# N564FE: 1978 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 CF6-6D](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: 46984
- Year built: 1978
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 22, 2009
- Certificate issued: March 21, 2003
- Last registry action: September 22, 2023
- Mode S code: A73648
- 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/N564FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=564FE
- Page: https://openairdocs.org/deregistered/N564FE-2024-03-02

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 (106, newest 50)

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

- [SDR FDEA201607162482](https://openairdocs.org/sdr/FDEA201607162482), Jul 16, 2016: ENGINE. FAILED. UPON ADVANCING POWER FOR TAKEOFF, FELT A RUMBLING IN THE RUDDER PEDALS. ABORTED T/O AT AT 10 KTS. TURNED OFF RUNWAY, ANOTHER ACFT ADVISED SEEING FLAMES FROM THE
- [SDR FDEA201607032231](https://openairdocs.org/sdr/FDEA201607032231), Jul 3, 2016: FIRE WARNING. FALSE ACTIVATION. DURING PREFLIGHT, CARGO FIRE LOWER FWD, LEVEL 3 ALERT DISPLAYED. INVESTIGATED AND FOUND CARGO DOOR CLOSED. COMPLIED WITH QRH. R & R NR 105LB, LOWER CARGO COMPAR
- [SDR FDEA201511173654](https://openairdocs.org/sdr/FDEA201511173654), Nov 17, 2015: SENSOR. FAILED. AT 370 RECEIVED LEVEL 1 HIGH STAGE 3 OFF ALERT, FOLLOWED BY LEVEL 1 MANIFOLD 3 FAIL ALERT. PERFORMED QRH, RAN THROTTLE IN IDLE. REPLACED NR 2 ENG HIGH STAGE TEM
- [SDR FDEA201508082517](https://openairdocs.org/sdr/FDEA201508082517), Aug 8, 2015: SLIDING WINDOW. UNSECURE. REJECTED TAKEOFF, AIR NOISE FROM CAPTAIN`S WINDOW. CHECKED LATCH. LATCH APPEARED CLOSED & LOCKED. THE CAPTAIN PUSHED THE LOCKING ARM FWD ABOUT .750 ON HIS SLIDI
- [SDR FDEA201508062490](https://openairdocs.org/sdr/FDEA201508062490), Aug 6, 2015: UNKNOWN. MALFUNCTIONED. LEVEL 2 ENG 1 OIL FILTER ALERT DURING CLIMB PASSING FL 200. ALL OIL PRESS & TEMP INDICATIONS WERE NORMAL, NO VIBRATION. REDUCED THROTTLE TO IDLE. LEVEL 2 ALERT 
- [SDR FDEA201507112199](https://openairdocs.org/sdr/FDEA201507112199), Jul 11, 2015: SLIDE. BLOWN. R1 SLIDE BLOWN ON ARRIVAL. REMOVED DEPLOYED SLIDE & RAFT ASSEMBLY AS REQUIRED IAW AMM 25-61-07-4. RESET & SERVICED RI DOOR AIR RESERVOIR AS REQUIRED IAW AMM 51-
- [SDR FDEA201503100790](https://openairdocs.org/sdr/FDEA201503100790), Mar 10, 2015: WIRE. BROKEN. DURING CLIMB OUT APPROXIMATELY FIVE MINUTES AFTER TAKEOFF RECEIVED A LEVEL 2 BRAKE OVERHEAT ALERT. CONFIGURATION PAGE SHOWED LT TRUCK RT AFT TIRE TEMP, BRAKE NR
- [SDR FDEA201502260600](https://openairdocs.org/sdr/FDEA201502260600), Feb 26, 2015: ANTI-ICE SYSTEM. UNKNOWN. DURING DESCENT WITH ENGINE & WING ANTI - ICE ON INITIALLY RECEIVED A NR 3 MANIFOLD FAILURE LIGHT SELECTED. WING ANTI - ICE OFF, NR 3 MANIFOLD FAIL LIGHT REMAINE
- [SDR FDEA201501300390](https://openairdocs.org/sdr/FDEA201501300390), Jan 30, 2015: SWITCH. STUCK. RAMP CREW REPORTED THAT AFTER CLOSING L1 DOOR, IT WOULD NOT OPEN ELECTRICALLY. ON INSPECTION FOUND DOOR OPEN SWITCH PLUNGER STUCK IN THE OPEN POSITION. LUBED AN
- [SDR FDEA201409302871](https://openairdocs.org/sdr/FDEA201409302871), Sep 30, 2014: SUPPORT. CORRODED. RIGHT AFT BODY FAIRING AFT SUPPORT SHOWING EXFOLIATION CORROSION. REPAIRED IAW EA 8-5320-T0311923.
