# N68057: 1982 Mcdonnell Douglas MD-10-10F, registration cancelled 2020-04-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 23, 2020
- 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: 48264
- Year built: 1982
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 13, 2004
- Certificate issued: September 10, 1990
- Last registry action: December 27, 2017
- Mode S code: A9065E
- 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/N68057
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=68057
- Page: https://openairdocs.org/deregistered/N68057-2020-04-23

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 (73, newest 50)

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

- [SDR FDEA201503190989](https://openairdocs.org/sdr/FDEA201503190989), Mar 19, 2015: SWITCH. DIRTY. DOOR 1 LT FAILED OPEN FROM OUTSIDE & INSIDE. CYCLED SLIDE ARM LEVER & OPENED WITH DOOR SWITCH. INSPECTED & CLEANED DOOR SWITCH IAW AMM 52-10-01-6. DOOR OPERATIO
- [SDR FDEA201407191858](https://openairdocs.org/sdr/FDEA201407191858), Jul 19, 2014: SKIN. CRACKED. ON POST FLIGHT WALK AROUND FOUND FUSELAGE SKIN CRACKED AT NR 1 PACK DOOR CUT OUT UPPER AFT CORNER. INSTALLED DOUBLER, TRIPLER & FILLER IAW SRM 53-50-00 FIG 3A &
- [SDR FDEA201406141448](https://openairdocs.org/sdr/FDEA201406141448), Jun 14, 2014: SKIN. CRACKED. FOUND A CRACK ON RT WING SKIN AT NR 3 SLAT TRACK BETWEEN NR 1 & 2 SLATS. TRIMMED OUT DAMAGED AREA. PERFORMED INTERNAL & EXTERNAL VISUAL INSPECTION WITH NO ADDIT
- [SDR FDEA201406091367](https://openairdocs.org/sdr/FDEA201406091367), Jun 9, 2014: SKIN. CRACKED. FOUND TWO CRACKS ON RT WING TAI DUCT CUT OUT. VERIFIED CRACKS IAW NDT SPM PART 6. REPAIRED IAW EA 8-5710-T0308893 & SRM.
- [SDR FDEA201406091368](https://openairdocs.org/sdr/FDEA201406091368), Jun 9, 2014: SKIN. CRACKED. DURING POST FLIGHT INSPECTION, FOUND POSSIBLE LT WING LE CRACK AT REFUEL DOOR INBD CORNER CUT OUT. CONFIRMED CRACK BY HFEC INSPECTION IAW NDTSPM PT 6 CRACK TERM
- [SDR FDEA201406091366](https://openairdocs.org/sdr/FDEA201406091366), Jun 9, 2014: SKIN. CRACKED. FOUND TWO CRACKS IN LEFT WING TAI DUCT. VERIFIED CRACK IAW NDT SPM PART 6. REPAIRED IAW EA.
- [SDR FDEA201312223028](https://openairdocs.org/sdr/FDEA201312223028), Dec 22, 2013: TRANSMITTER. FAILED. AT FL 320, NOTICED NR 2 FUEL FLOW 16150 PPH, ALL OTHER INDICATIONS NORMAL. FUEL USED SHOWED NR 2 HAD USED 2200 LBS MORE THAN 1 & 3. FUEL REMAINING WAS IN AGREEM
- [SDR FDEA201305100968](https://openairdocs.org/sdr/FDEA201305100968), May 10, 2013: FITTING. CRACKED. MAIN CARGO DOOR FRAME NR 1 SPOOL LOWER FITTING CRACKED IN FOUR LOCATIONS. VERIFIED WITH HFEC IAW NDT SPM93K0393, CRACK RUNS THOUGH FITTING. R & R MAIN CARGO DOO
- [SDR FDEA201301140091](https://openairdocs.org/sdr/FDEA201301140091), Jan 14, 2013: STRUT. DAMAGED. AFTER T/O LDG GEAR HANDLE WOULD NOT RAISE. QRH C/W. HANDLE RAISED & ALL IN FLIGHT SYSTEMS OPERATED NORMALLY. R & R THE NLG ASSY, REF WC 32T2101 AND 32T2701.
