# N386FE: 1973 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: 46620 - Year built: 1973 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: January 6, 2001 - Last registry action: July 10, 2023 - Mode S code: A47216 - 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/N386FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=386FE - Page: https://openairdocs.org/deregistered/N386FE-2024-04-13 From the FAA registry file of November 3, 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 (34) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FDEA201302090312](https://openairdocs.org/sdr/FDEA201302090312), Feb 9, 2013: GIRT BAR. OBSTRUCTED. OUTSIDE INDICATOR OF SAFE OR EMERGENCY (RED LEVER) LT SIDE OF JET STICKS TO "EMERGENCY". EMERGENCY OVERRIDE LEVER DOES NOT CORRESPOND TO ACTION ON DISARM LEVER - [SDR FDEA201111235006](https://openairdocs.org/sdr/FDEA201111235006), Nov 23, 2011: ELEMENT. FAILED. AFTER TAKEOFF, WITH NR 2 PACK OFF, CLIMBING PASSED 14000' MSL. RECEIVED NR 2 MANIFOLD FAILURE LEVEL ALERT, RTB LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR - [SDR FDEA201103311255](https://openairdocs.org/sdr/FDEA201103311255), Mar 31, 2011: WARNING LIGHT. ILLUMINATED. CLIMBING THRU 13,000' GOT LVL 3" BLD AIR 1 TEMP HI", COMPLIED WITH QRH. PERFORMED RTS ON ALL 3 AIU'S, ALL TESTS PASSED. PERFORMED RTS ON PNEUMATIC SYS CONTROLLE - [SDR FDEA201103181170](https://openairdocs.org/sdr/FDEA201103181170), Mar 18, 2011: SKIN. CORRODED. SKIN BULGING AT APPROX STA 859, STRINGER 43R FWD OF FWD CARGO DOOR, 6 INCHES IN LENGTH. INSPECTED, FOUND EXTERIOR SKIN OK. CORROSION FOUND UNDER SKIN AT RAIL AR - [SDR FDEA201103020825](https://openairdocs.org/sdr/FDEA201103020825), Mar 2, 2011: FLOORBEAM. CORRODED. CENTER CARGO COMPARTMENT FLOORBEAM CORRODED/EXFOLIATED AT BS 1781, RBL 36. - [SDR FDEA201103021171](https://openairdocs.org/sdr/FDEA201103021171), Mar 2, 2011: FITTING. CRACKED. CAC COMPARTMENT FITTING AT THE PRESSURE DOME ADJACENT TO THE "SUGAR SCOOP" HAS A 2 IN CRACK IN THE LOWER LARGE RADIUS. (PN AYB7000-1) REMOVED CRACKED FITTING AN - [SDR FDEA201102040467](https://openairdocs.org/sdr/FDEA201102040467), Feb 4, 2011: POWER SUPPLY. FAILED. EMERGENCY LIGHT TEST FAIL MEL 04FEB11. RELEASED FOR SERVICE IAW MEL: 33-50-02, CATEGORY: C. R & R EMERGENCY EXIT LIGHTS POWER-SUPPLY IAW AMM 33-51-01-4. OPS CHE - [SDR FDEA200904021164](https://openairdocs.org/sdr/FDEA200904021164), Apr 2, 2009: NONE. NONE. AT BEGINNING OF TAKEOFF ROLL, LEVEL 1 'UNABLE RNP'. DURING TAX IN, RNP INDICATED 4.1 NM. UPON RETURN TO BLOCKS, TROUBLESHOT THE CFDS/ MCDU: NO FAULTS PERFORMED - [SDR FDEA200902190593](https://openairdocs.org/sdr/FDEA200902190593), Feb 19, 2009: SPAR CAP. CRACKED. FUEL LEAK LT WING LOWER REAR SPAR CAP AT WS XORS 346, INDICATION OF CRACK AT THE POINT OF LEAK. REAR SPAR REPAIRED AS PER E.A. 8-5710-126158. SEQ.