- [SDR FDEA201409262790](https://openairdocs.org/sdr/FDEA201409262790), Sep 26, 2014: SKIN. CORRODED. LEFT WING INBD AILERON UPPER SURFACE SHOWS CORROSION. LT INBD AILERON R & R IAW N00135 & MM 27-10-01-4.
- [SDR FDEA201409252786](https://openairdocs.org/sdr/FDEA201409252786), Sep 25, 2014: SKIN. WORN. RIGHT INBD FLAP VANE LE WORN. REPAIRED IAW SRM 51-71-00 VOL II.
- [SDR FDEA201409232742](https://openairdocs.org/sdr/FDEA201409232742), Sep 23, 2014: SKIN. GOUGED. LEFT WING NR 5 SLAT LOWER SURFACE HAS DEEP GOUGE BY NR 11 SLAT TRACK. REPAIRED IAW SRM 57-00-01 VOL1 FIG 4 SHEET 2.
- [SDR FDEA201409232737](https://openairdocs.org/sdr/FDEA201409232737), Sep 23, 2014: SKIN. DENTED. LEFT WING INBD FLAP VANE TOP SURFACE HAS SHARP DENT. REPAIRED IAW SRM 51-71-00 VOL 2.
- [SDR FDEA201409232735](https://openairdocs.org/sdr/FDEA201409232735), Sep 23, 2014: VANE. DELAMINATED. LEFT FLAP VANE LE INBD OF NR 3 TRACK HAS SMALL SECTION OF DELAMINATION. REPAIRED IAW SRM 51-71-00 VOL 2.
- [SDR FDEA201409222704](https://openairdocs.org/sdr/FDEA201409222704), Sep 22, 2014: SKIN. DAMAGED. RIGHT LOWER FLAP SURFACE SKIN HAS HAIL DAMAGE. FABRICATED DOUBLER IAW SRM 57-10-00 FIG 85 SHEET 2.
- [SDR FDEA201409222703](https://openairdocs.org/sdr/FDEA201409222703), Sep 22, 2014: DOUBLER. CRACKED. LEFT WING FIXED LE INNER SKIN DOUBLER HAS APPROX 10 INCH CRACK AT STATION XORS 570. INSTALLED .020 TITANIUM DOUBLER IAW SRM 57-10-00 FIG 71 VOL 1.
- [SDR FDEA201409192678](https://openairdocs.org/sdr/FDEA201409192678), Sep 19, 2014: SHEAR TIE. CORRODED. AFT CARGO COMPARTMENT AT STATION 1781, BULKHEAD TO SKIN SHEAR TIE HAS EXFOLIATION CORROSION AT L48R. R & R SHEAR TIE IAW 51-30-00 VII.
