA 1490 TO 1531 LBL 27 IAW DC-10/MD-10 SRM 53-70-00, VOL I, F
- [SDR 07FDEA04931](https://openairdocs.org/sdr/07FDEA04931), Nov 26, 2007: SEAT TRACK. DAMAGED. MAIN CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 792 LBL 49. CHECK LIMITS AND IS OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. REMOVED SEAT TRACK IAW D
- [SDR 07FDEA04930](https://openairdocs.org/sdr/07FDEA04930), Nov 26, 2007: SEAT TRACK. DAMAGED. CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 1059 LBL 48. FOUND TO BE OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 PGS 21 & 22 VOL I REMOVED TRACK IAW DC/MD10-10 SR
- [SDR 07FDEA04929](https://openairdocs.org/sdr/07FDEA04929), Nov 26, 2007: SEAT TRACK. GOUGED. CABIN FLOOR TRACK GOUGED AT STA 1119 RBL 48 2 EACH SCALLOPS.
- [SDR 07FDEA04928](https://openairdocs.org/sdr/07FDEA04928), Nov 26, 2007: SEAT TRACK. GOUGED. CABIN FLOOR TRACK GOUGED AT STA 1119 RBL 48 2 EACH SCALLOPS. BLENDED AREA .500 MAX LIMIT GAP .510 REMAIN. OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21 
- [SDR 07FDEA04927](https://openairdocs.org/sdr/07FDEA04927), Nov 26, 2007: SEAT TRACK. WORN. FOUND MAIN CABIN AT STA 1441 RBL 48 SEAT TRACK WORN. BLENDED SEAT TRACK, WIDTH OF SCALOP HAS .200 REMAINING MIN IS .260 OUT OF LIMITS IAW DC 10 SRM 53-70-00 VOL
- [SDR 07FDEA04926](https://openairdocs.org/sdr/07FDEA04926), Nov 26, 2007: SEAT TRACK. DAMAGED. FOUND MAIN CABIN, BS 1085, RBL 28, SEAT TRACK SCALLOP CHIPPED. BLENDED AREA; CHECKED LIMITS. GAP BETWEEN SCALLOPS IS.520 MAX ALLOWED IS .500 OUT OF LIMITS IAW D
- [SDR 07FDEA04925](https://openairdocs.org/sdr/07FDEA04925), Nov 26, 2007: ANGLE. CHAFED. NR 1 PYLON THRUST LINK RUBBING AGAINST WING O/B THRUST ANGLE, STA YN348 CENTERED THRUST LINK, CLEANED AREA AROUND ATTACHMENT PIN & BUSHING, INSPECTED AREA OF BE
- [SDR 07FDEA04924](https://openairdocs.org/sdr/07FDEA04924), Nov 26, 2007: SEAT TRACK. DAMAGED. MAIN CABIN FLOOR TRACK SCALLOP BROKEN OUT AT STA 814 LBL 29. CHECKED LIMITS ON SEAT TRACK SCALLOPS. SCALLOPS TO SCALLOPS IS .510 OUT OF LIMITS IAW DC/MD10-10 SR
- [SDR 07FDEA04909](https://openairdocs.org/sdr/07FDEA04909), Nov 23, 2007: DOOR FRAME. CORRODED. MAIN CARGO DOOR LOWER JAMB AT NR 7 SPOOL LOCATION, ALL FOUR HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,D TO .517 AND HOLE D TO .484 TO REMOV
- [SDR 07FDEA04908](https://openairdocs.org/sdr/07FDEA04908), Nov 23, 2007: DOOR FRAME. CORRODED. MAIN CARGO DOOR LOWER JAMB AT NR 6 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C TO 0517 AND HOLE D TO .484 TO REMOVE C
- [SDR 07FDEA04907](https://openairdocs.org/sdr/07FDEA04907), Nov 23, 2007: DOOR FRAME. CORRODED. MAIN CARGO DOOR LOWER JAMB AT NR 5 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,D TO .517 AND HOLE D TO .484 TO REMOVE C
- [SDR 07FDEA04906](https://openairdocs.org/sdr/07FDEA04906), Nov 23, 2007: DOOR FRAME. CORRODED. MAIN CARGO DOOR LOWER JAMB AT NR 4 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C TO .460 TO REMOVE CORROSION. WITHIN LI
- [SDR 07FDEA04905](https://openairdocs.org/sdr/07FDEA04905), Nov 23, 2007: DOOR FRAME. CORRODED. MAIN CARGO DOOR LOWER JAMB AT NR 2 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C,D TO REMOVE CORROSION AND INSTALLED RE
- [SDR 07FDEA04904](https://openairdocs.org/sdr/07FDEA04904), Nov 23, 2007: DOOR FRAME. CORRODED. MAIN CARGO DOOR LOWER JAMB AT NR 1 SPOOL LOCATION, ALL 4 HOLES (A, B, C, D) HAD EVIDENCE OF CORROSION. REAMED HOLES A,B,C,D TO REMOVE COROSION AND INSTALLED REP
- [SDR 07FDEA04903](https://openairdocs.org/sdr/07FDEA04903), Nov 23, 2007: BEAM. CORRODED. MAIN CARGO DOOR JAMB TOP SURFACE UNDER CENTERING GUIDE HAS SURFACE CORROSION, STA 660. REMOVED AND REPLACED BEAMS ACA7225-1 AND ACA7226-1 IN REF TO DAC DRAWING 
- [SDR 07FDEA04799](https://openairdocs.org/sdr/07FDEA04799), Nov 15, 2007: SKIN. CRACKED. RT HORIZONTAL STAB UPPER REAR SKIN PANEL HAS APPROXIMATELY A I/2 INCH LONG CRACK INDICATION. REPAIRED RIGHT HAND HORIZONTAL STAB SKIN PANEL IN REFERENCE TO EA 8
- [SDR 07FDEA02092](https://openairdocs.org/sdr/07FDEA02092), Jun 7, 2007: DOOR FRAME. CORRODED. EXFOLIATION CORROSION LOCATED AT LOWER AFT CARGO DOOR CUTOUT, FWD LOWER CORNER. CORROSION EXCEEDED SRM LIMITS AFTER REMOVAL, REQUIRED EA TO FLY UNTIL NEXT C CHE
- [SDR 06FDEA03090](https://openairdocs.org/sdr/06FDEA03090), Aug 26, 2006: LOOP. FAULTY. CLIMBOUT FROM MEMPHIS GOT A LEVEL 3 AIR MAN NR 2 FAILED WARNING WENT AWAY AFTER THROTTLE WAS AT IDLE FOR A COUPLE OF MINUTES, DUMPED 6000 LBS FUEL FOR LANDING. 

All 186: https://openairdocs.org/deregistered/N68054-2024-02-03/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ANC78IA036](https://openairdocs.org/ntsb/ANC78IA036), May 9, 1978: Douglas DC-10 (N68054), Anchorage, AK, incident, minor damage

## 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 19780509032769I](https://openairdocs.org/incident/19780509032769I), May 9, 1978: Doug DC10/ (N68054), Anchorage, AK, Minor damage. Aircraft taxiing to gate truck improperly adjusted jetway.

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