- [SDR FDEA201301040056](https://openairdocs.org/sdr/FDEA201301040056), Jan 4, 2013: INTERCOSTAL. CORRODED. LEFT MLG WHEEL WELL AFT WALL LOWER SHELF HAS THE INTERCOSTAL JUST BELOW THE FLAP BUSS CABLE PULLEYS WITH A LARGE AREA BULGED. INSTALLED NEW INTERCOSTAL REF. SRM
- [SDR FDEA201212294396](https://openairdocs.org/sdr/FDEA201212294396), Dec 29, 2012: CONTROL UNIT. MALFUNCTIONED. AFTER TAKEOFF LANDING GEAR HANDLE WOULD NOT RAISE. COMPLIED WITH QRH THEN GOT LEVEL 1 ANTI-SKID NO TEST ALERT. REMAINED ON UNTIL GEAR HANDLE DOWN. ANTI-SKID ALE
- [SDR FDEA201209153328](https://openairdocs.org/sdr/FDEA201209153328), Sep 15, 2012: SCAVENGE PUMP. LEAKING. DURING CLIMB NR 1 OIL QUANTITY INDICATED '0'. ALL OTHER INDICATIONS NORMAL INITALLY. IN CRUISE NR 1 OIL PRESS DROPPED TO 14 PSI WITH AN AMBER INDICATION. CONFER
- [SDR FDEA201204241542](https://openairdocs.org/sdr/FDEA201204241542), Apr 24, 2012: POWER SUPPLY. FAILED. DURING PREFLIGHT EMERGENCY LIGHT TEST FAILED. R & R EMERGENCY LIGHTS POWER SUPPLY IAW MM 33-51-01-4, OPS CHECKS NORMAL.
- [SDR FDEA201111164931](https://openairdocs.org/sdr/FDEA201111164931), Nov 16, 2011: SENSOR. FAILED. ON TAKEOFF ROLL N2 VIA FAIL. REJECT AT 60 KTS. R & R NR 1, ENG N1 SENSOR.
- [SDR FDEA201111154928](https://openairdocs.org/sdr/FDEA201111154928), Nov 15, 2011: SENSOR. FAILED. NR 3 ENGINE N1 GAUGE FAILED ON DEPARTURE ROLL ALONG WITH AUTOTHROTTLE OFF - "VIA 1 FAIL" AND "VIA 2 FAIL" LEVEL 1 ALERTS. VIA 1 FAULT HISTORY SHOWED NR 3 ENGINE
- [SDR FDEA201110124425](https://openairdocs.org/sdr/FDEA201110124425), Oct 12, 2011: WINDSHIELD. FAILED. CAPT'S WINDSHIELD ARCING & SHATTERED. SHORTED IN WINDOW AT 18000 FT. REPLACED THE CAPT'S WINDSHIELD REF MM 56-11-00-2.
- [SDR FDEA201107192814](https://openairdocs.org/sdr/FDEA201107192814), Jul 19, 2011: FLOORBEAM. CRACKED. FLOORBEAM TEE CRACKED THROUGH ALL SIDES AT STA 1156 L29R. REPAIRED CRACKED FLOORBEAM REF SRM 53-30-00 FIG 7. COMPLIED WITH EA 8-5310-147795.
- [SDR FDEA201012024537](https://openairdocs.org/sdr/FDEA201012024537), Dec 2, 2010: LAMP. INOPERATIVE. R1 DOOR PRESSURE, PRESS TO TEST INDICATOR INOP. FOUND P/N 387 HIGH VOLTAGE LAMPS IN DOOR SLIDE PUSH BUTTON SWT. INSTALED P/N 368 LAMPS PER IPC. GRD OPS CHECKS O
- [SDR FDEA200911093915](https://openairdocs.org/sdr/FDEA200911093915), Nov 9, 2009: ACTUATOR. DAMAGED. DURING WALK AROUND, FOUND LT OTBD FLAP INBD ACT BROKEN. INSPECTED FLAP FOR ANY PULLED RIVETS AND NONE FOUND. INSPECTED OTBD FLAP ACT"S ATTACKING POINTS TO MAKE 
