# N68050: 1974 Mcdonnell Douglas MD-10-10F, registration cancelled 2024-04-13

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: April 13, 2024
- Status when cancelled: Sale reported, canceled
- 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: 47804
- Year built: 1974
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 10, 2004
- Last registry action: July 10, 2023
- Mode S code: A90657
- Location: [Victorville, CA](https://openairdocs.org/faa-place/CA/Victorville)
- Owner type: Individual
- Owner's area on the map: 34.5670° N, 117.3629° W: Placed by OpenAirDocs at the center of ZIP code 92394, within about 3 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N68050
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=68050
- Page: https://openairdocs.org/deregistered/N68050-2024-04-13

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 (63, newest 50)

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

- [SDR FDEA201211093924](https://openairdocs.org/sdr/FDEA201211093924), Nov 9, 2012: SEAL. FAILED. SHUTDOWN APU WITH FIRE HANDLE & DISCHARGED ONE FIRE BOTTLE AFTER ACFT FILLED WITH SMOKE DURING LOADING. APU RUNNING APPROX 15-20 MINUTES. RECEIVED AN ALERT FOR 
- [SDR FDEA201209213388](https://openairdocs.org/sdr/FDEA201209213388), Sep 21, 2012: ATTACH BRACKET. FAILED. UNSAFE NOSE GEAR INDICATION UPON EXTENSION. EXTENDED GEAR WITH ALTERNATE EXTENSION HANDLE. HEARD LOUD BANG ON RT SIDE ON TAKEOFF. NOTE: UPON CREW DEBRIEF. CAPT 
- [SDR FDEA201209203366](https://openairdocs.org/sdr/FDEA201209203366), Sep 20, 2012: MOUNT. BROKEN. UNSAFE NOSE GEAR INDICATION ON EXTENSION. EXTENDED GEAR WITH ALTERNATE EXTENSION HANDLE. HEARD LOUD BANG ON RT SIDE AFTER TAKEOFF. CAPTAIN STATED THEY DID NOT F
- [SDR FDEA201206042126](https://openairdocs.org/sdr/FDEA201206042126), Jun 4, 2012: BULKHEAD WEB. CRACKED. LEFT MLG WW HAS A CRACK ON INBD BULKHEAD. REPAIRED IAW EA 8-5310-157338, PART 1, STEPS 1 THROUGH 4.
- [SDR FDEA201206042125](https://openairdocs.org/sdr/FDEA201206042125), Jun 4, 2012: BULKHEAD WEB. CRACKED. CRACK IN LT MLG WW INBD BULKHEAD, FWD UPPER SIDE PROTUDING OUT OF LIGHTNING HOLE THREE INCH CRACKS. MWT REPAIRED IAW EA 8-5310-157337, PART 1, STEPS 1- 4.
- [SDR FDEA201111184968](https://openairdocs.org/sdr/FDEA201111184968), Nov 18, 2011: COMPRESSOR. STALLED. AT ROTATION NR 1 ENG COMPRESSOR STALLED. HEARD A LOUD BANG WITH YAW AND TEMP AT 1097 DEGREES. N2 INDICATION HAD AN X WITH NO INFORMATION SHOWING. REMOVED AND RE
- [SDR FDEA201011174408](https://openairdocs.org/sdr/FDEA201011174408), Nov 17, 2010: SUPPORT. CRACKED. LEFT OTBD FLAP INBD HINGE-FWD FITTING ATTACHED TO THE WING HAS A CRACK ON INBD SIDE. REMOVED CRACKED SUPPORT FITTINGS IAW SRM 51-33-01. WORKED HOLES TO FINAL SI
- [SDR FDEA200902120514](https://openairdocs.org/sdr/FDEA200902120514), Feb 12, 2009: FUEL CONTROL. MALFUNCTIONED. NR 3 ENG ROLLBACK AT FL370, ENG IGN OVERRIDE ON. ENGINE RESTARTED ITSELF AT FL 270 IN CLOUDS -10C WITH ALL ENG ANTI-ICE ON. ROLL BACK RESULTED IN N1 OF 48 PERCE