- [SDR FDEA201409082533](https://openairdocs.org/sdr/FDEA201409082533), Sep 8, 2014: FLOOR SUPPORT. CRACKED. LEFT CORNER OF FLOOR SUPPORT HAS A 1.25 INCH CRACK EMANATING FROM TOP FASTENER ON FRAME VERTICAL FWD FLANGE. PERFORMED REPAIR IAW SRM 53-30-00 FIG 7, VOL 1
- [SDR FDEA201402270418](https://openairdocs.org/sdr/FDEA201402270418), Feb 27, 2014: STRUT. CRACKED. FOUND NOSE GEAR LEAKING FLUID. INVESTIGATION FOUND ROUGHLY 15 INCH CRACK IN STRUT FROM TOP OF SERVICE POINT TO DOWN TO FRONT OF STRUT. INSTALLED SERVICEABLE NOS
- [SDR FDEA201401260202](https://openairdocs.org/sdr/FDEA201401260202), Jan 26, 2014: MECHANISM. DIRTY. HAD 3 GEAR UNSAFE, AFTER 2 CYCLES OF GEAR HANDLE, RAN QRH. ON THIRD ATTEMPT GOT 3 GREEN. FOUND EXCESSIVE FRICTION IN THE LONGITUDINAL AXIS OF THE LG CONTROL LEV
- [SDR FDEA201312243037](https://openairdocs.org/sdr/FDEA201312243037), Dec 24, 2013: CONTROL UNIT. FAULTY. LEFT ANTI-SKID FAIL. CREW STATED DURING DEBRIEF ALERT APPEARED AT GEAR EXTENSION, DID GO AROUND & HAD NO ALERT ON THE SECOND GEAR EXTENSION. ASCU SHOWS ASCU FAU
- [SDR FDEA201210013520](https://openairdocs.org/sdr/FDEA201210013520), Oct 1, 2012: SLEEVE. DAMAGED. ON TAXI, ADVISED BY THE TOWER THAT A PIECE OF OUR ENGINE COWL HAD FALLEN OFF. FOUND NR 2 ENGINE RT THRUST REVERSER COWL DAMAGED AND A LARGE SECTION MISSING. REM
- [SDR FDEA201208263178](https://openairdocs.org/sdr/FDEA201208263178), Aug 26, 2012: SKIN. MISREPAIRED. LEFT WING NR 6 SLAT MISREPAIRED. REPAIRED IAW EA 8-5750-160700, REPAIR CLASSIFIED AS MAJOR.
- [SDR FDEA201205231960](https://openairdocs.org/sdr/FDEA201205231960), May 23, 2012: SKIN. CORRODED. LOWER AFT RUDDER, FWD RT SIDE HAS AREA OF SURFACE CORROSION. REPAIRED LWR AFT RUDDER ON RT SIDE IAW SRM 55-10-00 AND EA 8-5540-157335.
- [SDR FDEA201108153279](https://openairdocs.org/sdr/FDEA201108153279), Aug 15, 2011: LAMP. INOPERATIVE. ENTRY DOOR LIGHTED EMERGENCY EXIT SIGN HAS SEVERAL INOPERATIVE BULBS, DIM ILLUMINATION. RELAMPED THE LT EXIT LIGHT'S IAW SMP CHECKED OK.
- [SDR FDEA201104041309](https://openairdocs.org/sdr/FDEA201104041309), Apr 4, 2011: LIGHT. INOPERATIVE. WHILE DOING PREFLIGHT FOUND R1 DOOR SLIDE TEST LIGHT NOT WORKING. REPLACED SLIDE PACK LIGHT SW ASSY, SLIDE LIGHT OPS. GOOD, IAW AMM 25-61-03-2. (CLOSED)
- [SDR FDEA201009023237](https://openairdocs.org/sdr/FDEA201009023237), Sep 2, 2010: COALESCER BAG. DIRTY. AT FL360, AFTER COCKPIT TEMP ADJUSTMENT-STRONG SMOKE ODOR FOLLOWED BY LARGE AMOUNT OF SMOKE IN COCKPIT. FOLLOWED QUICK REF HANDBOOK FOR SMOKE AND FUMES. EMERGEN
- [SDR FDEA201008012753](https://openairdocs.org/sdr/FDEA201008012753), Aug 1, 2010: ANGLE. CORRODED. CTR PIT SUMP DRAIN COMPT SHEAR TIE HAS CORROSION AT STA. 1761 APPROX. BETWEEN S- 51L TO S-51R. FOUND CORROSION OUT OF LIMITS AFTER BLENDING, REMOVED AND REPLACE
