# N387FE: 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 CF6-6D](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: 46621
- Year built: 1974
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 27, 2007
- Last registry action: July 10, 2023
- Mode S code: A475CD
- 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/N387FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=387FE
- Page: https://openairdocs.org/deregistered/N387FE-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 (64, newest 50)

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

- [SDR FDEA201209253431](https://openairdocs.org/sdr/FDEA201209253431), Sep 25, 2012: HANDLE. MALFUNCTIONED. ON DEPARTURE, RAISED THE GEAR AND THE RED UNSAFE INDICATIONS REMAINED ON AT THE GEAR HANDLE PANEL AND ON THE CONFIGURATION SYNOPTIC PAGE. RECYCLED THE GEAR IAW 
- [SDR FDEA201201260335](https://openairdocs.org/sdr/FDEA201201260335), Jan 26, 2012: COALESCER BAG. ODOR. IN CRUISE, WITH PACK 1 & PACK 3 ON, SMELLED FUMES IN COCKPIT. TURNED ON PACK 2 AND TURNED OFF PACK 1, THE ODOR STOPPED. REPLACED COALESTER BAG ON NR1 PACK IAW M
- [SDR FDEA201105171852](https://openairdocs.org/sdr/FDEA201105171852), May 17, 2011: PRESSURE SWITCH. FAILED. AT FL 370, GOT AIR SYS 3 OFF WITH ILLUMINATED RED MFG LIGHT. RAN QRH. MOMENTARY LEVEL 3 AIR MFG 3 FAIL WITH TRI TONE, DIVERT. T/S IAW FIM 36-23 ITEM 3, CHECKED 
- [SDR FDEA201009173519](https://openairdocs.org/sdr/FDEA201009173519), Sep 17, 2010: PAN. CORRODED. AT APPROX FS 383 LAV SERVICE PANEL. THE LAV PAN HAS CORROSION AND CRACKED FLANGE. R & R PAN AND DOUBLER. REF SRM 51-35-01
- [SDR FDEA201009163510](https://openairdocs.org/sdr/FDEA201009163510), Sep 16, 2010: BULKHEAD. CORRODED. LT WHEEL WELL FWD BULKHEAD SLANT PANEL LWR OTBD CORNER HAS CORROSION. REPAIRED SLANT PANEL TO REAR SPAR CAP ANGLE. REF SRM 53-40-00
- [SDR FDEA200907202679](https://openairdocs.org/sdr/FDEA200907202679), Jul 20, 2009: ENGINE. MALFUNCTIONED. REJECTED T/O PDX 28L NR 2 ENGINE N2 EXCEEDENACE 90KTS. INSPECTED EXHAUST FOR PARTICLES NONE FOUND. ACFT OK FOR SERVICE. REMOVED BOROSCOPE PLUGS FOR INSPECTION A
- [SDR FDEA200812025049](https://openairdocs.org/sdr/FDEA200812025049), Dec 2, 2008: SPAR. CRACKED. NR 3 PYLON HORIZONTAL UPPER SPAR WEB HAS 4 INCH CRACK, REFERENCE INSPECTION OF PYLON S177 WORKCARD 54X1201ALI-P2. COMPLIED WITH HFEC. VERIFIED NR 3 PYLON HORIZO
- [SDR FDEA200811285002](https://openairdocs.org/sdr/FDEA200811285002), Nov 28, 2008: SKIN. CRACKED. RT HORIZONTAL STAB FRONT SPAR CAP AND UPPER PORTION OF THE SKIN CRACKED AT STA XF 88.834, (N/R 513 GENERATED WO 43105). INSTALLED RT HORIZONTAL STAB FRONT SPAR 
- [SDR 07FDEA02234](https://openairdocs.org/sdr/07FDEA02234), Jun 21, 2007: SKIN. CRACKED. 1 CRACK LONG 1" ON EXT SKIN LOWER AT STA 485 RT SIDE DOOR FWD W/W REPAIRED IAW SRM 53-50-00 FIG 25 VOL 1.
- [SDR 07FDEA02233](https://openairdocs.org/sdr/07FDEA02233), Jun 21, 2007: SKIN. MISREPAIRED. EXISTING REPAIR EXT FUS FROM STA 1901 TO 1921 BETWEEN LONGERONS 37 LT AND 35 LT REPAIRED IAW SRM 53-20-00 FIG 6 VOL I.
- [SDR 07FDEA02141](https://openairdocs.org/sdr/07FDEA02141), Jun 15, 2007: DOUBLER. DAMAGED. EXISTING SKIN REPAIR RIGHT WING L/E SKIN AT STA XOS 800 REPAIRED IAW SRM 57-10-00 FIG 20 VOL 1.