- [SDR FDEA200906102018](https://openairdocs.org/sdr/FDEA200906102018), Jun 10, 2009: SMOKE DETECTOR. MALFUNCTIONED. DECENDING THRU 14,000` RECEIVED "CARGO FIRE ALERT" COMPLIED WITH QRH AND DISCHARGED BOTH FIRE BOTTLES. NEVER HAD ANY SECONDARY INDICATIONS OF FIRE. REMOVED AND 
- [SDR FDEA200807012617](https://openairdocs.org/sdr/FDEA200807012617), Jul 1, 2008: SEAL. WORN. LOUD NOISE THAT APPEARED TO COME FROM THE CAPT'S SLIDING WINDOW AREA. A VIBRATION COULD BE FELT ON THE POST IN THE WINDOW ARM. BUT COMMUNICATION WAS NEARLY IMPO
- [SDR 08FDEA02617](https://openairdocs.org/sdr/08FDEA02617), Jul 1, 2008: WINDOW FRAME. DAMAGED. LOUD NOISE THAT APPEARED TO COME FROM THE CAPT'S SLIDING WINDOW AREA. A VIBRATION COULD BE FELT ON THE POST IN THE WINDOW ARM. BUT COMMUNICATION WAS NEARLY IMPO
- [SDR 07FDEA03587](https://openairdocs.org/sdr/07FDEA03587), Sep 11, 2007: SKIN. DAMAGED. FUSELAGE SKIN AND FRAME AT STA 642 HAVE OVERSIZED FASTENER HOLE. REPAIRED IAW EA 8-53-109196-FUSELAGE-EXISTING BUSHINGS FOUND AT STA 641.5 MCD, LOWER SILL-REPAI
- [SDR 07FDEA03403](https://openairdocs.org/sdr/07FDEA03403), Sep 6, 2007: FLOORBEAM. CORRODED. AFT CABIN BULKHEAD FLOOR TEE ANGLE SUPPORT CORRODED UNDER FLOOR PANEL SUPPORT AT RBL 20 REMOVED CORROSION IAW MD10 SRM 53-40-00 VOL1 FIG 18. ORIGINAL THICKNESS 
- [SDR 07FDEA03234](https://openairdocs.org/sdr/07FDEA03234), Aug 29, 2007: SEAT TRACK. CORRODED. MAIN CABIN SEAT TRACK HAS CORROSION AT STA.720 AT LBL 107. REMOVED, FABRICATED AND INSTALLED SPLICED PLATE, SPLICE HAT AND SEAT TRACK IAW MD/DC10 SRM 53-70-00 V
- [SDR 07FDEA03006](https://openairdocs.org/sdr/07FDEA03006), Aug 21, 2007: STRINGER. CORRODED. CENTER W/WELL AREA L48L END FITTING CORRODED IN AREAS STA 1509 TO 1521. REMOVED, FABRICATED AND INSTALLED FITTING P/N AYB7020-1 STA 1509-1521 L48L IAW DC/MD10 S
- [SDR 07FDEA02982](https://openairdocs.org/sdr/07FDEA02982), Aug 20, 2007: SEAT TRACK. CRACKED. CABIN SEAT TRACK FLANGE IS CRACKED AT STA 449 LBL 28.5 REMOVED SEAT TRACK AT STA 449 LBL 28.5 IAW DC-10 SRM 51-31-01 VOL 2 PG 1-10. FABRICATED IAW DC-10 SRM 53-
- [SDR 07FDEA02980](https://openairdocs.org/sdr/07FDEA02980), Aug 20, 2007: SEAT TRACK. GOUGED. GOUGED CABIN SEAT TRACK SCALLOPS AT STA 879 TO 899 LBL 85 REMOVED AND REPLACED SEAT TRACK IAW DC-10 SRM 53-70-00 VOL 1 PG 51. FABRICATED SPLICE PLATES AND SPLIC
