# N394FE: 1975 Mcdonnell Douglas MD-10-10F, registration cancelled 2024-03-02

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 2, 2024
- Status when cancelled: Valid registration
- 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: 46628
- Year built: 1975
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 18, 2003
- Certificate issued: September 6, 2001
- Last registry action: May 12, 2023
- Mode S code: A49227
- Owner when cancelled: [Federal Express Corp](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORP)
- 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/N394FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=394FE
- Page: https://openairdocs.org/deregistered/N394FE-2024-03-02

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 (99, newest 50)

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

- [SDR FDEA2020031760571](https://openairdocs.org/sdr/FDEA2020031760571), Mar 16, 2020: CONTROL UNIT. MALFUNCTIONED. PDIS 394 27-50 4766 15MAR20 MEM FACT U LOGPAGES:3200325 DECLARED EMERGENCY. UNRESPONSIVE FLAPS. UNABLE TO SELECT FLAPS BEYOND SLATS EXTENDED. USED DIAL-A-FLAP T
- [SDR FDEA2020031760570](https://openairdocs.org/sdr/FDEA2020031760570), Mar 16, 2020: UNKNOWN. MALFUNCTIONED. PDIS 394 27-50 4765 15MAR20 MEM FACT U DURING APPROACH REQUESTED "FLAPS 15", FO TRIED SELECTING FLAPS 15 UNSUCCESSFULLY. WE USED THE DIAL-A-FLAP TO SELECT FLAPS
- [SDR FDEA201910312811](https://openairdocs.org/sdr/FDEA201910312811), Oct 31, 2019: SKIN. CRACKED. LH WING OUTBOARD FLAP UPPER SURFACE SKIN HAS TWO CRACKS LOCATED AT THE INBOARD HINGE AREA 0000608631 : F - 01-NOV-2019 01:12 REPAIRED REF MD10 SRM 57-10-00 TRAC
- [SDR FDEA201906301440](https://openairdocs.org/sdr/FDEA201906301440), Jun 30, 2019: WARNING SYSTEM. FALSE ACTIVATION. AFTER LANDING ROLLOUT, THE LEVEL 1 BRAKE DIFF TEMP ALERTED, FOLLOWED BY THE LEVEL II (2) BRAKE OVERHEAT. BRAKES 5 & 6 PEAKED AT APPROX 600, BRAKES 1 & 2 PEAKED 
- [SDR FDEA201812183534](https://openairdocs.org/sdr/FDEA201812183534), Dec 18, 2018: PROBE. OUT OF LIMITS. PDIS 394 28-40 3649 18DEC18 BNA OPEN U LOGPAGES:2876587 NR 2 FUEL QUANTITY DECREASED DISPROPORTIONATELY WITH NR 1 & NR 3 TANKS. POSSIBLE FUEL LEAK, OR SENSOR MA
- [SDR FDEA201810172932](https://openairdocs.org/sdr/FDEA201810172932), Oct 17, 2018: CAP. DAMAGED. RT WING REAR UPPER SPAR AREA, APPROX XORS 402, INSIDE FUEL TANK UPPER RIB CAP HAS SMALL AREA OF DAMAGE. REPAIRED PER EA 8-5710-T0342036 PART 1.
- [SDR FDEA201808292262](https://openairdocs.org/sdr/FDEA201808292262), Aug 29, 2018: RIB. DAMAGED. RIGHT WING, REAR UPPER SPAR AREA, XORS 402, INSIDE FUEL TANK UPPER RIB CAP HAD A SMALL AREA OF DAMAGE. REPAIRED IAW EA 8-5710-T0342036.
- [SDR FDEA201807121688](https://openairdocs.org/sdr/FDEA201807121688), Jul 12, 2018: REPAIR. DAMAGED. LT I/B FLAP VANE, I/B END HAS A DAMAGED REPAIR ON TOP SKIN. REPAIRED DAMAGE ON LT I/B FLAP VANE, I/B END TOP SIDE, IAW SRM 51-71-00 VOL 2, PAR 16.