- [SDR 08FDEA04876](https://openairdocs.org/sdr/08FDEA04876), Nov 14, 2008: SEAT TRACK. WORN. MAIN CARGO DECK SEAT TRACK AT STA 879 TO 919 LBL 107 HAS SEVERAL FASTENER HOLES DAMAGED ON THE OTBD LOWER LEG FROM PREVIOUS REWORK. REMOVED AND REPLACED SEAT TR
- [SDR 08FDEA04562](https://openairdocs.org/sdr/08FDEA04562), Oct 27, 2008: SEAT TRACK. DAMAGED. MCDECK SEAT TRACK AT STA 1089 LBL 48 IS DAMAGED, REMOVED FLOORBOARDS FOR ACCESS. REMOVED SEAT TRACK, FABRICATED NEW TRACK. INSTALLED NEW TRACK AND REINSTALLED F
- [SDR 07FDEA02341](https://openairdocs.org/sdr/07FDEA02341), Jun 29, 2007: UNKNOWN. UNKNOWN. EN ROUTE TO SEA, NOTICED ON PNEUMATIC PNL RED MANF NR 3 LIGHT AND AMBER BLEED OFF LIGHT. PNEUMATIC SYNOPTIC PG SHOWED NR 3 PNEU MANF IN THE RED AND PRESS IN MAN
- [SDR 07FDEA01983](https://openairdocs.org/sdr/07FDEA01983), May 25, 2007: SPAR. CRACKED. RT HORIZONTAL STABILIZER OUTBOARD LEADING BOTTOM ATTACH ANGLE CRACKED. REPAIRED IAW FEDEX EA NR 8-5510-109166 "STABILIZERS, RT STAB LOWER LEADING EDGE, SPAR CRA
- [SDR 07FDEA01982](https://openairdocs.org/sdr/07FDEA01982), May 25, 2007: FLOORBEAM. CORRODED. FORWARD LOWER CARGO, DOOR TORQUE BOX FORWARD FRAME CORRODED. REMOVED CORROSION FROM FRAME AND SUPPORT BRACKET AND FOUND BOTH TO EXCEED ALLOWABLE LIMITS IAW MD/D
- [SDR 07FDEA01981](https://openairdocs.org/sdr/07FDEA01981), May 25, 2007: FRAME. CORRODED. FORWARD LOWER CARGO, DOOR TORQUE BOX FORWARD FRAME CORRODED. REMOVED CORROSION FROM FRAME AND WEB AND FOUND MATERIAL LOSS FOR BOTH TO EXCEED ALLOWABLE LIMITS IA
- [SDR 07FDEA01965](https://openairdocs.org/sdr/07FDEA01965), May 24, 2007: WEDGE. DENTED. LEFT INBOARD ELEVATOR TRAILING EDGE DENTED AT MID-SECTION AREA. REMOVED DAMAGED SECTION OF LEFT INBOARD ELEVATOR PER DC/MD10 SRM 51-31-01 VOL 11. RECEIVED NEW T
- [SDR 07FDEA01944](https://openairdocs.org/sdr/07FDEA01944), May 22, 2007: FITTING. CORRODED. MAIN CARGO DOOR NR 7 LATCH SPOOL AND FITTING IS CORRODED. REMOVED NR 7 SPOOL IAW FEDEX EA NR 8-5230-110663 REV A. " FUSELAGE-MAIN CARGO DOOR - LOWER JAMB SUPPOR
- [SDR 07FDEA01942](https://openairdocs.org/sdr/07FDEA01942), May 22, 2007: FITTING. CORRODED. MAIN CARGO DOOR-LOWER JAMB FITTING NR 4 SHOWS CORROSION AT AFT UPPER HOLE. REPAIRED NR 4 LOWER JAMB FITTING AND WEB IAW FEDEX EA 8-5230-110663 REV A. "FUSELAGE-
- [SDR 07FDEA01941](https://openairdocs.org/sdr/07FDEA01941), May 22, 2007: FITTING. CORRODED. MAIN CARGO DOOR-LOWER JAMB FITTING NR 5 SHOWS CORROSION AT LOWER FORWARD HOLE. REPAIRED NR 5 LOWER JAMB AND REPLACED SUPPORT FITTING IAW FEDEX EA 8-5230-110663 
- [SDR 07FDEA01940](https://openairdocs.org/sdr/07FDEA01940), May 22, 2007: FITTING. CORRODED. MAIN CARGO DOOR LOWER JAMB FITTING NR 2 SHOWS CORROSION AT LOWER FORWARD HOLE. REPAIRED LOWER JAMB AND REPLACED SUPPORT FITTING NR 2 IAW FEDEX EA. 8-5230-110663
- [SDR 07FDEA01939](https://openairdocs.org/sdr/07FDEA01939), May 22, 2007: FITTING. CORRODED. MAIN CARGO DOOR-LOWER JAMB FITTING NR 1 SHOWS CORROSION AT LOWER FORWARD HOLE. REPAIRED LOWER JAMB AND REPLACED SUPPORT FITTING NR 1 IAW FEDEX EA 8-5230-110663.