#924. - [SDR FDEA200902020425](https://openairdocs.org/sdr/FDEA200902020425), Feb 2, 2009: WINDOW FRAME. CRACKED. CAPTAIN SLIDING VIEW WINDOW FRAME AIRPLANE SIDE CRACKED OUTSIDE (MARKED). - [SDR 07FDEA04975](https://openairdocs.org/sdr/07FDEA04975), Dec 1, 2007: CONTROL VALVE. MALFUNCTIONED. ON INITIAL GEAR EXTENSION GOT ALL RED AND NO GREEN ON LIGHTS AND CONFIG PAGE. SAME ON SECOND ATTEMPT. NO WIND NOISE ON 1ST AND SECOND TIME, THIRD TIME ALL GREEN - [SDR 07FDEA04381](https://openairdocs.org/sdr/07FDEA04381), Sep 29, 2007: ENGINE. DAMAGED. CLIMBING THROUGH FL190 AIRCRAFT SHUDDERED TWICE WITH SLIGHT YAW TO LEFT. LOOKED DOWN AND "ENG 1 EXCEEDENCE" ALERT AND RED BOXED ENG 1 EGT "951". PULLED ENG 1 TO - [SDR 06FDEA1312](https://openairdocs.org/sdr/06FDEA1312), Apr 5, 2006: ENGINE. FAILED. ON CLIMBOUT TO CRUISE ALTITUDE PASSING 28,000 FT HEARD A THUD & EXPERIENCED AIRCRAFT YAW TO THE RIGHT. ENGINE INSTRUMENTS INDICATED NR 3 ENGINE FAILURE. SHUT DO - [SDR 06FDEA1310](https://openairdocs.org/sdr/06FDEA1310), Apr 4, 2006: ENGINE. FAILED. ON CLIMB-OUT TO CRUISE, ALTITUDE PASSING 28000' HEARD A "THUD" AND EXPERIENCED AIRCRAFT YAW TO THE RIGHT. ENGINE INSTRUMENTS INDICATED NR 3 ENGINE FAILURE. SHUT - [SDR 04FDEA02071](https://openairdocs.org/sdr/04FDEA02071), Jul 14, 2004: FLOORBEAM. DAMAGED. FLOORBEAM AT FUSELAGE STATION 1921, LBL 50, FOUND DAMAGED ON EDGE OF CUTOUT, AT CABLE LOCATION. COMPLIED WITH FEDEX EA 8-5310-77598, FUSELAGE STATION 1921, X=-5 - [SDR 04FDEA02026](https://openairdocs.org/sdr/04FDEA02026), Jul 7, 2004: CONTROL CABLE. CROSSED. AFT PIT BEHIND STATION 1967, 36 INCHES, LEFT BUTT LINE CABLES CROSSED BELOW MAIN CABIN FLOOR. OPENED CEILING PANELS AND REMOVED LEFT HAND VERTICAL ACCESS PANELS - [SDR 04FDEA02025](https://openairdocs.org/sdr/04FDEA02025), Jul 7, 2004: PANEL. DENTED. RIGHT HAND WING TRAILING EDGE INBOARD LOWER PANEL NUMBER 641 BB HAS NUMEROUS DENTS IN ITS UPPER SURFACE. REPAIRED BY FABRICATING AND BONDING NEW METAL OUTER SKI - [SDR 04FDEA02022](https://openairdocs.org/sdr/04FDEA02022), Jul 7, 2004: SKIN. DENTED. SEVERAL DENTS IN REPAIR DOUBLER, JUST AFT OF LOWER FWD CARGO DOOR. REMOVED DOUBLER AND TRIPLER. FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW DC10 SRM 53-20- - [SDR 04FDEA02021](https://openairdocs.org/sdr/04FDEA02021), Jul 7, 2004: SKIN. DENTED. SEVERAL DENTS IN REPAIR DOUBLER, JUST AFT OF LOWER FWD CARGO DOOR. REMOVED DOUBLER AND TRIPLER. FABRICATED AND INSTALLED DOUBLER AND TRIPLER IAW DC10 SRM 53-20- - [SDR 04FDEA02019](https://openairdocs.org/sdr/04FDEA02019), Jul 7, 2004: DOOR FRAME. CORRODED. FORWARD PIT, FORWARD DOOR FRAME STATION 886 HAS CORROSION. DOOR FRAME FOUND TO BE OUT OF LIMITS. CUT AND REMOVED CORRODED FRAME SECTION, CUT WEB TO FOM. FABRICA - [SDR 04FDEA02018](https://openairdocs.org/sdr/04FDEA02018), Jul 7, 2004: STATIC PORT. DAMAGED. RIGHT PRIMARY STATIC PORT FAILS RVSM CONVEXITY AND CONCAVITY AND WAVINESS INSPECTION IAW WORK CARD 34C1501 STEP 9 AND 10. REMOVED AND REPLACED RIGHT HAND PRIMAR - [SDR 04FDEA02016](https://openairdocs.org/sdr/04FDEA02016), Jul 7, 2004: SKIN. CORRODED. RIGHT HAND WING INBOARD AILERON LOWER SKIN BULGED/CORRODED AND I EACH FASTENER POPPED. REMOVED AND REPLACED INBOARD AILERON LOWER SKIN PER FEDEX EA 8-5750-77595 - [SDR 04FDEA02015](https://openairdocs.org/sdr/04FDEA02015), Jul 7, 2004: BEAM. CRACKED. RIGHT WING INBOARD AILERON LOWER BEAM CRACKED AT END. REMOVE TEE-CAP IAW DC10 SRM 51-35-01 VOL I, FABRICATED -4 TEE CAP IAW DCA DWG ARC 3012 AND DC10 SRM 51-10- - [SDR 04FDEA00468](https://openairdocs.org/sdr/04FDEA00468), Feb 20, 2004: WARNING SYSTEM. ACTIVATED. AT 6000 FT ON DOWN WIND LEG WITH SLATS EXTENED AND 180 KTS,THE LEVEL 2 FUEL USED ALERT CAME ON. FUEL USED AND FUEL REMAINING EQUALLED DEPARTURE FUEL. APPROXIMAT - [SDR 03FDEA01948](https://openairdocs.org/sdr/03FDEA01948), Nov 18, 2003: SELECTOR VALVE. FAILED. AT 180 KTS ON FINAL DROPPED LANDING GEAR AND GOT UNSAFE ON BOTH PRI-SEC. CYCLED GEAR WITH SAME RESULT. INITIATED GO-AROUND. AT 210 KTS ON VECTORS CYCLED GEAR AN - [SDR 03FDEA00780](https://openairdocs.org/sdr/03FDEA00780), May 20, 2003: ENGINE. MALFUNCTIONED. CRUISE ALT (FL370) ANC -- SEA 2+19 ENROUTE TIME "ENG NR 3 OIL PRESS LOW" ALERT. FOLLOWED APPROPRIATE CHECKLIST & LANDED AT DESTINATION. EMERGENCY DECLARED. FOUN - [SDR 02FDEA00953](https://openairdocs.org/sdr/02FDEA00953), Dec 17, 2002: MOTOR. FAILED. R1 ENTRY DOOR HARD TO OPEN, MOTOR SOUNDS LIKE IT SPINS, CLUTCH SLIPS. REMOVED AND REPLACED R1 DOOR ELECTRIC MOTOR, SHAFT, BEARINGS, AND PNEUMATIC MOTOR REF MM. - [SDR 02FDEA00954](https://openairdocs.org/sdr/02FDEA00954), Dec 17, 2002: BEARING. WORN. RT WING OUTBOARD FLAP CARRIAGE ASSY HAS 2 SMALL ROLLER BEARINGS WORN. REMOVED AND REPLACED 2 SMALL ROLLER BEARINGS. - [SDR 02FDEA00948](https://openairdocs.org/sdr/02FDEA00948), Dec 16, 2002: BRAKE ASSY. DAMAGED. NUMBER 2 BRAKE BINDING. DURING TIRE CHANGE, FOUND FIRST THREE SETS OF ROTORS FROZEN & STUCK. REMOVED OLD DEFECTIVE NR 2 BRAKE AND INSTALLED NEW BRAKE IAW MM. - [SDR 02FDEA00918](https://openairdocs.org/sdr/02FDEA00918), Dec 4, 2002: DUCT. OVERHEATED. RADIO RACK FAN EXHAUST DUCT EXHIBITS SIGNS OF FIRE AND OVERHEATING, INSULATION BLANKETS AND FOAM MATERIAL FROM INSIDE OF DUCT BELOW MAIN CABIN FLOORING AT BS 47 - [SDR 02FDEA00921](https://openairdocs.org/sdr/02FDEA00921), Dec 4, 2002: MOTOR. FAILED. DOOR HARD TO OPEN. MOTOR SOUNDS LIKE SPINS, CLUTCH SLIPS. R/R R1 DOOR ELECTRIC MOTOR, SHAFT, BEARINGS AND PNEU MOTOR REF MM 52-11-01-02. - [SDR 02FDEA00772](https://openairdocs.org/sdr/02FDEA00772), Oct 26, 2002: O-RING. DAMAGED. NR 3 HYDRAULIC QUANTITY DROPPED TO 4.9 GAL. WITH HYDRAULIC 3 ELEVATOR OFF LEVEL 2 ALERT, DECLARED EMERGENCY. APPROACH, LANDING AND TAXI NORMAL. ON BLOCK IN NR 3 - [SDR 98FDEA00475](https://openairdocs.org/sdr/98FDEA00475), Jul 29, 1998: FITTING. CORRODED. SNRM 042 STA-LAX - CORROSION FOUND TO EXCEED LIMITS ON NR 1 PYLON AFT MOUNT BULKHEAD FITTING. REMOVED AND REPLACED NR 1 PYLON AFT BULKHEAD FITTING PER SRM 51-00 - [SDR 98FDEA00324](https://openairdocs.org/sdr/98FDEA00324), May 3, 1998: FITTING. CRACKED. STA-LAX - NR 3 PYLON HAS A HIGH FREQUENCY EDDY CURRENT CRACK INDICATION IN THE OUTBOARD ENGINE TRUSS FITTING AS PER FED-EX EO 8-5410-7-3323 PT W. COMPLIED WITH ## 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 DCA06FA033](https://openairdocs.org/ntsb/DCA06FA033), Apr 4, 2006: Mcdonnell Douglas DC10 (N386FE), Memphis, TN, substantial damage. Probable cause: The rupture of a fatigue crack in the forward air seal tooth serration of the No. 3 engine low pressure turbine stage 1 disk that initiated due to an improper weld repair performed during original… ## 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. - [Accident 20060404004029A](https://openairdocs.org/incident/20060404004029A), Apr 4, 2006: Doug MD1010F (N386FE), Jonesboro, AR, Substantial damage. (-23) On 4 April 2006 at approximately 1550 hours fedex flight #597, N386FE, an MD-10-10, was enroute from memphis to seattle when the crew experienced engine… --- 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.