- [SDR FDEA2018062981593](https://openairdocs.org/sdr/FDEA2018062981593), Jun 28, 2018: SKIN. DAMAGED. RT DETACHABLE ELEVATOR HAD DAMAGE ON THE TOP INBD EDGE. REMOVED AND REPLACED THE SKIN IAW SRM 55-10-00, VOL 1, FIG 7, AND SRM 51-31-01, VOL 2.
- [SDR FDEA201805311403](https://openairdocs.org/sdr/FDEA201805311403), May 31, 2018: SPAR. DAMAGED. RT WING LOWER REAR SPAR REQUIRES SR10570049-60 REPAIR. PART TO BE FABRICATED PER EA 8-5710-T034000.
- [SDR FDEA201805311402](https://openairdocs.org/sdr/FDEA201805311402), May 31, 2018: SPAR. DAMAGED. RT WING LOWER REAR SPAR REQUIRES (2) SR10570048-38 REPAIR. PART TO BE FABRICATED PER EA 8-5710-T034000. REPAIRED PER ES 8-5710-T0340000.
- [SDR FDEA201805311401](https://openairdocs.org/sdr/FDEA201805311401), May 31, 2018: SPAR. DAMAGED. RT WING LOWER REAR SPAR REQUIRES SR10570048-6 REPAIR. PART TO BE FABRICATED PER EA 8-5710-T034000. REPAIRED PER EA 8-5710-T0340000.
- [SDR FDEA201805221371](https://openairdocs.org/sdr/FDEA201805221371), May 22, 2018: FLAP SYSTEM. CRACKED. REWORK REF N/R N00460 "LH WING ATTACH FITTING FOR O/B FLAP I/B HINGE HAS A .5 IN. CRACK ON THE O/B HALF AT THE FWD FASTENER. (MRKD)" REWORK PER QA REVIEW REJECT
- [SDR FDEA201805221447](https://openairdocs.org/sdr/FDEA201805221447), May 22, 2018: FRAME. CORRODED. CTR CARGO COMPT STA 1741 FRAME HAS CORROSION BY LONG 52. REMOVED AND REPLACED A SECTION OF CORRODED FRAME (CHANNEL) AT STA 1741 AT LONGERON 52 REF SRM 53-30-00 
- [SDR FDEA201804301147](https://openairdocs.org/sdr/FDEA201804301147), Apr 30, 2018: FITTING. CORRODED. RIGHT WING OTBD FLAP, OTBD HINGE, SIDE LOAD FITTING ON THE AIRCRAFT SIDE, FOUND CORRODED AT THE FASTENER HOLES. REMOVED THE CORROSION. REMOVED AND REPLACED THE 
- [SDR FDEA2018042601118](https://openairdocs.org/sdr/FDEA2018042601118), Apr 25, 2018: SEAT TRACK. DAMAGED. UPPER MAIN CARGO DECK LT SIDE, UNDER A BALLMAT AT BS 800, LBL 48 SEAT TRACK LOBE DAMAGED. REPAIRED THE SEAT TRACK IAW SRM 53-70-00, FIG 1, VOL 1.
- [SDR FDEA2018042601113](https://openairdocs.org/sdr/FDEA2018042601113), Apr 25, 2018: SKIN. CORRODED. LEFT UPPER WING SKIN HAS CORROSION AT FASTENER, XORS 423. AFT OF FRONT SPAR. REPAIRED IAW EA 8-5730-T0339577-P1. REPAIR CLASSIFIED AS MINOR.
- [SDR FDEA2018043001136](https://openairdocs.org/sdr/FDEA2018043001136), Apr 23, 2018: RIB. CRACKED. RIGHT WING L/E ACCESS PANEL 619DB, INSIDE UPPER RIB FLANGE IS CRACKED ABOVE PULLEY OTBD OF THE NR 10 SLAT TRACK.
- [SDR FDEA201804231101](https://openairdocs.org/sdr/FDEA201804231101), Apr 23, 2018: SKIN. DELAMINATED. LEFT WING NR 3 SPOILER TOP SKIN HAS MULTIPLE AREAS OF DELAMINATION. REPAIRED IAW SRM 51-71-00, VOL II, PAR 16.
