# N68056: 1975 Mcdonnell Douglas MD-10-10F, registration cancelled 2009-09-30

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: September 30, 2009
- Status when cancelled: Triennial form not returned
- 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: 47810
- Year built: 1975
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 8, 2006
- Certificate issued: November 10, 1986
- Last registry action: July 21, 2009
- Mode S code: A9065D
- 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/N68056
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=68056
- Page: https://openairdocs.org/deregistered/N68056-2009-09-30

From the FAA registry file of November 4, 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 (150, newest 50)

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

- [SDR 07FDEA02519](https://openairdocs.org/sdr/07FDEA02519), Jul 18, 2007: STIFFENER. CRACKED. NR 1 PYLON HAS 6" CRACK VERTICAL STRUCTURE SUPPORT ON OUTBOARD BULKHEAD. VIEWED THROUGH ACCESS PANEL AUB7025-3 APPROXIMATE 4 FEET FWD PYLON STATION YN=358. [08-
- [SDR 06FDEA1550](https://openairdocs.org/sdr/06FDEA1550), Apr 20, 2006: PANEL. CRACKED. DURING NDT INSPECTION, FOUND 4 PANEL CRACKED, HORIZ STAB ZONE. REPLACED PANELS ON CENTER BOX STABILIZER AND LT STABILIZER IAW EA #8-5510-93812. FABRICATED PARTS
- [SDR 06FDEA1022](https://openairdocs.org/sdr/06FDEA1022), Mar 13, 2006: DOOR FRAME. DAMAGED. MAIN CABIN FOUND NR 1EA CRACK ON WEB JAMB DOOR NR 3 AFT AT STA 1305 LONG 15 RT SIDE. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1, FAB PART IAW DETAIL
- [SDR 06FDEA1020](https://openairdocs.org/sdr/06FDEA1020), Mar 13, 2006: SKIN. CRACKED. LEFT WING UPPER SURFACE T/E FOUND 1EA CRACK ON HONEYCOMB PANEL AT XORS 299. REPAIRED PANEL IAW SRM 57-00-01 FIG 1 SHT 1 VOL 1 AND SRM 51-70-00 PARA 16 VOL 2, FA
- [SDR 06FDEA0983](https://openairdocs.org/sdr/06FDEA0983), Mar 8, 2006: REPAIR. DAMAGED. FOUND EXTERNAL DOUBLER REPAIR AT RIGHT AIR CONDITIONING COMPT DOOR AT APPROX STA 515. INSTALLED REPAIR FILLERS, REPAIR STRAP, AND REPAIR ANGLE, AND REPAIR DOUBL
- [SDR 06FDEA0944](https://openairdocs.org/sdr/06FDEA0944), Mar 6, 2006: REPAIR. UNKNOWN. LEFT WING O/B FLAP T/E AREA FOUND AN EXTERNAL DOUBLER REPAIR BETWEEN WING STA XOF 563 AND XOF 575. REMOVED T/E IAW SRM 51-35-01 PAGE 1-13 VOL 2 AND DWG ARC1653,
- [SDR 06FDEA0943](https://openairdocs.org/sdr/06FDEA0943), Mar 6, 2006: SKIN. CRACKED. LWR FUSELAGE EXT STRUCTURE FOUND 1EA CRACK 0.25 INCH LONG ON SKIN AT STA 595 BETWEEN LONG NR 48 LEFT AND LONG NR 47 LEFT NEAR CORNER OF EXHAUST. REMOVED RAM AIR
- [SDR 06FDEA0942](https://openairdocs.org/sdr/06FDEA0942), Mar 6, 2006: SKIN. CRACKED. LEFT WING O/B FLAP UPPER SKIN SURFACE STA XOF 575 FOUND CRACK 2 INCHES LONG BETWEEN INTERCOSTAL PLANE NR 1 AND NR 2. REMOVED AND REINSTALLED SECTION T/E IAW SRM