- [SDR 07FDEA02140](https://openairdocs.org/sdr/07FDEA02140), Jun 15, 2007: DOUBLER. DAMAGED. EXISTING SKIN REPAIR AT STA 322 X=-7 EXTERNAL SKIN REPAIRED IAW SRM 53-20-00 FIG 6.
- [SDR 07FDEA02139](https://openairdocs.org/sdr/07FDEA02139), Jun 15, 2007: REPAIR. DAMAGED. EXISTING REPAIR EXT FUSELAGE AT SAT 339 X=31 REPAIR IAW 53-20-00 FIG 6 AND SRM 57-30-00.
- [SDR 07FDEA02138](https://openairdocs.org/sdr/07FDEA02138), Jun 15, 2007: RIB. CRACKED. LT WING STATION XORS 346 STRINGERS 42-43 AND 43-44 LWR RIB CHORD CRACKED IN TWO PLACES IN THE VERTICAL LEG REPAIRED IAW SRM 57-20-00 FIG 27 SHEET 3 VOL 1.
- [SDR 07FDEA02137](https://openairdocs.org/sdr/07FDEA02137), Jun 15, 2007: SKIN. DENTED. RT O/B ELEVATOR FOUND DENT 1.25" BY 1.25 INCH DEEP 0.82" ON UPPER SKIN AT STA XE 280. REPAIR SKIN IAW SRM 55-10-00 VOL1 FIG 8.
- [SDR 07FDEA02136](https://openairdocs.org/sdr/07FDEA02136), Jun 15, 2007: WEB. WORN. ON PYLON, NR 3 DEEP WEAR ON UPPER SURFACE OF HORIZONTAL WEB AT STA YN 200. REPAIRED IAW SRM 54-20-00 FIG 5.
- [SDR 07FDEA02135](https://openairdocs.org/sdr/07FDEA02135), Jun 15, 2007: STRUCTURE. LEAKING. HEAVY LEAK ON LT WING REAR SPAR AREA AT M22 DOUBLERS REMOVE CLIP TO GAIN ACCESS AND RESEAL AREA IAW SRM 51-33-01 VOL II AND MM 28-11-01-2.
- [SDR 07FDEA02134](https://openairdocs.org/sdr/07FDEA02134), Jun 15, 2007: DOUBLER. CRACKED. CAC COMPT CRACK .50" ON DOUBLER OF BULKHEAD AT STA 1156 LONG 40 LT ACCOMPLISHED EA NR 8-5330-108092.
- [SDR 07FDEA01993](https://openairdocs.org/sdr/07FDEA01993), May 29, 2007: BULKHEAD. CRACKED. CLG W/W SPACE 2 EA CRACKS ON LT VERTICAL BULKHEAD. REPAIRED IAW SRM 53-00-01 FIG 10 VOL 1.
- [SDR 07FDEA01949](https://openairdocs.org/sdr/07FDEA01949), May 23, 2007: SKIN. DENTED. LT INBOARD ELEVATOR FOUND DEEP DENT AND NICK 5.250" BY 2.25" DEEP .080" ON UPPER SKIN. REPAIRED SKIN IAW SRM 55-10-00 VOL 1 FIG 8.
- [SDR 07FDEA01936](https://openairdocs.org/sdr/07FDEA01936), May 22, 2007: STRUCTURE. CRACKED. RT WING STATION CHORD VERTICAL LEG CRACKED. CRACK TRIMMED OUT FOR RELIEF AND REPAIRED ANGLE INSTALLED IAW SRM 57-20-00 FIG 27 SHT 3 VOL 1.
- [SDR 07FDEA01935](https://openairdocs.org/sdr/07FDEA01935), May 22, 2007: RETAINER. CRACKED. FWD CARGO CUTOUT DOOR 2 CRACKS ON RETAINER SEAL AND DEEP WEAR ON EXISTING REPAIR SKIN. SKIN REPAIRED IAW SRM 53-20-00 FIG 6 AND 53-50-00 FIG 26 VOL 1. SEAL RETA
- [SDR 07FDEA01934](https://openairdocs.org/sdr/07FDEA01934), May 22, 2007: LONGERON. CORRODED. LT AIR CONDITIONING COMPT SEVERE CORROSION WITH EXFOLIATION ON LONGERON. REPLACED SECTION OF LONGERON P/N ACA3796-501 IAW SRM 53-10-00 VOL 1 FIG 6.
- [SDR 07FDEA01775](https://openairdocs.org/sdr/07FDEA01775), May 14, 2007: CHANNEL. CORRODED. FWD CARGO COMPT LIGHT CORROSION ON CHANNEL. REPAIR CHANNEL IAW SRM 53-70-00 FIG 4, SHT 1 VOL 1 PAGE 17.