- [SDR FDEA201804191139](https://openairdocs.org/sdr/FDEA201804191139), Apr 19, 2018: SHEAR TIE. CORRODED. AFT CARGO BAY, BS 1950, CORROSION ON THE FRAME SHEAR TIE BETWEEN LONGERONS 51 AND 52R. REPAIRED THE SHEAR TIE IAW SRM 53-30-00, PG 2, FIG 10, VOL 1.
- [SDR FDEA2018062981594](https://openairdocs.org/sdr/FDEA2018062981594), Apr 18, 2018: SKIN. DAMAGED. RT DETACHABLE ELEVATOR HAD DAMAGE ON THE TOP INBD EDGE. REMOVED AND REPLACED THE SKIN IAW SRM 55-10-00, VOL I, FIG 7, SRM 51-31-01, VOL II.
- [SDR FDEA201804111067](https://openairdocs.org/sdr/FDEA201804111067), Apr 11, 2018: BEAM. CRACKED. L3 DOOR, NR 1 BEAM AFT SIDE AT THE DOOR FRAME STOP WAS FOUND CRACKED. REMOVED AND REPLACED THE BEAM IAW DWG ADA 0006, AND SRM 51-31-01.
- [SDR FDEA2018042601128](https://openairdocs.org/sdr/FDEA2018042601128), Apr 9, 2018: BULKHEAD WEB. CRACKED. BS 595 BULKHEAD, RT FWD SIDE OF WEB HAS A 1 INCH CRACK THRU FASTENER HOLE AT RBL 60, Z100.00. PERFORMED A BULKHEAD REPAIR IAW SRM 53-40-00, FIG 25 V1.
- [SDR FDEA201804021245](https://openairdocs.org/sdr/FDEA201804021245), Apr 2, 2018: SPAR CAP. CRACKED. RT WING REAR SPAR LOWER CAP AT XORS 446 HAS A 2.0 INCH CRACK AT THE AFT EDGE OF TEE CAP EXTENDING THROUGH THE RADIUS AND TERMINATING 1.0 IN UP THE VERTICAL LEG.
- [SDR FDEA201804011123](https://openairdocs.org/sdr/FDEA201804011123), Apr 1, 2018: FRAME. CORRODED. CENTER CARGO BAY BS 1741 FRAME HAS CORROSION BY LONGERON 52. REPAIRED THE CORRODED FRAMED IAW SRM 53-30-00, VOL I, PAGE 31.
- [SDR FDEA201803280901](https://openairdocs.org/sdr/FDEA201803280901), Mar 28, 2018: WEB. CRACKED. NOSE LANDING GEAR WW, RT SIDE FWD OF INNER WEB, BS 495, Z-65. CRACKED FROM FASTENER HOLES. REPAIRED IAW SRM 53-30-00, FIG 6, SH 8, VOL I. MAJOR REPAIR.
- [SDR FDEA201803271246](https://openairdocs.org/sdr/FDEA201803271246), Mar 27, 2018: SPAR CAP. CRACKED. RT WING REAR SPAR LOWER CAP AT XORS 421 HAS A .200 INCH CRACK PROPAGATING FWD OF A PREVIOUS TRIM OUT REPAIR AND EXTENDING INTO THE RADIUS. REPAIRED PER EA 8-571
- [SDR FDEA201803270974](https://openairdocs.org/sdr/FDEA201803270974), Mar 27, 2018: SKIN. CRACKED. RT WING SKIN AT THE INBOARD UPPER CORNER OF THE SLAT ANTI-ICE DUCT CUT OUT HAS A .500 INCH CRACK PROPAGATING THROUGH AN EXISTING STOP DRILL. INSTALLED A REPAIR 
- [SDR FDEA201803270791](https://openairdocs.org/sdr/FDEA201803270791), Mar 27, 2018: CARGO TRACK. DAMAGED. MAIN CARGO TRACK BS 635 RBL 27.5 DAMAGED BEYOND LIMITS. REPAIRED THE TRACK IAW SRM 53-70-00, FIG 1, VOL 1.
