# N314FE: 1988 Mcdonnell Douglas MD-10-30F, registration cancelled 2013-07-09 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: July 9, 2013 - Exported to: Bolivia - Status when cancelled: Valid registration - Airframe: [Mcdonnell Douglas MD-10-30F](https://openairdocs.org/model/mcdonnell-douglas-md-10-30f) (registry code 3024020) - Engine: [GE CF6-50C2](https://openairdocs.org/engine/ge-cf6-50c2) (registry code 30085) - Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs) - Serial number: 48312 - Year built: 1988 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 23, 2009 - Certificate issued: September 6, 1988 - Last registry action: June 20, 2012 - Mode S code: A3562F - Owner when cancelled: [Wilmington Trust Company Trustee](https://openairdocs.org/faa-owner/WILMINGTON%20TRUST%20COMPANY%20TRUSTEE) - Location: [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington) - Owner type: Corporation - Owner's area on the map: 39.7357° N, 75.5321° W: Placed by OpenAirDocs: center of Wilmington, DE, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft was based - The mark today: https://openairdocs.org/aircraft/N314FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=314FE - Page: https://openairdocs.org/deregistered/N314FE-2013-07-09 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-10-30F: https://openairdocs.org/model/mcdonnell-douglas-md-10-30f.md ## Service difficulty reports (45) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FDEA201203020739](https://openairdocs.org/sdr/FDEA201203020739), Mar 2, 2012: ANTI-ICE VALVE. FAILED. ON CLIMB OUT, RECEIVED LT WING ANTI-ICE DISAGREE. WING ANTI-ICE WAS CYCLED OFF-ON BUT SAME RESULT. TRIED A SECOND ON-OFF CYCLE AND SAME RESULT. ALSO RECEIVED NR - [SDR FDEA201203020738](https://openairdocs.org/sdr/FDEA201203020738), Mar 2, 2012: ANTI-ICE VALVE. FAILED. ON CLIMB OUT, RECEIVED LEFT WING ANTI-ICE DISAGREE. WING ANTI-ICE WAS CYCLED OFF-ON BUT SAME RESULT. TRIED A SECOND ON-OFF CYCLE AND SAME RESULT. ALSO RECEIVED - [SDR FDEA201109093812](https://openairdocs.org/sdr/FDEA201109093812), Sep 9, 2011: SUPPORT FITTING. CRACKED. MAIN CARGO DOOR FRAME, CENTERING GUIDE, LOWER AFT SUPPORT FITTING CRACKED. FABRICATED & INSTALLED SUPPORT FITTING. - [SDR FDEA201101070067](https://openairdocs.org/sdr/FDEA201101070067), Jan 7, 2011: STATIC INVERTER. INOPERATIVE. EMERGENCY POWER TEST FAIL. TROUBLESHOT IAW FIM 24-24-00 FAULT D. FOUND STATIC INVERTER BAD. R & R STATIC INVERTER IAW AMM 24-24-01-2, OK FOR SERVICE. - [SDR FDEA201005121519](https://openairdocs.org/sdr/FDEA201005121519), May 12, 2010: WIRE HARNESS. DAMAGED. ON CLIMB OUT OF ANC - NR3 ENGINE EGT GAGE FLUCTUATED WILDLY OUT OF 20,000 FT HIT 1020 GOT "ENG 3 EXCEEDANCE ALL ENG 3 OIL, TEM, PRESSURE SHOWED NORMAL DUMPED FU - [SDR FDEA201003040649](https://openairdocs.org/sdr/FDEA201003040649), Mar 4, 2010: WARNING LIGHT. ILLUMINATED. AT CRUISE ALTITUDE 350, RECEIVED LEVEL 3 ALERT "AIR MANF 2 FAIL" COMPLIED WITH QRH AND PROCEEDED TO NEAREST SUITABLE KOKC FOUND SYSTEM TEST GOOD PER AMM 36-23-0 - [SDR FDEA201002230494](https://openairdocs.org/sdr/FDEA201002230494), Feb 