- [SDR 07FDEA01938](https://openairdocs.org/sdr/07FDEA01938), May 22, 2007: FITTING. CORRODED. MAIN CARGO DOOR-LOWER JAMB FITTING NR 3 SHOWS CORROSION AT AFT LOWER HOLE. REPAIRED NR 3 LOWER JAMB WEB IAW FEDEX EA 8-5230-110663 REV. A. " FUSELAGE, MAIN CARG
- [SDR 07FDEA01937](https://openairdocs.org/sdr/07FDEA01937), May 22, 2007: FITTING. CORRODED. MAIN CARGO DOOR LOWER JAMB FITTING NR 3 SHOWS CORROSION AT FORWARD LOWER HOLE. REPAIRED NR 3 LOWER JAMB AND REPLACED SUPPORT FITTING IAW FEDEX EA 8-5230-110663 
- [SDR 07FDEA01945](https://openairdocs.org/sdr/07FDEA01945), May 22, 2007: FITTING. CORRODED. MAIN CARGO DOOR NR 6 LATCH SPOOL AND FITTING IS CORRODED. REMOVED NR 6 SPOOL IAW DC/MD10 FEDEX EA NR 8-5230-110663 STEPS 5A AND B. CLEANED,TREATED AND PRIMED IA
- [SDR 07FDEA01943](https://openairdocs.org/sdr/07FDEA01943), May 22, 2007: FITTING. CORRODED. COMPLY WITH FEDEX EA NR 8-5230-110663 "FUSELAGE-MAIN CARGO DOOR - LOWER JAMB FITTING INSPECTION AND DOOR RIG". COMPLIED WITH FEDEX EA NR 8-5230-110663 "FUSELAGE
- [SDR 07FDEA01846](https://openairdocs.org/sdr/07FDEA01846), May 18, 2007: FRAME. CRACKED. RIGHT WING LEADING EDGE FORMER CRACKED AT XOS625.5 STOP DRILLED CRACK AND INSTALLED REPAIR CLIP PER MD/DC 10-10 SRM 57-20-00 FIG 1 VOL I . FUEL CONTROL PANEL WA
- [SDR 07FDEA01835](https://openairdocs.org/sdr/07FDEA01835), May 17, 2007: BUSHING. LOOSE. LEFT OUTBD ELEVATOR THIRD HINGE FROM INBD SIDE HAT BUSHINGS LOOSE IN FITTING BORE FOR OUTBOARD DAMPNER. REMOVED AND REPLACED LT O/B ELEVATOR THIRD HINGE FROM I/
- [SDR 07FDEA01834](https://openairdocs.org/sdr/07FDEA01834), May 17, 2007: BUSHING. CORRODED. RT O/B ELEVATOR I/B ACTUATOR MOUNT FITTING (ON ELEVATOR) CORRODED ON I/B SIDE. REMOVED CORROSION/DAMAGE IAW DAC CMM 55-21-01. REMOVED, FABRICATED AND INSTALLED 
- [SDR 07FDEA01833](https://openairdocs.org/sdr/07FDEA01833), May 17, 2007: BUSHING. LOOSE. RT O/B ELEVATOR I/B DAMPNER HINGE FITTING HAT BUSHINGS ARE LOOSE. REMOVED AND REPLACED RT O/B ELEVATOR I/B DAMPNER HINGE FITTING HAT BUSHINGS IAW CMM 55-21-01 A
- [SDR 07FDEA01832](https://openairdocs.org/sdr/07FDEA01832), May 17, 2007: BUSHING. LOOSE. RT O/B ELEVATOR O/B DAMPER HINGE FITTING HAT BUSHINGS ARE LOOSE. REMOVED AND REPLACED RT O/B ELEVATOR O/B ELEVATOR O/B DAMPNER HINGE FITTING HAT BUSHINGS IAW CM
- [SDR 07FDEA01825](https://openairdocs.org/sdr/07FDEA01825), May 16, 2007: SKIN. CRACKED. RT INBOARD ELEVATOR UPPER SKIN IS CRACKED ON EDGE. CUT OUT DAMAGED SKIN, FABRICATED REPAIR DOUBLER AND FILLER, AND INSTALLED REF. DC/MD 10 SRM 55-00-01 FIG 3 VO
- [SDR 07FDEA01824](https://openairdocs.org/sdr/07FDEA01824), May 16, 2007: SKIN. CRACKED. DURING DENT EVALUATION ON RT OUTBOARD ELEVATOR UPPER SKIN HFEC INSPECTION REVEALED A 1" CRACK. CUT OUT DAMAGED SKIN, FABRICATED REPAIR DOUBLER AND FILLER AND IN