- [SDR 07FDEA01773](https://openairdocs.org/sdr/07FDEA01773), May 14, 2007: SKIN. CRACKED. LT WING LOWER EXT SKIN L/E SLAT TRACK NR 10 FOUND CRACK .50" LONG CUT OUT CRACK AREA AND INSTALLED FILLER AND DOUBLER REPAIR IAW SRM 57-10-00 FIG 68 VOL 1.
- [SDR 07FDEA01771](https://openairdocs.org/sdr/07FDEA01771), May 14, 2007: DOOR FRAME. CRACKED. MAIN CABIN CRACK LONG .25" ON WEB. REPAIRED JAMB WEB IAW SRM 53-50-00 VOL 1 FIG 19 SHT 2.
- [SDR 07FDEA01769](https://openairdocs.org/sdr/07FDEA01769), May 14, 2007: ANGLE. CORRODED. AFT CARGO COMPT BILGE ON CAP ANGLES FOUND LIGHT SURFACE CORROSION. REPAIRED IAW SRM 53-30-00 VOL 1 FIG 9.
- [SDR 07FDEA01342](https://openairdocs.org/sdr/07FDEA01342), Apr 4, 2007: BULKHEAD. CRACKED. LT AIR COND COMPT CRACK 1" LONG ON VERTICAL BULKHEAD. REPAIRED WEB IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1.
- [SDR 07FDEA01341](https://openairdocs.org/sdr/07FDEA01341), Apr 4, 2007: BULKHEAD. CRACKED. RT AIR COND COMPT CRACK 1" LONG ON VERTICAL BULKHEAD. REPAIRED CRACK IAW SRM 53-30-00 FIG 6 SHT 8 VOL 1.
- [SDR 07FDEA01340](https://openairdocs.org/sdr/07FDEA01340), Apr 4, 2007: SKIN. DAMAGED. FWD AVIONIC COMPT LT SIDE 2 HOLES ON SKIN. REPAIRED IAW SRM 53-30-00 FIG 4 VOL 1.
- [SDR 07FDEA01337](https://openairdocs.org/sdr/07FDEA01337), Apr 4, 2007: STIFFENER. WORN. LT AIR COND COMPT DEEP WEAR ON VERTICAL STIFFENER. REPAIRED STIFFENER IAW SRM 53-00-01 FIG 9 SHT 7 VOL 1.
- [SDR 07FDEA01335](https://openairdocs.org/sdr/07FDEA01335), Apr 4, 2007: BULKHEAD. CRACKED. RT AIR COND COMPT CRACK 1" LONG ON VERTICAL BULKHEAD. REPAIRED WEB IAW SRM 53-30-00 FIG 6 SHT 4 VOL 1.
- [SDR 07FDEA01343](https://openairdocs.org/sdr/07FDEA01343), Apr 4, 2007: SKIN. CRACKED. LT WING LWR EXT SKIN L/E FOUND CRACK 0.5" LONG. REPAIRED CRACK IAW SRM 57-10-00 FIG 68 SHT 2 VOL 1.
- [SDR 06FDEA03905](https://openairdocs.org/sdr/06FDEA03905), Nov 5, 2006: SENSOR. FAULTY. AT SLAT RETRACTION AFTER T/O THE STICK SHAKER ACTIVATED AND SLAT DISAGREE LIGHT STAYED ILLUMINATED AND ALSO SLAT RESET LIGHT CAME ON AND STAYED ON. RAN UNSCHEDU
- [SDR 06FDEA03892](https://openairdocs.org/sdr/06FDEA03892), Nov 5, 2006: ACTUATOR. MALFUNCTIONED. AFTER T/O AT KLAX, ON SLAT RETRACTION GOT THE STICK SHAKER AND AUTO SLAT EXTENSION. RAN QRH PROCEDURE AND STILL EXPERIENCED THE SAME. DUMPED FUEL TO LANDING WEI
- [SDR 06FDEA03230](https://openairdocs.org/sdr/06FDEA03230), Sep 7, 2006: WARNING SYSTEM. ACTIVATED. AFTER TAKEOFF POWER WAS SET, MASTER WARNING LIGHT FLICKERED ON MOMENTARILY. NO OTHER LIGHTS NOTED. AFTER AIRBORNE, MASTER WARNING LIGHT STAYED ON BRIEFLY WITH N
- [SDR 04FDEA01915](https://openairdocs.org/sdr/04FDEA01915), Jul 2, 2004: SUPPORT. CRACKED. CENTER CARGO CEILING SUPPORT IS CRACKED. REMOVED AND REPLACED SUPPORT S2922781-1 AT MAE.