23, 2010: CLAMP. LOOSE. BASED ON MX REPORT, DECIDED TO GIVE A LITTLE EXTRA TIME FOR ACCELERATION . IT WAS NECESSARY TO GO FULL QUADRANT TO GET CLOSE TO TAKEOFF POWER. WHEN THE AUTOFLIG - [SDR FDEA201001080044](https://openairdocs.org/sdr/FDEA201001080044), Jan 8, 2010: THROTTLE. MALFUNCTIONED. AFTER TAKEOFF, DURING CLEAN-UP, THROTTLES WOULD CONTINUOUSLY RETARD DUE TO AN UPPER FOOT ON THE PFD LOWERING BELOW PRESENT AIRSPEED. EVEN WITH AUTO THROTTLES OF - [SDR FDEA200911143954](https://openairdocs.org/sdr/FDEA200911143954), Nov 14, 2009: SPAR CAP. CRACKED. LT HORIZ STABILIZER L/E, FOUND 1EA CRACK 1,5" LONG ON UPPER FRONT SPAR CAP AT XE 115 REPAIRED IAW SRM 55-20-00 VOL 1, FIG9. - [SDR FDEA200910063482](https://openairdocs.org/sdr/FDEA200910063482), Oct 6, 2009: SKIN. DENTED. DURING INSP EXT FUSELAGE LWR SURFACE FOUND 1 EA DENT ON SKIN OF CTR CARGO DOOR 4"X2" DEEP .120". REPAIRED DENT IAW SRM 52-10-00, FIG 6, VOL I. - [SDR FDEA200909233370](https://openairdocs.org/sdr/FDEA200909233370), Sep 23, 2009: SKIN. DENTED. RT WING INBD FLAP UPPER SKIN FOUND DEEP DENT AND OIL CANING 2.50 INCH X 1.50 INCH DEEP .055 INCH. REPAIRED AREA IAW SRM 57-10-00 FIG 85 SHT 1-4 VOL I. - [SDR FDEA200908313170](https://openairdocs.org/sdr/FDEA200908313170), Aug 31, 2009: DOOR FRAME. CORRODED. INSPECTED UPPER CARGO DOOR JAMB STRUCTURE CORROSION ON UPPER DOOR JAMB. ACCOMPLISHED EA NR 8-5310-129649. - [SDR FDEA200908102964](https://openairdocs.org/sdr/FDEA200908102964), Aug 10, 2009: CHANNEL. CORRODED. CTR CARGO COMPT REF EO 8-2550-7-2354 P2 STEP "E1" AFTER REMOVAL PARTS FOUND DEEP CORROSION ON CHANNEL. REPAIRED AREA IAW SRM 53-70-00 FIG 7 SHT 5 VOL I. - [SDR FDEA200907282794](https://openairdocs.org/sdr/FDEA200907282794), Jul 28, 2009: SKIN. CRACKED. LT WING L/E FOUND CRACKED ON LOWER EXT SKIN L/E. REPAIRED AREA IAW SRM 57-10-00 FIG 68 SHT 2 VOL I. - [SDR FDEA200907282793](https://openairdocs.org/sdr/FDEA200907282793), Jul 28, 2009: SKIN. CRACKED. LT WING EXT STRUCTURE FOUND CRACKED ON LWR EXT SKIN L/E SLAT NR 4. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 & SRM 57-10-00 FIG 43 VOL I. - [SDR FDEA200907202671](https://openairdocs.org/sdr/FDEA200907202671), Jul 20, 2009: BEAM. CRACKED. CTR CARGO BILGE INSP FOUND CRACK ON BEAM. REPAIRED AREA IAW SRM 53-00-01 FIG 9 SHT 9 VOL I. - [SDR FDEA200907202670](https://openairdocs.org/sdr/FDEA200907202670), Jul 20, 2009: HINGE. NICKED. LT WING INBD FLAP FOUND ON OUTBD HINGE "ON WING" INBD SIDE DEEP NICKS. REPAIRED AREA IAW SRM 57-20-00 FIG 17 SHT 1 VOL I. - [SDR FDEA200907202668](https://openairdocs.org/sdr/FDEA200907202668), Jul 20, 2009: ANGLE. CRACKED. UPPER INT. FUSELAGE COMPT "ZONE 312" DURING REPAIR ASSESSMENT WITH EO 8-5100-7- 5001-P2. FOUND CRACK ON ANGLE UPPER SIDE AFT VERTICAL BULKHEAD. REPAIRED CRACK I - [SDR FDEA200907132601](https://openairdocs.org/sdr/FDEA200907132601), Jul 13, 2009: SKIN. CRACKED. RT WING EXT SURFACE FOUND CRACK ON UPPER EXT SKIN OTBD FLAP. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 VOL I. - [SDR FDEA200907112584](https://openairdocs.org/sdr/FDEA200907112584), Jul 11, 2009: SKIN. DENTED. LT WING EXT FOUND 2 EA DENTS ON INBD FLAP LOWER EXT. SKIN LWR PNL. 1): 0.75 INCH X 0.50 INCH MAX DEEP 0.070 INCH. 2): 0.50 INCH X 0.50 INCH MAX DEEP 0.060 INCH. - [SDR FDEA200907112583](https://openairdocs.org/sdr/FDEA200907112583), Jul 11, 2009: SKIN. DENTED. LT WING EXT FOUND 1 EA DENT .75 INCH X 1 INCH MAX DEEP .060 INCH ON INBD FLAP LWR EXT. SKIN LWR PANEL. REPAIRED AREA IAW SRM 57-00-01 FIG 4 SHT 2 VOL I. - [SDR FDEA200907012435](https://openairdocs.org/sdr/FDEA200907012435), Jul 1, 2009: SKIN. LOOSE. RT WING EXT SURFACE FOUND NR 180 EA LOOSE FASTENERS ON UPPER EXT SKIN OUTBD FLAP. REPAIRED SKIN IAW SRM 57-10-00 FIG 85 & SRM 57-20-00 FIG 2 VOL I. - [SDR FDEA200906262319](https://openairdocs.org/sdr/FDEA200906262319), Jun 26, 2009: SKIN. CRACKED. RT WING LWR EXT SURFACE FOUND CRACKS AND NR 100 EA LOOSE FASTENERS ON LWR EXT SKIN OTBD FLAP. REPAIRED AREA IAW SRM 57-10-00 FIG 7, SHT 3, VOL I. - [SDR FDEA200906262318](https://openairdocs.org/sdr/FDEA200906262318), Jun 26, 2009: FRAME. WORN. DURING INSP LT AIR COND FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4 & 4A VOL I. - [SDR FDEA200906262317](https://openairdocs.org/sdr/FDEA200906262317), Jun 26, 2009: FRAME. CRACKED. DURING INSPECTION LT AIR COND FOUND CRACK ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4 VOL I. - [SDR FDEA200906262316](https://openairdocs.org/sdr/FDEA200906262316), Jun 26, 2009: FRAME. WORN. DURING INSP AVIONIC COMPT BILGE AREA FOUND DEEP WEAR ON FRAME. REPAIRED AREA IAW SRM 53-30-00 FIG 4, VOL I. - [SDR FDEA200906232239](https://openairdocs.org/sdr/FDEA200906232239), Jun 23, 2009: MEMBRANE. CRACKED. AFTER REMOVAL PANELS ON FLIGHT COMPT WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. REPAIRED MEMBRANE IAW SRM 53-00-01 FIG 4 SHT 2 VOL I. - [SDR FDEA200906232238](https://openairdocs.org/sdr/FDEA200906232238), Jun 23, 2009: MEMBRANE. CRACKED. AFTER REMOVAL PANELS ON FLIGHT COMPT WITH OAN J/C 0600C210-1JR FOUND CRACK ON MEMBRANE. REPAIRED MEMBRANE IAW SRM 53-00-01, FIG 4, SHT 2, VOL I. - [SDR FDEA200906122044](https://openairdocs.org/sdr/FDEA200906122044), Jun 12, 2009: SKIN. CRACKED. DURING INSP OF COSTANT SECTION STB, FOUND UP PANEL, INSP POSITION 3, WITH CRACK IN FLYABLE LIMITS, ACCOMPLISHED EA NR 8-5510-129688. - [SDR 08FDEA03885](https://openairdocs.org/sdr/08FDEA03885), Sep 15, 2008: LINE. LEAKING. CENTER GEAR FAILED TO EXTEND WITH GEAR HANDLE. RAN CHECK LIST, CENTER GEAR EXTENDED WHEN THE CENTER GEAR ALTERNATE EXTENSION HANDLE WAS PULLED. ON LANDING ROLLO - [SDR FDEA200807182982](https://openairdocs.org/sdr/FDEA200807182982), Jul 18, 2008: ENGINE. FAILED. DURING DEPARTURE NR 1 ENGINE HAD LOUD BANG AND VIBRATION. NR 1 ENG TO IDLE AND THEN OIL QUANTITY WENT TO ZERO, NO N1. PERFROMED PHASE 1'S AND QRH PROCEDURE. RET - [SDR 08FDEA02982](https://openairdocs.org/sdr/08FDEA02982), Jul 18, 2008: ENGINE. FAILED. DURING DEPARTURE NR 1 ENGINE HAD LOUD BANG AND VIBRATION. NR 1 ENG TO IDLE AND THEN OIL QUANTITY WENT TO ZERO, NO N1. PERFORMED PHASE 1'S AND QRH PROCEDURE. RET - [SDR 03FDEA00337](https://openairdocs.org/sdr/03FDEA00337), Mar 