- [SDR 07FDEA02879](https://openairdocs.org/sdr/07FDEA02879), Aug 14, 2007: SPAR. CRACKED. RT HORIZONTAL STAB REAR SPAR CAP CRACKED ON AFT SIDE NEAR RT UPPER AFT BARREL NUT AT STA XE 48.500 CRACK EXTENDS APPROX 3.0", HORIZONTALLY FROM INBD END OF FITT
- [SDR 07FDEA02877](https://openairdocs.org/sdr/07FDEA02877), Aug 14, 2007: DOOR FRAME. CORRODED. FOUND MAIN CARGO LOWER DOOR JAMB HAS CORROSION ON LOWER BEAM AT STA 750. 09-04-07 REMOVED AND REPLACED MAIN CARGO DOOR JAMB LOWER DOOR JAMB LOWER BEAM IN REF TO
- [SDR 07FDEA02864](https://openairdocs.org/sdr/07FDEA02864), Aug 13, 2007: SEAT TRACK. GOUGED. GOUGED/SCUFFED SCALLOPS ON CABIN SEAT TRACK AT STA 1199, TO 1219, RBL 47.5 REMOVED SEAT TRACK SECTION AT STA 1209-1269 RBL 47 IAW DC-10/MD-10 SRM 51-31-01, VOL2
- [SDR 07FDEA02863](https://openairdocs.org/sdr/07FDEA02863), Aug 13, 2007: SEAT TRACK. GOUGED. GOUGED, CABIN SEAT TRACK AT STA 1039 TO 1059, LBL 27.5 CHECKED LIMITS, GAP BETWEEN SCALLOPS FOUND TO BE GREATER THAN .500 (MAX ALLOWED) OUT OF LIMITS IAW DC/MD-
- [SDR 07FDEA02862](https://openairdocs.org/sdr/07FDEA02862), Aug 13, 2007: SEAT TRACK. DAMAGED. ELONGATED SCALLOPS AT CABIN SEAT TRACK, STA 899 TO 919, RBL47.5. [08-29-07] CHECKED LIMITS, MAX ALLOW BETWEEN EDGE OF SCALLOP IS .500. FOUND TO BE GREATER THAN 
- [SDR 07FDEA02797](https://openairdocs.org/sdr/07FDEA02797), Aug 8, 2007: SEAT TRACK. DAMAGED. ELONGATED SCALLOPS AT CABIN SEAT TRACK LBL 47.5, STA 939 TO 1019 (2-PLACES) REMOVED SEAT TRACK AT STA 879-1019 IAW DC10-SRM 53-70-00 VOL 1 PG5. SEAT TRACK WAS O
- [SDR 07FDEA02796](https://openairdocs.org/sdr/07FDEA02796), Aug 8, 2007: SEAT TRACK. DAMAGED. BROKEN SCALLOPS ON CABIN SEAT TRACK AT STA 755 REMOVED FLOOR PANEL IAW DC10/MD10 SRM 51-31-01 VOL 2 PGS 1-5. REMOVED SEAT TRACK AT STA 700-760 LBL 47.5 IAW DC10
- [SDR 07FDEA02795](https://openairdocs.org/sdr/07FDEA02795), Aug 8, 2007: SEAT TRACK. WORN. ELONGATED SCALLOPS ON CABIN SEAT TRACK AT RBL 47.5, STA 1019 TO 1039 CHECKED LIMITS, SEAT TRACK HAS SEVERAL BROKEN SCALLOPS OUT OF LIMITS IAW DC/MD10 SRM 53-70-
- [SDR 07FDEA02794](https://openairdocs.org/sdr/07FDEA02794), Aug 8, 2007: SEAT TRACK. GOUGED. GOUGED, CABIN SEAT TRACK SCALLOPS AT STA 1159 TO STA 1099, RBL 27.5 STA 1099-1119, RBL 27.5 REMOVED GOUGE, REMAINING .434, FOUND TO BE WITHIN LIMITS IAW DC10/MD
- [SDR 07FDEA02780](https://openairdocs.org/sdr/07FDEA02780), Aug 6, 2007: STRINGER. CORRODED. CENTER WHEEL AREA L48L END FITTING CORRODED IN AREAS STA1509 TO 1521. [08-21-07] ALL WORK ACCOMPLISHED ON SDR 07-3006 -W/O 37284.