- [SDR 04FDEA01913](https://openairdocs.org/sdr/04FDEA01913), Jul 2, 2004: BULKHEAD. CRACKED. VERTICAL STAB BULKHEAD BELOW NR 2 ENGINE FUEL LINE DRAIN SCUFFER, BOTH ENDS GOUGED AND CRACKED. REMOVED AND REPLACED DRAIN SCUFFER SEAL FAB ON TRAVLER T4/440479
- [SDR 04FDEA01912](https://openairdocs.org/sdr/04FDEA01912), Jul 2, 2004: BULKHEAD. GOUGED. VERTICAL STAB BULKHEAD BELOW NR 2 ENGINE FUEL LINE DRAIN SCUFFER, BOTH ENDS GOUGED AND CRACKED. REMOVED AND REPLACED DRAIN SCUFFER SEAL FAB ON TRAVLER T4/440479
- [SDR 04FDEA01910](https://openairdocs.org/sdr/04FDEA01910), Jul 1, 2004: ANGLE. WORN. FUSE TAIL CONE CENTER PLATFORM LT ANGLE SUPPORT WORN. REMOVED AND REPLACED ANGLE IAW SRM 51-31-01 AT MAE.
- [SDR 04FDEA01909](https://openairdocs.org/sdr/04FDEA01909), Jul 1, 2004: GUIDE. WORN. RIGHT TAIL CONE GUIDE CAM WORN. REMOVED AND REPLACED GUIDE IAW 51-33-01 AT MAE.
- [SDR 04FDEA01898](https://openairdocs.org/sdr/04FDEA01898), Jun 30, 2004: GUIDE. WORN. LEFT TAILCONE GUIDE CAM WORN. REMOVED AND REPLACED GUIDE IAW SRM 51-33-01 AT MAE.
- [SDR 04FDEA01883](https://openairdocs.org/sdr/04FDEA01883), Jun 30, 2004: BRACKET. DAMAGED. BOTH LEFT AND RIGHT FWD SUPPORT PIN BRACKETS HAVE ELONGATED HOLES ON TAIL CONE WORK PLATFORM. REMOVED AND REPLACED BRACKETS IAW SRM 51-35-01 AT MAE.
- [SDR 04FDEA01882](https://openairdocs.org/sdr/04FDEA01882), Jun 30, 2004: ANGLE. BENT. NR 1 ENG I/B FAN COWL LWR EDGE ANGLE BENT. REMOVED AND REPLACED IAW SRM 51-31-01 AT MAE.
- [SDR 04FDEA01880](https://openairdocs.org/sdr/04FDEA01880), Jun 29, 2004: DOUBLER. GOUGED. NR 3 ENG PYLON AFT UPPER FAIRING ANGLES LT AND RT GOUGED AND CHAFED AT AFT FASTENER HOLES. REMOVED AND REPLACED WORN ANGLES LT AND RT IAW SRM 51-35-01 AT MAE.
- [SDR 04FDEA01878](https://openairdocs.org/sdr/04FDEA01878), Jun 29, 2004: VANE. CORRODED. COMPLY WITH EA 8-5750-78235 WINGS OUTBOARD FLAP ARC 1537 FLAP VANE SUPPORT CORROSION REWORK. COMPLIED WITH EA 8-5750-78235 WINGS O/B FLAP ARC1537 FLAP VANE SUPP
- [SDR 04FDEA01870](https://openairdocs.org/sdr/04FDEA01870), Jun 28, 2004: RIB. GOUGED. ACCOMPLISH EA 8-5710-78226, WINGS REWORK OF GOUGES IN WING LEADING EDGE RIB ARB1086-1. COMPLIED WITH EA 8-5710-78226.
- [SDR 04FDEA01843](https://openairdocs.org/sdr/04FDEA01843), Jun 22, 2004: RIB. GOUGED. LT FIXED LEADING EDGE SLAT TRACK RIB GAUGE REPAIR XOS 427.4. COMPLIED WITH FED EX EA 8-5740-79537, LT FIXED LEADING EDGE SLAT TRACK RIB GOUGE REPAIR XOS 477.41.
- [SDR 04FDEA01841](https://openairdocs.org/sdr/04FDEA01841), Jun 21, 2004: DUCT. BROKEN. COMPLY WITH EA 8-2150-78236, AIR CONDITIONING NR 2 AC PACK EXHAUST DUCT STIFFENER REPAIR P/N-ACM7019. COMPLIED WITH EA 8-2150-78236 FOR STIFFENER REPAIR.
- [SDR 04FDEA01803](https://openairdocs.org/sdr/04FDEA01803), Jun 19, 2004: FITTING. CORRODED. RIGHT I/B FLAP SIDE LOAD ROLLER FITTING 3 EA ROLLER BORES AND FACES CORRODED. SIDE LOAD FITTING REMOVED AND REPLACED WITH NEW FITTING IAW CMM 57-55-22 AT MAE.

All 64: https://openairdocs.org/deregistered/N387FE-2024-04-13/reports.md

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