- [SDR 06FDEA0895](https://openairdocs.org/sdr/06FDEA0895), Mar 2, 2006: BOLT. MISINSTALLED. DISCREPANCY FUSELAGE STA 275 FWD PRESSURE BULKHEAD DURING VISUAL INSP IAW EA NR 8-5310-79443B P2 FOUND INSTALLED BOLT INSTEAD OF LOCK FASTENERS. REMOVED MECH AS
- [SDR 06FDEA0903](https://openairdocs.org/sdr/06FDEA0903), Mar 2, 2006: WEB. CRACKED. UPPER CARGO AREA STA 1256 L15 LEFT SIDE FOUND WEB CRACK ON THE RADIUS ON L3 JAMB DOOR .5 INCH LONG. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1. FABR
- [SDR 06FDEA0904](https://openairdocs.org/sdr/06FDEA0904), Mar 2, 2006: STRUCTURE. CRACKED. CTR CARGO COMPT CRACK 5 INCHES LONG ON FWD DOOR JAMB. REMOVED CRACKED SECTION IAW SRM 51-35-01 PG 1/13 VOL 2 AND SRM 51-33-01 PG 34/47 VOL 2. FABRICATED AND INS
- [SDR 06FDEA0905](https://openairdocs.org/sdr/06FDEA0905), Mar 2, 2006: BULKHEAD. CRACKED. CLG WHEEL WELL SPACE FOUND 4EA CRACKS FROM .5" INCH TO 2 INCHES LONG ON UPPER SIDE LEFT VERTICAL BULKHEAD FROM STA 1491 TO 1501 LEFT SIDE X 31. INSTALLED CABLE,
- [SDR 06FDEA0906](https://openairdocs.org/sdr/06FDEA0906), Mar 2, 2006: SKIN. CRACKED. RIGHT WING O/B FLAP T/E FROM STA XOF 458 TO XOF 467 FOUND 1EA CRACK 2 INCHES LONG ON UPPER SURFACE SKIN, 1EA CRACK ON INT CHANNEL REF SRM 57-52-01 PG 52, MANY R
- [SDR 06FDEA0820](https://openairdocs.org/sdr/06FDEA0820), Feb 24, 2006: INTERCOSTAL. CRACKED. ON DOOR NR 3 RT FOUND 1EA CRACK 0.50 INCH LONG ON INTERCOSTAL SPLICE AT STA 1256 BETWEEN DOOR BEAM NR 5 AND NR 6 (REMOVED PART). BLENDED OUT DAMAGE AREA IAW SRM
- [SDR 06FDEA0819](https://openairdocs.org/sdr/06FDEA0819), Feb 24, 2006: INTERCOSTAL. CRACKED. ON DOOR NR 3 RT FOUND NR 1EA CRACK 0.50 INCH LONG ON INTERCOSTAL SPLICE AT STA 1305 BETWEEN DOOR BEAM NR 5 AND NR 6 (REMOVED PART). BLENDED OUT DAMAGE PART IAW 
- [SDR 06FDEA0683](https://openairdocs.org/sdr/06FDEA0683), Feb 14, 2006: SKIN. DENTED. RT ELEVATORS FOUND DEEP DENT ON SKIN AT STA XE 136 UPPER SURFACE. TRIMMED OUT DAMAGED SKIN AND INSTALLED REPAIR DOUBLER IAW SRM 55-10-00 FIG 8 VOL 1. FABRICATED
- [SDR 06FDEA0682](https://openairdocs.org/sdr/06FDEA0682), Feb 14, 2006: BULKHEAD. CRACKED. AFT BODY BLKHD EXT STRUCTURE FOUND 1 CRACK 0.50" LONG ON HORIZONTAL LONGERON AT STA 2163.685 X37 LT SIDE. REPAIRED CRACKED STIFFENER IAW SRM 53-40-00 FIG 7 VOL 
- [SDR 06FDEA0627](https://openairdocs.org/sdr/06FDEA0627), Feb 9, 2006: CHANNEL. BROKEN. LT WING L/E AT PYLON INTERSECTION ZONE 517 STA XDLE 315 FOUND CHANNEL BROKEN 1"1/2 LONG AND NUTPLATE MISSING ON THE AFT SECTION REF SRM 57-21-01 PAGE 18 ITEM 2.
- [SDR 06FDEA0626](https://openairdocs.org/sdr/06FDEA0626), Feb 9, 2006: RIB. CRACKED. FUEL TANK NR 1 STA XORS 372 BELOW STR 12 UPPER RIB CHORD FOUND CRACKED. REPAIRED CRACK IAW SRM 57-20-00 FIG 38 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER N
- [SDR 06FDEA0545](https://openairdocs.org/sdr/06FDEA0545), Feb 6, 2006: SKIN. CRACKED. RT WING OUTBOARD FLAP CRACK 1,5" LONG AND NR 20 FASTENERS U/S ON UPPER SKIN AT STA XOF 542. TRIMMED OUT CRACK AND REPAIRED IAW SRM 57-10-00 FIG 85 VOL 1. FABRIC