- [SDR FDEA201803270790](https://openairdocs.org/sdr/FDEA201803270790), Mar 27, 2018: CARGO TRACK. GOUGED. MAIN CARGO TRACK BS 879, RBL 8.5 GOUGED OUT OF LIMITS. REPLACED THE CARGO TRACK SRM 53-70-00, FIG 1, VOL 1.
- [SDR FDEA201803270788](https://openairdocs.org/sdr/FDEA201803270788), Mar 27, 2018: CARGO TRACK. WORN. MAIN CARGO BAY, BS 859, LBL 107.25 SEAT TRACK IS WORN OUT OF LIMITS. REPAIRED SEAT TRACK IAW SRM 53-70-00, FIG 1.
- [SDR FDEA201803261127](https://openairdocs.org/sdr/FDEA201803261127), Mar 26, 2018: CAP. CRACKED. RIGHT BS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43R HAS A .100 INCH CRACK THROUGH THE LOWER FASTENER HOLE. PERFORMED A TEE CAP REPAIR IAW DWG SR10530064.
- [SDR FDEA201803261112](https://openairdocs.org/sdr/FDEA201803261112), Mar 26, 2018: CAP. CRACKED. LEFT BS 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 41L HAS A 1 INCH CRACK THROUGH THE LOWER FASTENER HOLE. REPAIIRED THE TEE CAP IAW EA 8- 5310-T0339305 P1/P
- [SDR FDEA201803160722](https://openairdocs.org/sdr/FDEA201803160722), Mar 16, 2018: SENSOR. OUT OF ADJUST. AFTER SELECTING FLAPS 35 ON FINAL AT ORD GOT SLAT DISAGREE ALERT. DUE TO TIME LAG BETWEEN SELECTING FINAL FLAPS AND ALERT ELECTED, A SECOND APPROACH IN NORMAL C
- [SDR FDEA201708152224](https://openairdocs.org/sdr/FDEA201708152224), Aug 15, 2017: LEVER. BINDING. R1 ARMING LEVER VERY DIFFICULT TO MOVE, FEELS LIKE CABLE IS STRETCHING RATHER THAN PARTS ARE MOVING.
- [SDR FDEA201708052122](https://openairdocs.org/sdr/FDEA201708052122), Aug 5, 2017: WIRE HARNESS. DAMAGED. DURING CLIMBOUT, NOTICED THE NR 2 ENGINE EXCEEDENCE LEVEL 1 ALERT. EGT GAUGE FOR NR 2 SHOWED MAX 998. NORMAL EGT AT REDUCED POWER FOR LEVEL FLIGHT AT 7000 FT. O
- [SDR FDEA201609263369](https://openairdocs.org/sdr/FDEA201609263369), Sep 26, 2016: SEAT TRACK. DAMAGED. SEAT TRACK FOUND DAMAGED BS 1388 RBL 75.25. REPAIRED IAW SRM 53-70-00.
- [SDR FDEA201609213367](https://openairdocs.org/sdr/FDEA201609213367), Sep 21, 2016: SEAT TRACK. DAMAGED. REPORTS A LOCK AT STA 1400, LOCK IN MAIN DECK CARGO IS NOT SECURE. PRIOR TO DEPARTURE, DISCOVERED SEAT TRACK DAMAGED WHERE LOCK IS LOCATED. NO DAMAGE TO LOCK WA
- [SDR FDEA201605011439](https://openairdocs.org/sdr/FDEA201605011439), May 1, 2016: LONGERON. CORRODED. CENTER CARGO AREA LT SIDE AT BS 1781, STRINGER 43L HAS CORROSION. R & R THE LONGERON END CAP IAW SRM 51-31-01 VOL 2. FABRICATED NEW LONGERON END CAP ON T16 1202
- [SDR FDEA201605011438](https://openairdocs.org/sdr/FDEA201605011438), May 1, 2016: SKIN. CORRODED. TOP SURFACE OF CTR WING TANK AT STATION 1224, LBL 90 - 105 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-01 VOL II FOUND TO BE OUT OF LIMITS IAW SRM 57-20-00 F
- [SDR FDEA201605011437](https://openairdocs.org/sdr/FDEA201605011437), May 1, 2016: SKIN. CORRODED. CENTER WING UPPER SKIN AT STATION 1297, LBL 84 HAS CORROSION. REMOVED CORROSION IAW SRM 51-21-01 VOL 2, FOUND TO BE OUT OF LIMITS IAW SRM 57-20-00 FIG 8A VOL 1.