- [SDR 07FDEA01736](https://openairdocs.org/sdr/07FDEA01736), May 10, 2007: SEAT TRACK. CORRODED. AFT LOWER CARGO, CORROSION AT TIEDOWN SEAT TRACK SURFACE AND AT NUT PLATES HOLES UPPER AND LOWER SURFACES, FS 1790-167 LBL 21". REMOVED DAMAGE SEAT TRACK SECTIO
- [SDR 07FDEA01709](https://openairdocs.org/sdr/07FDEA01709), May 6, 2007: SEAT TRACK. BROKEN. CABIN FLOOR SEAT TRACK LUG BROKEN OUT AT STA 635 LBL47. REMOVED AND REPLACED CABIN FLOOR SEAT TRACK SECTION FROM STA 622 TO STA 746 LBL47 IAW DC/MD10 SRM 53-70-
- [SDR 07FDEA01708](https://openairdocs.org/sdr/07FDEA01708), May 6, 2007: SEAT TRACK. GOUGED. CABIN FLOOR SEAT TRACK GOUGED AT STA 1161 TO STA 1171 LBL 48. REMOVED AND REPLACED CABIN SEAT TRACK FROM STA 1129 TO STA 1189, LBL 48 IAW DC/MD10 SRM 53-70-00 F
- [SDR 07FDEA01707](https://openairdocs.org/sdr/07FDEA01707), May 4, 2007: SEAT TRACK. WORN. MAIN CABIN SEAT TRACK WORN STA 635 BL 8.5. REMOVED AND REPLACED SEAT TRACK REF DC/MD 10 SRM 51-10-01 VOL III PG 85 53-70-00 VOL I FIG 1, 51-31-01 VOL II PG 4 , 
- [SDR 07FDEA01706](https://openairdocs.org/sdr/07FDEA01706), May 4, 2007: SEAT TRACK. GOUGED. CABIN FLOOR SEAT TRACK GOUGED BETWEEN STA-1019 AND STA 1039 LBL 50. REMOVED AND REPLACED MAIN CABIN FLOOR SEAT TRACK AT LBL 50 FROM STA 1006 TO STA 1046 IAW DC/
- [SDR 07FDEA01685](https://openairdocs.org/sdr/07FDEA01685), May 2, 2007: DOUBLER. CORRODED. AFT FUSELAGE WASTE TANK COMPT, FRAME LWR FWD AND AFT CHORDS AT LONGERONS ATTACH FASTENERS HAVE CORROSION BETWEEN L49R AND L52 AT STA 1997 REMOVED FASTENERS FROM
- [SDR 07FDEA01679](https://openairdocs.org/sdr/07FDEA01679), May 1, 2007: FITTING. CRACKED. MAIN CARGO DOOR-LOWER JAMB FITTING NR 5 SHOWS CRACK/CORROSION AT LOWER HOLE.
- [SDR 07FDEA01676](https://openairdocs.org/sdr/07FDEA01676), May 1, 2007: FLANGE. CRACKED. RT HORIZONTAL STAB CENTER LE SECTION OB UPPER ATTACH POINT FLANGE CRACKED AT NUTPLATES. REMOVED AND REPLACED RT HORIZONTAL LE SECTIONS CENTER OUTBOARD UPPER "T"
- [SDR 07FDEA01673](https://openairdocs.org/sdr/07FDEA01673), Apr 30, 2007: RIB. CRACKED. RT HORIZONTAL STABILIZER I/B L/E SECTION NOSE O/B RIB FLANGE CRACKED XFS108, AND ATTACHED CLIP HAS SHEARED FASTENER. INSTALLED REPAIR ANGLE AND STOP DRILLED CRA
- [SDR 07FDEA01672](https://openairdocs.org/sdr/07FDEA01672), Apr 30, 2007: SEAT TRACK. BENT. MAIN CABIN SEAT TRACK BENT SEVERAL AREAS BETWEEN STA. 625 AND STA. 775, BL107.5. REMOVED BENT AREAS IAW EA NR 8-5310-11060411, (FUSELAGE MAINFRAME-SEAT TRACK BE
- [SDR 07FDEA01671](https://openairdocs.org/sdr/07FDEA01671), Apr 30, 2007: ANGLE. CRACKED. RT HORIZONTAL L/E CENTER I/B SECTION UPPER I/B ATTACHED FLANGE CRACKED MARKED. REMOVED CRACKED RT HORIZ L/E T-CAP SECTION AT UPPER I/B STA XFS 166 IAW DC/MD 10 
- [SDR 07FDEA01634](https://openairdocs.org/sdr/07FDEA01634), Apr 26, 2007: DOOR. CORRODED. FWD PIT HAS CORROSION IN THE AFT CORNER BETWEEN DOOR SEAL AND BEAM. [SUP 05-30-07] REMOVED CORROSION FROM RAIL AND FOUND MATERIAL LOSS TO WITHIN ALLOWABLE LIMIT