- [SDR FDEA201007292724](https://openairdocs.org/sdr/FDEA201007292724), Jul 29, 2010: SUPPORT. CORRODED. AFT CARGO COMPT LOWER FRAME SUPPORT HAS CORROSION AT STA. 1841 BETWEEN S-49R AND S-50R. REMOVED AND REPLACED FRAME SUPPORT AT STA 1841 BETWEEN S-49R AND S-50R I
- [SDR FDEA201007282690](https://openairdocs.org/sdr/FDEA201007282690), Jul 28, 2010: SHEAR TIE. CORRODED. CENTER PIT SUMP DRAIN COMPT. SHEAR TIE IS CORRODED AT AFT SURFACE AT STA. 1781 BETWEEN S-47R TO S-48R. REMOVED AND REPLACED CENTER PIT SUMP DRAIN COMPT. SHEAR T
- [SDR FDEA201007172575](https://openairdocs.org/sdr/FDEA201007172575), Jul 17, 2010: SEAT TRACK. DAMAGED. UPPER CARGO COMPT SEAT TRACK LBL 107 FS 1701 TO 1841 HAS 4 EA LOBES WORN. FABRICATED SEAT TRACK, HAT AND SPLICE USING TRAVELER T10/844703 AND T10/84470544705 FR
- [SDR FDEA201007162563](https://openairdocs.org/sdr/FDEA201007162563), Jul 16, 2010: SEAT TRACK. DAMAGED. UPPER CARGO SEAT TRACK FS 1731 TO 1721, LBL 28 HAS 2 LOBES PROTRUDING UPWARD AND ADDITIONAL LOBES DISTORTED. R & R DAMAGED SEAT TRACK SECTION AT LBL 28 FS 1721-
- [SDR FDEA201007162562](https://openairdocs.org/sdr/FDEA201007162562), Jul 16, 2010: FLOORBEAM. CRACKED. MAIN DECK STA 475, LBL 77 TO 107, FLOORBEAM IS CRACKED/DAMAGED. FABRICATED FLOORBEAM SEC REPAIR FROM 7075-T6 .071 BATCH NR 183113 IAW SRM 53-00-01, FIG 9, SHEET
- [SDR FDEA200909263389](https://openairdocs.org/sdr/FDEA200909263389), Sep 26, 2009: SENSOR. FAILED. FLT 3707. NR 2 ENGINE ROLLED BACK ON TAKEOFF, MAX N1 WAS 84 PERCENT, ENGINE FAIL LIGHT ON. CKED VIA'S AND HAD NR 2 ENG N1 FAILED MSG -PROBABLE CAUSE ENG 2 TACHO
- [SDR FDEA200909113286](https://openairdocs.org/sdr/FDEA200909113286), Sep 11, 2009: COALESCER BAG. ODOR. AFTER STARTING APU AND TURNING ON THE PACKS. HAD SMOKE COMING OUT OF DUCTS. R & R NR 3 PACK COALESCER BAGS, RAN APU, CLEARED FUMES FROM AIR CONDITIONING DUCTS. 
- [SDR FDEA200909103285](https://openairdocs.org/sdr/FDEA200909103285), Sep 10, 2009: PLUG. LEAKING. WHEN APU WAS STARTED AND APU BLEED TURNED ON, CABIN FILLED WITH SMOKE, TURNED OFF BLEEDS FOUND HYD FLUID RUNNING FROM AFT DRAIN HOLE INTO APU INLET. FOUND REV M
- [SDR FDEA200907172661](https://openairdocs.org/sdr/FDEA200907172661), Jul 17, 2009: WARNING LIGHT. FALSE ACTIVATION. GEAR UNSAFE WARNING DURING GEAR EXTENSION. GA PROCEDURE. ACCOMPLISHED QRH PROCEDURE ACCOMPLISHED WITH NORMAL GEAR EXTENSION - LEFT MAIN. NO CURRENT FAULTS LOGGE
- [SDR 08FDEA03715](https://openairdocs.org/sdr/08FDEA03715), Sep 3, 2008: PANEL. DAMAGED. NR 2 PYLON APRON HAS EDGE DAMAGE AT THE FWD END WHERE THE LT FAN COWL MATES. REPAIRED NR 2 FAN COWL LT APRON IAW E.A. 8-5480-123629.