- [SDR 06FDEA0544](https://openairdocs.org/sdr/06FDEA0544), Feb 6, 2006: HINGE. CRACKED. FOUND LT WING L/E XOS 792 FOUND ACCESS PANEL TEE/HINGE CRACK 1" LONG AND EXT SKIN LOWER SECTION CRACK 2" LONG. REPAIRED L/E SKIN IAW SRM 57-10-00 FIG 68 VOL 1 A
- [SDR 06FDEA0543](https://openairdocs.org/sdr/06FDEA0543), Feb 6, 2006: SKIN. DAMAGED. RIGHT WING LOWER SURFACE OUTBOARD FLAP FOUND REPAIR AT TRAILING EDGE SECTION AT APPROX STA XOS 470. SCRAPED DOUBLER OF EXISTING EA REMOVED DAMAGED SECTION OF SK
- [SDR 06FDEA0542](https://openairdocs.org/sdr/06FDEA0542), Feb 6, 2006: REPAIR. UNKNOWN. RIGHT SIDE BELOW AND FWD OG R-2 DOOR FOUND EXT DOUBLER REPAIR BETWEEN STA 735 AND 755 AND LONGERONS 29 TO 31. REMOVED EXISTING REPAIR AND INSTALLED REPAIR IAW S
- [SDR 06FDEA0541](https://openairdocs.org/sdr/06FDEA0541), Feb 6, 2006: SKIN. CRACKED. FOUND LT WING L/E XOS 613 FOUND CRACK 1" LONG ON THE REFUEL DOOR VANE EXTERNAL SKIN. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 68 VOL 1. FABRICATED PART IAW
- [SDR 06FDEA0540](https://openairdocs.org/sdr/06FDEA0540), Feb 6, 2006: SKIN. CRACKED. RT WING L/E FOUND CRACK 2" LONG ON EXT SKIN AT STA XORS 480. REPAIRED CRACK IAW SRM 57-10-00 FIG 68 SHT 2-3 VOL 1. FABRICATED PART IAW DETAIL PART TRAVELER F163
- [SDR 06FDEA0247](https://openairdocs.org/sdr/06FDEA0247), Jan 18, 2006: TANK. CRACKED. AFT FUSELAGE WASTE TANK COMPT FOUND 1EA CRACK ON LONG 43, 3 INCHES LONG BETWEEN STA 1986 AND 1997 LT. REMOVED FRAME SPLICE AND ANGLES AND REINSTALLED PARTS IAW 
- [SDR 06FDEA0246](https://openairdocs.org/sdr/06FDEA0246), Jan 18, 2006: SKIN. CRACKED. LEFT WING EXTERNAL SKIN OF L/E SLAT TRACK NR 10 XOS 660 FOUND CRACK .5 INCH LONG ON THE SLAT TRACK HOLE ANGLE. INSTALLED EXTERNAL DOUBLER IAW SRM 57-10-00 FIG 6
- [SDR 06FDEA0154](https://openairdocs.org/sdr/06FDEA0154), Jan 12, 2006: DOOR FRAME. CRACKED. MAIN CABIN FOUND 2 EA CRACKS 1 INCH LONG AND .50 INCH LONG ON WEB JAMB DOOR 3 FWD AT STA 1256 LONG 27 RT. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 1 VOL. 
- [SDR 05FDEA04282](https://openairdocs.org/sdr/05FDEA04282), Dec 13, 2005: BULKHEAD. CRACKED. FOUND LT AIR CONDITIONING COMPT FOUND 1 CRACK 4" LONG ON SKIN OF BULKHEAD BETWEEN STA 584 AND STA 580 Z-46 BY 24. TRIMMED OUT CRACK AND INSTALLED FILLER AND 2 R
- [SDR 05FDEA04151](https://openairdocs.org/sdr/05FDEA04151), Dec 6, 2005: FRAME. CRACKED. CAC LOWER LOBE BILGE FOUND 1EA CRACK, 3 INCHES LONG ON LT FRAME AT STA 1159 CLOSE TO PRESSURE PANEL FWD CENTER WING. REMOVED ATTACH ANGLE IAW SRM 51-33-01 PAR 6
- [SDR 05FDEA04150](https://openairdocs.org/sdr/05FDEA04150), Dec 6, 2005: DOUBLER. NONE. DISCREPANCY FOUND EXTERNAL DOUBLER BETWEEN STA 735 AND 755 AND LONGERONS 34 AND 35 LT SIDE, WHERE POTABLE WATER SERVICE PANEL USED TO BE LOCATED. PERFORMED INSP