- [SDR 07FDEA01631](https://openairdocs.org/sdr/07FDEA01631), Apr 26, 2007: BEAM. CORRODED. FWD PIT HAS CORROSION IN THE FORWARD LOWER CORNER BETWEEN DOOR SEAL AND BEAM. [SUP 05-30-07] REMOVED CORROSION FROM RAIL, VERIFIED BLEND OUT AND REMAINING THICK
- [SDR 07FDEA01587](https://openairdocs.org/sdr/07FDEA01587), Apr 24, 2007: HANDLE. WORN. R1 DOOR EMERGENCY HANDLE BACKLOCK DOES NOT HOLD HANDLE ONCE HANDLE IS MOVED TO EMERGENCY POSITION. FOUND OVERRIDE LEVER BINDING WITH BACKLOCK. REPLACED BUSHING,
- [SDR 07FDEA01534](https://openairdocs.org/sdr/07FDEA01534), Apr 22, 2007: SKIN. GOUGED. LT WING O/B FLAP O/B LOWER SKIN GOUGED ON INTERIOR SIDE. CUT OUT DAMAGED PART REF; DC/MD10-10 SRM 57-10-00 FIG 85 VOL 1. FABBED DOUBLER REF; DC/MD10-10 SRM 57-1
- [SDR 07FDEA01533](https://openairdocs.org/sdr/07FDEA01533), Apr 22, 2007: SKIN. GOUGED. LT WING O/B FLAP O/B LOWER SKIN GOUGED ON INTERIOR SIDE. CUT OUT DAMAGE REF; DC/MD10-10 SRM 57-10-00 FIG 85 VOL 1. FABBED REPAIR DOUBLER. [SUP 04-30-07] REF; DC
- [SDR 06FDEA03143](https://openairdocs.org/sdr/06FDEA03143), Aug 30, 2006: SHUTOFF VALVE. INOPERATIVE. LEVEL 3 MANF FAIL SYS 1 RAN QRH, DIVERTED TO SMF PER CREW VERBAL, ALERT APPEARED WHEN WING ANTI-ICE MEL. ACN RELEASED FOR SERVICE PER MEL/CDL: 30-11-01 CATEGORY
- [SDR 06FDEA1114](https://openairdocs.org/sdr/06FDEA1114), Mar 12, 2006: WARNING SYSTEM. MALFUNCTIONED. UNSAFE GEAR IND RT MAIN AFTER T/O PRI AND SEC DISPLAY. FOLLOWED CHECKLIST TO SAFE GEAR UP CONDITION. FACT INSP RT GEAR AND DOOR AREA FOR DAMAGE OR DEFECTS WITH 
- [SDR 06FDEA0868](https://openairdocs.org/sdr/06FDEA0868), Feb 28, 2006: FINGER DOUBLER. CORRODED. LT OUTBOARD AILERON, I/B UPPER SKIN FINGER DOUBLERS DELAMINATED WITH CORROSION. FABRICATED AND INSTALLED NEW SKIN IAW DC 10 SRM 51-35-01 VOL II AND DAC DWG ARC1

All 63: https://openairdocs.org/deregistered/N68050-2024-04-13/reports.md

## FAA accident and incident reports (4)

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 19850203007079I](https://openairdocs.org/incident/19850203007079I), Feb 3, 1985: Doug DC1010F (N68050), Memphis, TN. Electronics compartment door warning light came on. Door was reclosed, departed. Follow up check at destination.
- [Incident 19800512090801I](https://openairdocs.org/incident/19800512090801I), May 12, 1980: Doug DC1010F (N68050), Chicago, IL, Minor damage. Struck aircraft while both were taxiing. N776NC.
- [Incident 19790216006029I](https://openairdocs.org/incident/19790216006029I), Feb 16, 1979: Doug DC1010F (N68050), Houston, TX. Ground observer thought tire blew on takeoff.
- [Incident 19781106023209I](https://openairdocs.org/incident/19781106023209I), Nov 6, 1978: Doug DC10/ (N68050), Houston, TX. Crew heard noises in tail. After landing found cargo door seal hanging out. It was slapping the airplane.

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