# N644FE: 1991 Mcdonnell Douglas MD-11F, 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-11F](https://openairdocs.org/model/mcdonnell-douglas-md-11f) (registry code 3023600)
- Engine: [Pratt & Whitney PW4462](https://openairdocs.org/engine/pratt-whitney-pw4462) (registry code 52171)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E24NE](https://openairdocs.org/tcds/E24NE) (OpenAirDocs)
- Serial number: 48444
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: June 8, 2011
- Certificate issued: January 18, 2011
- Last registry action: September 30, 2023
- Mode S code: A87499
- 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/N644FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=644FE
- Page: https://openairdocs.org/deregistered/N644FE-2024-03-02

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-11F: https://openairdocs.org/model/mcdonnell-douglas-md-11f.md

## Service difficulty reports (117, newest 50)

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

- [SDR FDEA201411063539](https://openairdocs.org/sdr/FDEA201411063539), Nov 6, 2014: FIRE BOTTLE. DISCHARGED. MULTIPLE BIRD STRIKES DESCENDING TO 7000 FT. RECEIVED ENGINE FIRE AGENT LOW, AGENT 2 LOW NR 3 ENG, ALERT. NO ADDITIONAL ENG ANOMALIES NOTED. REMOVED NR 3 ENGINE
- [SDR FDEA201311022674](https://openairdocs.org/sdr/FDEA201311022674), Nov 2, 2013: PUMP. LEAKING. LEVEL 2 NR 3 HYD FAIL ON SHORT FINAL, 3.9 GAL LEFT BOTH PUMPS WERE OFF. FOUND NR 3 FWD EDP LEAKING AT PUMP HSG ON ENGINE. R & R NR 3 ENGINE FWD EDP IAW AMM 29-1
- [SDR FDEA201305100964](https://openairdocs.org/sdr/FDEA201305100964), May 10, 2013: SKIN. CRACKED. LEFT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND STA XORS=713.6, SIX FASTENER HOLES FOUND CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY 
- [SDR FDEA201305100963](https://openairdocs.org/sdr/FDEA201305100963), May 10, 2013: SKIN. CRACKED. RIGHT WING LOWER SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS = 683.4 AND STA XORS=713.6. THREE FASTENER HOLES FOUND CRACK INDICATION DURING OPEN-HOLE HIGH FREQUENC
- [SDR FDEA201305080941](https://openairdocs.org/sdr/FDEA201305080941), May 8, 2013: FRAME. DENTED. MAIN DECK BS 1701, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 11
- [SDR FDEA201305080940](https://openairdocs.org/sdr/FDEA201305080940), May 8, 2013: FRAME. DENTED. MAIN DECK BS 1661, LONGERON 12R, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 11
- [SDR FDEA201305080939](https://openairdocs.org/sdr/FDEA201305080939), May 8, 2013: FRAME. DENTED. MAIN DECK BS 1741, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 11
- [SDR FDEA201305080938](https://openairdocs.org/sdr/FDEA201305080938), May 8, 2013: FRAME. DENTED. MAIN DECK BS 1701, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 11
- [SDR FDEA201305080937](https://openairdocs.org/sdr/FDEA201305080937), May 8, 2013: FRAME. DENTED. MAIN DECK BS 1661, LONGERON 12L, FRAME FOUND DENTED. FRAME REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REVISION 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, R
- [SDR FDEA201305060918](https://openairdocs.org/sdr/FDEA201305060918), May 6, 2013: VANE. DELAMINATED. RT WING INBD FLAP VANE LOWER SURFACE FOUND DELAMINATED. R & R RT WING INBD FLAP VANE IAW AMM 27-50-22-4, REV 76.1 CARRIED OUT FLAP VANE ADJUSTMENT TEST IAW AMM 
- [SDR FDEA201305060917](https://openairdocs.org/sdr/FDEA201305060917), May 6, 2013: SEAT TRACK. CORRODED. CABIN - RT BS 1019 X= -8.5 SEAT TRACK FOUND CORROSION. SEAT TRACK REPAIRED BY SECTIONAL REPLACEMENT BS 1009 TO 1049 IAW SRM 53-00-52, FIGURE 201, REPAIR 1, REV 
- [SDR FDEA201303200618](https://openairdocs.org/sdr/FDEA201303200618), Mar 20, 2013: PITOT LINE. BLOCKED. RTO DUE TO IAS ALERT AT 90 KTS ON CAPTAIN`S SIDE. REPLACED CAPTAINS PITOT TUBE, FOUND BLOCKAGE.
- [SDR FDEA201302210401](https://openairdocs.org/sdr/FDEA201302210401), Feb 21, 2013: BUSS. MALFUNCTIONED. ON FINAL, RECEIVED "EMER PWR ON" ALERT. AFTER LANDING, RECYCLED EMERGENCY POWER SWITCH AND CPT DISPLAY UNITS 1,2,3 WENT BLANK/DARK WITH NR 2 DISPLAY RED "X". TR
- [SDR FDEA201107092624](https://openairdocs.org/sdr/FDEA201107092624), Jul 9, 2011: COMPUTER. FAILED. ON TAKEOFF F/O AND STBY FLT INSTRUMENTS WERE ERRATIC. FOUND BOTH FCC'S AND ALL 3 IRU'S WITH NUMEROUS FAULTS ON NR2 ADC, REPLACED NR2 ADC IAW AMM 34-16-01-4 CK'S