- [SDR 07FDEA02779](https://openairdocs.org/sdr/07FDEA02779), Aug 6, 2007: STRINGER. CORRODED. CENTER WHEEL WELL AREA L52 END FITTING HAS CORROSION IN AREAS STA1509 TO 1521. [08-21-07] RMEOVED, FABRICATED, INSTALLED FITTING P/N AYB7020-2 IAW DC/MD10 SRM 5
- [SDR 07FDEA02778](https://openairdocs.org/sdr/07FDEA02778), Aug 6, 2007: STRINGER. CORRODED. CENTER WHEEL WELL AREA L51R END FITTING HAS CORROSION IN AREAS STA 1509 TO 1521. [08-21-07] REMOVED, FABRICATED, AND INSTALLED FITTING P/N AYB 7020-1 STA.1509 T
- [SDR 07FDEA02728](https://openairdocs.org/sdr/07FDEA02728), Aug 2, 2007: FITTING. CRACKED. MAIN CARGO DOOR FITTING NR 3 BORES A, C AND D SHOWS CRACK INDICATION WITH BHEC BORES MARKE DIN BLACK. 09-04-07 REMOVED AND REPLACED NR 3 DOOR FITTING AT STA 666
- [SDR 07FDEA02727](https://openairdocs.org/sdr/07FDEA02727), Aug 2, 2007: DOOR FRAME. CORRODED. MAIN CARGO DOOR CUT-OUT LOWER JAMB TOP SIDE, JUST FWD OF NR 3 LATCH SPOOL FITTING WEB CORRODED. 09-04-07 REMOVED AND REPLACED MAIN CARGO DOOR JAMB UPPER BEAM AC
- [SDR 07FDEA02726](https://openairdocs.org/sdr/07FDEA02726), Aug 2, 2007: FITTING. CRACKED. MAIN CARGO DOOR FITTING NR 7 BORES A, B, C AND D SHOW CRACK INDICATIONS WITH BHEC BORES MARKED IN BLACK. 09-04-07 REMOVED AND REPLACED FITTING NR 7 IN REF TO DC
- [SDR 07FDEA01117](https://openairdocs.org/sdr/07FDEA01117), Mar 23, 2007: BOLT. CORRODED. LT MAIN LANDING GEAR SUPPORT FITTING-FWD TRUNNION BOLT DOES NOT TAKE GREASE AND IS FROZEN. UPON REMOVAL, FOUND BOLT CORRODED. REPAIRED BOLT PER SEQ NR 13 EA 8-5
- [SDR 06FDEA04310](https://openairdocs.org/sdr/06FDEA04310), Dec 22, 2006: ENGINE. MAKING METAL. SHUT DOWN NR 3 ENGINE IN FLIGHT BECAUSE OF LEVEL 2 ALERT, ENG NR 3 OIL FILTER. BEFORE SHUT DOWN OIL PRESS WAS NORMAL. OIL TEMP WAS 20 PERCENT HIGHER THAN OTHER 
- [SDR 06FDEA03439](https://openairdocs.org/sdr/06FDEA03439), Sep 26, 2006: CYLINDER. FAILED. RT MAIN GEAR DOWN ON RETRACTION AFTER T/O. LIGHT WENT RED AND STAYED RED UNTIL GEAR HANDLE PLACED DOWN. RECYCLED, SAME THING. LANDED @ KOAK. PER CREW DEBRIEF, A
- [SDR 06FDEA1616](https://openairdocs.org/sdr/06FDEA1616), Apr 25, 2006: DIMMER. FAILED. APPROACHING TOP OF DESCENT A SLIGHT ELECTRICAL ODOR WAS NOTED IN COCKPIT. UNABLE TO LOCATE SOURCE, BUT A BRIEF SQUEAL WAS HEARD NEAR COCKPIT DOOR, FOLLOWED SHOR
- [SDR 06FDEA1276](https://openairdocs.org/sdr/06FDEA1276), Mar 31, 2006: SEAL. LEAKING. 1 40 INTO FLIGHT AT FL370, WINDOW SEAL ON CAPT SIDE DEVELOPED LOUD SQUEAL. TOO LOUD TO CONTINUE FLIGHT. NOISE DISSIPATED UPON DESCENT THRU 15,000'. REMOVED AND 
- [SDR 06FDEA0953](https://openairdocs.org/sdr/06FDEA0953), Mar 6, 2006: REPAIR. NONE. REPAIR DOUBLER STATION 1059 - 1085 L51 - L52 MARKED NR 15 REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA 
- [SDR 06FDEA0924](https://openairdocs.org/sdr/06FDEA0924), Mar 2, 2006: REPAIR. UNKNOWN. REPAIR LT OB FLAP UPPER SKIN,STA.XOF 587 MARKED NR 71. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF THE REPAIR WAS ACCOMPLISHED USING FAA APP

All 73: https://openairdocs.org/deregistered/N68057-2020-04-23/reports.md

## FAA accident and incident reports (2)

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 20060925027409I](https://openairdocs.org/incident/20060925027409I), Sep 25, 2006: Doug MD1010F (N68057), Oakland, CA. (-23) Investigation revealed: rt main gear down on retraction after t/o. light went red and stayed red until gear handle placed down again. Crew recycled gear…
- [Incident 19920721033479I](https://openairdocs.org/incident/19920721033479I), Jul 21, 1992: Doug DC1010 (N68057), Los Angeles, CA. Avionics compartment exit door light on after rotation. Returned. Door was fully open and locked in place.

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