19, 2003: ANTI-ICE SYSTEM. INOPERATIVE. RIGHT WINDSHIELD ANTI/ICE INOPERATIVE LIGHT ILLUMINATED SHORTLY AFTER TAKE OFF. REMOVED AND REPLACED RIGHT WINDSHIELD IAW M.M. 56-11-00-2. REMOVED AND REPLACED - [SDR 02FDEA00383](https://openairdocs.org/sdr/02FDEA00383), Jun 6, 2002: TRANSMITTER. LEAKING. AFTER 2+15 OF FLT HYD SYS 3 ELEV OFF LIGHT ILLUMINATED. PERFORMED RED TABS, WITH FLUID DOWN TO 4.5 GALS. WHEN ENG 3 HYD PUMPS TURNED BACK ON, STARTED TO SLOWLY - [SDR 02FDEA00355](https://openairdocs.org/sdr/02FDEA00355), May 19, 2002: SEAL. SPLIT. HYD SYS 3 ELEV OFF LIGHT ILLUMINATED. PRESSURE WAS NORMAL, QTY ABOUT 4.5 GALS. RAN RED TABS. LANDED AT TJSJ. HYD LEAK CONFIRMED BY COMPANY MX AFTER LANDING. UPO - [SDR 02FDEA00219](https://openairdocs.org/sdr/02FDEA00219), Mar 26, 2002: PERISEAL. FAILED. AFTER T/O NR 3 PNEU MANIFOLD FAIL LIGHT ILLUMINATED. REMOVED AND REPLACED PERISEALS PER SMP. - [SDR 01FDEA00025](https://openairdocs.org/sdr/01FDEA00025), Jan 17, 2001: SENSOR. DAMAGED. AFT T/O AND LAND GEAR UP S/O PNL IND RED UNSAFE NOSE GEAR. RECYCLED LG AND NOSE RED UNSAFE LIGHT ON EXT AND RETRACTION. *S/D* REPLACED DAMAGED NOSE GEAR LOCKED - [SDR 00FDEA00782](https://openairdocs.org/sdr/00FDEA00782), Nov 19, 2000: TIRE. DISINTEGRATED. 00-317 NR 3 & 4 TIRE REQUIRES REPLACEMENT DUE TO DISINTEGRATION ON T/O OUT OF CDG. R&R NR 3, 4, 7, 8 TIRES, & DAMAGED PANELS 152PT, 152MT, 152NT, PER MM 20-21-0 - [SDR 00FDEA00729](https://openairdocs.org/sdr/00FDEA00729), Oct 21, 2000: CONTROLLER. MALFUNCTIONED. DURING CLIMB HAD UNCOMMANDED AUTO SLAT EXTENSION. - [SDR 00FDEA00307](https://openairdocs.org/sdr/00FDEA00307), May 1, 2000: VALVE. FAILED. LOUD BANG FROM REAR OF A/C PRESS BUMP FELT. REMOVED AND REPLACED AIR CONDITIONING SYS AIR CK VALVE IN REF TO AMM 21-22-03-2. OPS CK NORM. - [SDR 00FDEA0025](https://openairdocs.org/sdr/00FDEA0025), Jan 18, 2000: CONNECTOR. FAILED. NR 751 - RT W/W FWD INBD ELECT HYD PUMP CANNON PLUG WAS A SHORTED WIRE. PUMP HAD 2 EA SHORT WIRES CAUSING ELECTRICAL FIRE. - [SDR 00FDEA00025](https://openairdocs.org/sdr/00FDEA00025), Jan 18, 2000: CONNECTOR. FAILED. NR 751 - RT W/W FWD INBD ELECT HYD PUMP CANNON PLUG WAS A SHORTED WIRE. PUMP HAD 2 EA SHORT WIRES CAUSING ELECTRICAL FIRE. REPLACED WIRE HARNESS, PLUG CONNECTOR - [SDR 99FDEA00013](https://openairdocs.org/sdr/99FDEA00013), Jan 14, 1999: TRANSMITTER. FAILED. 99-0013 - ON T/O FLAP LIMIT CHANNEL INOP AND SELECT FLAP LIMIT OVERRIDE LIGHT ILL IN READ 10 DEG LT SIDE AND 4 DEG RT SIDE. FOUND LT OTBD FLAP POS TRANSMITTER B - [SDR 98FDEA00692](https://openairdocs.org/sdr/98FDEA00692), Nov 10, 1998: TEMP GAUGE. INOP. NR 3 HYDRAULIC TEMP HAD SLOWLY INCREASED IN TEMP AFTER T/O. TEMP 108C, NO TEMP LIGHT, PRESS TO TEST WAS OK. REMOVED AND REPLACED HYDRAULIC GAUGE AFTER TROUBLESH - [SDR 97FDEA00907](https://openairdocs.org/sdr/97FDEA00907), Dec 19, 1997: CONTROL UNIT. FAILED. 97-0260 - ON T/O CTR AND RT GEAR RED LIGHTS WERE SLOW TO EXTINGUISH, LEFT GEAR LIGHT WENT FROM EXTINQUISHED TO RED RECYCLE GEAR AND ALL LIGHTS EXTINGUISHED. ON --- 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.