- [SDR 05FDEA03973](https://openairdocs.org/sdr/05FDEA03973), Nov 28, 2005: HINGE. CRACKED. LT WING LEADING EDGE AT STA XOS 906 FOUND ACCESS PANEL TEE/HINGE CRACK .5 INCH LONG. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 49 VOL 1. FABRICATED PARTS IA
- [SDR 05FDEA03972](https://openairdocs.org/sdr/05FDEA03972), Nov 28, 2005: FLANGE. CRACKED. CLG WHEEL WELL/SPACE: 1EA CRACK 1 INCH LONG ON DOUBLER FLANGE UPPER SIDE LT VERTICAL BULKHEAD FROM STA 1421 TO 1431 LT SIDE X 31. REMOVED DOUBLER IAW SRM 51-35-
- [SDR 05FDEA03955](https://openairdocs.org/sdr/05FDEA03955), Nov 24, 2005: REPAIR. PROPER. FWD OF FWD CARGO DOOR STA 859 BETWEEN STRINGERS 36 AND 37 ON THE RT SIDE THERE IS AN INTERNAL DOUBLER REPAIR. PERFORMED A INSPECTION OF REPAIR IAW EA#8-5330-932
- [SDR 05FDEA03954](https://openairdocs.org/sdr/05FDEA03954), Nov 24, 2005: REPAIR. UNKNOWN. FWD AVIONICS COMPT AT STA 475 FOUND FRAME REPAIR AT X 60. NO ACTION TAKEN FRAME WILL BE REMOVED WITH NRC N00579.
- [SDR 05FDEA03953](https://openairdocs.org/sdr/05FDEA03953), Nov 24, 2005: DOOR FRAME. CRACKED. MAIN CABIN FOUND 2 CRACKS 1" LONG ALL ON WEB JAMB DOOR NR 3 AFT AT STA 1305 LONG 27 RT SIDE. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 2 VOL 1. FABRICATED 
- [SDR 05FDEA03952](https://openairdocs.org/sdr/05FDEA03952), Nov 24, 2005: BULKHEAD. CRACKED. RT AIR CONDITIONING COMPT FOUND 1 CRACK 2.50" LONG ON BULKHEAD BETWEEN STA 575 AND STA 569 Z-60 X-24. REPAIRED CRACK IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1. FABRICA
- [SDR 05FDEA03836](https://openairdocs.org/sdr/05FDEA03836), Nov 16, 2005: ANGLE. CRACKED. RIGHT AIR CONDITIONING COMPT FOUND 1 CRACK 1" LONG ON TEE ANGLE AT STA 535 Z-39 X-102. REPAIRED CRACK IAW SRM 53-00-01 FIG 9 SHT 7 VOL 1.
- [SDR 05FDEA03834](https://openairdocs.org/sdr/05FDEA03834), Nov 16, 2005: BULKHEAD. CRACKED. RT AIR CONDITIONING COMPT FOUND 1 CRACK 2 INCHES LONG ON BULKHEAD BETWEEN STA 482 AND STA 489 Z-60 X-24. REPAIRED CRACK IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1, FABR
- [SDR 05FDEA03823](https://openairdocs.org/sdr/05FDEA03823), Nov 15, 2005: REPAIR. PROPER. JUST ABOVE FWD NOSE LANDING GEAR DOOR BETWEEN STA 490 AND 555 LT SIDE, FOUND FLUSH DOUBLER OF APROX 62 X 25 INCH. PERFORMED A GVI OF REPAIRS IAW CONTINENTAL AIR
- [SDR 05FDEA03822](https://openairdocs.org/sdr/05FDEA03822), Nov 15, 2005: REPAIR. PROPER. FOUND FLUSH DOUBLER REPAIR RT SIDE BETWEEN STA 490 AND 535 JUST ABOVE OF FWD NOSE LANDING GEAR ON AN AREA OF ABOUT 43'' BY 21''. PERFORMED A GVI OF REPAIRS IAW 
- [SDR 05FDEA03821](https://openairdocs.org/sdr/05FDEA03821), Nov 15, 2005: REPAIR. PROPER. FOUND EXTENSIVE DOUBLER REPAIR AROUND L-1 DOOR BETWEEN STA 401 AND 470.25 BOTTOM FWD AND AFT CORNERS ON FUSELAGE SKIN. PERFORMED A GVI OF EXISTING DOUBLER IAW F
- [SDR 05FDEA03796](https://openairdocs.org/sdr/05FDEA03796), Nov 14, 2005: DOOR FRAME. CRACKED. MAIN CABIN, FOUND 1 CRACK .25" LONG ON WEB JAMB DOOR NR 3 FWD AT STA 1256 LONG 15 RT. REPAIRED DOOR JAMB IAW SRM 53-50-00 FIG 19 SHT 1 VOL 1. FABRICATED PART IA