- [SDR 08FDEA03642](https://openairdocs.org/sdr/08FDEA03642), Aug 29, 2008: VANE. DELAMINATED. LEFT OUTBOARD FLAP VANE; INBOARD LOWER SKIN IS DELAMINATED. REMOVED DELAMINATED INBOARD LOWER SKIN ON LEFT OUTBOARD FLAP VANE INBOARD END. FABRICATED SKIN PLUG 
- [SDR 08FDEA03629](https://openairdocs.org/sdr/08FDEA03629), Aug 28, 2008: SKIN. CRACKED. RIGHT NR 1 SLAT LOWER SURFACE SKIN IS CRACKED AT A FASTENER HOLE, TRAILING EDGE APPROX 1 INCH FROM THE INBD END. REMOVED RIGHT WING NR 1 SLAT IAW AMM 27-80-01-4
- [SDR 08FDEA03599](https://openairdocs.org/sdr/08FDEA03599), Aug 26, 2008: FRAME. CORRODED. FRAME P/N AEA 0273-3 REQUIRES FABRICATION DUE TO EXISTING FRAME BEING CORRODED BEYOND LIMITS AT STA 1501. FABRICATED A NEW FRAME SECTION AND SHEAR TIE IAW DAC D
- [SDR 08FDEA03528](https://openairdocs.org/sdr/08FDEA03528), Aug 21, 2008: LONGERON. CORRODED. LONGERON 51 L RIGHT END FITTING AT STA 1521 IS CORRODED. FABRICATED 1 LONGERON 51 L END FITTING P/N AYB 7020-2 IAW DWG NR AYB 7020.
- [SDR 08FDEA03527](https://openairdocs.org/sdr/08FDEA03527), Aug 21, 2008: LONGERON. CORRODED. LONGERON 51 L LEFT END FITTING AT STA 1521 IS CORRODED. FABRICATED 1 LONGERON END FITTING P/N AYB 7020-2 IAW BAC DWG NR AYB7020.
- [SDR 08FDEA03505](https://openairdocs.org/sdr/08FDEA03505), Aug 19, 2008: LONGERON. CORRODED. LONGERON 52 AT STA 1480 IN THE CENTER LANDING GEAR COMPARTMENT HAS CORROSION. REMOVED DAMAGED SECTION OF LONGERON 52 IAW SRM 51-33-01; PG 1; VOL II. LOCATED AND
- [SDR 08FDEA03445](https://openairdocs.org/sdr/08FDEA03445), Aug 15, 2008: FRAME. CORRODED. FRAME P/N AEA 0273-3 REQUIRES FABRICATION DUE TO BEING CORRODED BEYOND LIMITS. FABRICATED A NEW FRAME SECTION AND SHEAR TIE IAW DWG AEA 0273; REV "G". LOCATED A
- [SDR 08FDEA03398](https://openairdocs.org/sdr/08FDEA03398), Aug 13, 2008: BULKHEAD. CORRODED. THE CENTER WHEEL WELL SKIN HAS VARIOUS AREAS OF CORROSION FROM STA 1521 THRU 1380; BETWEEN LONGERON 51L TO LONGERON 51R. REPAIRED THE CENTER WHEEL WELL SKIN IAW
- [SDR 08FDEA03444](https://openairdocs.org/sdr/08FDEA03444), Aug 12, 2008: SKIN. CRACKED. RIGHT SIDE FUSELAGE SKIN AT STA 322 IS CRACKED 10 INCHES ABOVE THE FINGER DOUBLERS. REMOVED FIRST OFFICERS SEAT IAW AMM 25-11-01-4. REMOVED DAMAGE AND FABRICATE
- [SDR 08FDEA03377](https://openairdocs.org/sdr/08FDEA03377), Aug 11, 2008: LONGERON. CORRODED. CORROSION ON LONGERON 51L FROM BODY STA 1441 TO 1461. REMOVED DAMAGED SECTION OF LONGERON 51L FROM FS 1430 TO 1520 IAW SRM 51-33-01; PG 1; VOL II. LOCATED AND D
- [SDR 08FDEA03265](https://openairdocs.org/sdr/08FDEA03265), Aug 5, 2008: LONGERON. CORRODED. NR 1 AIR CONDITIONING COMP FUSELAGE SKIN, ANGLES; INTERCOSTAL WEB AND FASTENERS ARE CORRODED BETWEEN STA 562 AND STA 593; LONGERON 43L IMMEDIATELY OUTBOARD OF T

All 106: https://openairdocs.org/deregistered/N564FE-2024-03-02/reports.md

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