- [SDR FDEA201604281424](https://openairdocs.org/sdr/FDEA201604281424), Apr 28, 2016: SKIN. CORRODED. CENTER WING UPPER SKIN AT 1298, LBL 95, HAS CORROSION. REMOVED 6 EACH FASTENERS IAW SRM 51-30-01, VOL 2. REMOVED CORROSION IAW SRM 51-21-01 VOL 2. CHECKED LIMIT
- [SDR FDEA201604281423](https://openairdocs.org/sdr/FDEA201604281423), Apr 28, 2016: SKIN. DENTED. TWO EACH DENTS ON UPPER FUSELAGE, EXTERNAL SURFACE AT FS 401, CLOSE TO L1 DOOR. COMPLIED WITH EA. 8-5330-T0324851 PT 1, DENTS AT FS 401 FWD OF L1 DOOR. APPLIED 
- [SDR FDEA201604271389](https://openairdocs.org/sdr/FDEA201604271389), Apr 27, 2016: FLOORBEAM. CRACKED. FLOORBEAM CRACKED AT STATION 1801, LBL 54 AT AFT CARGO DOOR CUT OUT. REPAIRED FLOORBEAM IAW SRM 53-60-01 FIG 3 VOL 1. MAJOR REPAIR.
- [SDR FDEA201604211331](https://openairdocs.org/sdr/FDEA201604211331), Apr 21, 2016: FLOOR PANEL. DAMAGED. MAIN DECK AREA STATION 775, BL 0 FLOOR PANEL PUNCTURE. FABRICATED REPLACEMENT PANEL ON T16 1202347 IAW DWG SRZ-25-005. R & R FLOOR PANEL IAW 53-21-08-04, MAJOR 
- [SDR FDEA201604151231](https://openairdocs.org/sdr/FDEA201604151231), Apr 15, 2016: SEAT TRACK. GOUGED. GOUGES & MINOR DAMAGES ON SEAT TRACK SCALLOPS AT MAIN DECK CARGO COMPARTMENT, LBL 8.5 LT, BETWEEN FS 1521 & 1621. R & R SEAT TRACK AT LBL 8.5, FROM STATION 1531
- [SDR FDEA201604131203](https://openairdocs.org/sdr/FDEA201604131203), Apr 13, 2016: FLOORBEAM. CRACKED. FLOORBEAM AT STATION 1821, HAS A CRACK AT LBL 54, INBD OF AFT CARGO DOOR CUT OUT. REPAIRED FLOORBEAM AT STATION 1821, LBL 54 IAW SRM 53-60-01 FIG 3 VOL 1 MAJOR 
- [SDR FDEA201604101182](https://openairdocs.org/sdr/FDEA201604101182), Apr 10, 2016: STRAP. DEFECTIVE. BOTH THE CAPTAIN & FIRST OFFICER ESCAPE STRAPS DO NOT REACH THE GND, AS REQUIRED BY STEPS 2 B 3 & 3 B 3 OF WC 25C6503. R & R CAPTAINS & FIRST OFFICERS ESCAPE ST
- [SDR FDEA201512294101](https://openairdocs.org/sdr/FDEA201512294101), Dec 29, 2015: LIGHT. INOPERATIVE. R1 DOOR PNEUMATIC PSI TEST FAILED. RELAMPED WITH CORRECT LIGHT BULBS. OPERATIONS CHECKED NORMAL IAW AMM 25-61-03-5-0.
- [SDR FDEA201502240591](https://openairdocs.org/sdr/FDEA201502240591), Feb 24, 2015: SWITCH. INTERMITTENT. LEFT ENTRY DOOR FAILS TO MOVE UP OR DOWN, STUCK IN MID POSITION. DOOR SWITCH INTERMITTENT INTERIOR & EXTERIOR. REPLACED OPEN/CLOSE SOLENOID. ADJUST AND TEST CHE

All 99: https://openairdocs.org/deregistered/N394FE-2024-03-02/reports.md

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