- [SDR 05FDEA03798](https://openairdocs.org/sdr/05FDEA03798), Nov 14, 2005: REPAIR. UNDAMAGED. BARON REPAIR, DOUBLER INSTALLED AT APPROX STA 505 RT SIDE BETWEEN LONG 39 AND 40. PERFORMED A GVI OF BARON DOUBLER IAW FEDEX EA NR 8-5320-38573B AND FEDEX EA NR
- [SDR 05FDEA03799](https://openairdocs.org/sdr/05FDEA03799), Nov 14, 2005: REPAIR. PROPER. FOUND FWD PRESSURE BULKHEAD STA 275 LT HAND SIDE FOUND REPAIR DOUBLER BETWEEN X 13, X28 AND Z-14, Z-27.7 BEAMS. PERFORMED A GVI OF DOUBLER IAW CONTINENTAL AIRLI
- [SDR 05FDEA03710](https://openairdocs.org/sdr/05FDEA03710), Nov 8, 2005: DOOR FRAME. UNKNOWN. FOUND MAIN CABIN L-3 DOOR FWD DOOR JAMB STA 1259 FOUND DOUBLER REPAIR BETWEEN STRINGER 24 AND 27. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITER
- [SDR 05FDEA03709](https://openairdocs.org/sdr/05FDEA03709), Nov 8, 2005: REPAIR. UNDAMAGED. FOUND EXTERNAL TRIPLE DOUBLER REPAIR AT STA 1139 BETWEEN LONGERON 47 AND 48 RT SIDE. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FOUND DOUB
- [SDR 05FDEA03708](https://openairdocs.org/sdr/05FDEA03708), Nov 8, 2005: SKIN. UNKNOWN. FOUND MAIN CABIN BETWEEN FUSELAGE STA 1601 AND 1621, STRINGERS 8 AND 9 RT SIDE FOUND A FLUSH REPAIR. PERFORMED A GVI OF EXISTING REPAIR IAW SRM 53-20-00 FIG 13 
- [SDR 05FDEA03707](https://openairdocs.org/sdr/05FDEA03707), Nov 8, 2005: REPAIR. UNDAMAGED. AFT AIR CONDITIONING ACCESS DOOR, AFT TOP CORNER FOUND AN EXTERNAL TRIPLE DOUBLER REPAIR AT STA 595 LT SIDE. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-
- [SDR 05FDEA03706](https://openairdocs.org/sdr/05FDEA03706), Nov 8, 2005: REPAIR. UNDAMAGED. AFT FUSELAGE ABOVE HORIZONTAL STABILIZER LT SIDE STA Y2131 FOUND AN EXTERNAL DOUBLER REPAIR. PERFORMED A GVI OF EXISTING REPAIR IAW EO 8-5100-7-5001 CRITERIA FO

All 150: https://openairdocs.org/deregistered/N68056-2009-09-30/reports.md

## NTSB investigations (2)

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 LAX90FA148](https://openairdocs.org/ntsb/LAX90FA148), Apr 18, 1990: McDonnell Douglas DC-10-10F (N68056), Los Angeles, CA, substantial damage. Probable cause: PILOT FAILED TO ADHERE TO ESTABLISHED LANDING PROCEDURES, MAINTAIN A STABILIZED APPROACH, AND ALLOWED THE AIRSPEED TO GO BELOW THE PREDICTED V.
- [NTSB DEN83FA021](https://openairdocs.org/ntsb/DEN83FA021), Nov 19, 1982: Mcdonald Douglas DC-10 (N68056), Denver, CO, substantial damage

## 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.

- [Accident 19900418010239A](https://openairdocs.org/incident/19900418010239A), Apr 18, 1990: Doug DC1010F (N68056), Los Angeles, CA, Substantial damage. Excessive pitch up on landing flare causing tail strike.
- [Incident 19801006082419I](https://openairdocs.org/incident/19801006082419I), Oct 6, 1980: Doug DC1010F (N68056), Houston, TX. Hydraulic quantity dropped to one gallon en route. Replaced isolation valve and one hydraulic pump.

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