- [SDR FDEA201106012060](https://openairdocs.org/sdr/FDEA201106012060), Jun 1, 2011: DOUBLER. CRACKED. WHEEL COMPARTMENT LT FWD SIDE SPOILER MIXER ROD CUT-OUT DOUBLER FOUND CRACK. R & R AS SRM 51-31-01, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201105302026](https://openairdocs.org/sdr/FDEA201105302026), May 30, 2011: SKIN. CHAFED. RT WING L/E LOWER SKIN FOUND WITH CHAFE MARKS WHERE PYLON NR1- TO -WING FAIRING CONTACTS. CHAFED SKIN REMOVED AS PER SRM 51-33-01 AND SRM 51-35-01 REV 46. FABRI
- [SDR FDEA201105302025](https://openairdocs.org/sdr/FDEA201105302025), May 30, 2011: SKIN. CHAFED. LEFT WING FIXED L/E LOWER SKIN FOUND WITH CHAFE MARKS WHERE PYLON-TO-WING CONTACTS. REFER TO SNRM N01217: LT WING FIXED L/E SKIN CHAFED. R & R SRM 51-33-01, REV
- [SDR FDEA201105302031](https://openairdocs.org/sdr/FDEA201105302031), May 30, 2011: RIB. CRACKED. RIGHT HAND WING LEADING EDGE COMPARTMENT NR 16 SLAT TRACK INBOARD SUPPORT BRACKET FOUND CRACKED RIB REMOVED AS PER SRM 51-33-01 & 51- 35-01 REV 46. FABRICATED R
- [SDR FDEA201105292023](https://openairdocs.org/sdr/FDEA201105292023), May 29, 2011: LONGERON. CORRODED. CENTER CARGO COMPARTMENT BILGE AREA STA 1651, LONGERON 47R, FOUND CORROSION ACCOMPLISHED EA ED E.A. 1-5310-149713 REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REV
- [SDR FDEA201105292022](https://openairdocs.org/sdr/FDEA201105292022), May 29, 2011: LONGERON. CORRODED. CENTER ACCESSORY COMPARTMENT - STA 6-70 TO STA 6-90, LONGERON NR 49R CORRODED CENTER ACCESSORY COMPARTMENT - CORRODED LONGERON NR 49R CUT-OUT AT STA 6-90 IAW SR
- [SDR FDEA201105282017](https://openairdocs.org/sdr/FDEA201105282017), May 28, 2011: SPAR CAP. CRACKED. CRACK INDICATION FOUND ON THE LOWER VERTICAL STABILIZER LEFT HAND UPPER FORWARD FLANGES OF THE REAR SPAR CAP. ACCOMPLISHED E.A.1-5530-149805, REPAIR CLASSIFIED 
- [SDR FDEA201105241959](https://openairdocs.org/sdr/FDEA201105241959), May 24, 2011: LONGERON. CORRODED. LOWER AFT CARGO STA 1853 TO STA 1863, LONGERON 48R FOUND CORRODED. CORROSION REMOVED IAW SRM 51-31-01, REV 46. FOUND EXCEEDED LIMITS IAW SRM 53-00-00, REV 46, F
- [SDR FDEA201105161844](https://openairdocs.org/sdr/FDEA201105161844), May 16, 2011: SUPPORT BRACKET. CRACKED. RIGHT WING FIXED L/E COMPARTMENT NR 16 SLAT TRACK INBD SUPPORT BRACKET FOUND CRACKED. RT WING L/E COMPT NR 16 SLAT TRACK INBD SUPPORT RIB REMOVED IAW SRM 51-33-
- [SDR FDEA201105121821](https://openairdocs.org/sdr/FDEA201105121821), May 12, 2011: SEAT TRACK. CORRODED. CABIN BETWEEN STA 1561 TO 1661, X = 7.0 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE UPPER AND LOWER SURFACE FOUND CORRODED. TRIMMED OFF AS PER SRM 53-00-52 REV 46,
- [SDR FDEA201105121822](https://openairdocs.org/sdr/FDEA201105121822), May 12, 2011: SEAT TRACK. CORRODED. CABIN BETWEEN STA 1561 TO 1661, X = -7.0 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE UPPER AND LOWER SURFACE FOUND CORRODED. ACCOMPLISHED "EA 1-5310-142539, REPAIR
- [SDR FDEA201105121820](https://openairdocs.org/sdr/FDEA201105121820), May 12, 2011: SEAT TRACK. CORRODED. CABIN BETWEEN STA 1581 TO 1601, X = 76.5 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE UPPER AND LOWER SURFACE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-5
- [SDR FDEA201105121819](https://openairdocs.org/sdr/FDEA201105121819), May 12, 2011: SEAT TRACK. CORRODED. CABIN BETWEEN STA 1561 TO 1581, X = 76.5 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201 NEW S
- [SDR FDEA201105121817](https://openairdocs.org/sdr/FDEA201105121817), May 12, 2011: FLOOR PANEL. WORN. CABIN BETWEEN STA 5-32 TO 5-53, X =-74 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND ELONGATED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SE
- [SDR FDEA201105121816](https://openairdocs.org/sdr/FDEA201105121816), May 12, 2011: SEAT TRACK. CORRODED. CABIN BETWEEN STA 1541 TO 1561, X = 7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. SEAT TRACK TRIMMED- OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW S
- [SDR FDEA201105121813](https://openairdocs.org/sdr/FDEA201105121813), May 12, 2011: SEAT TRACK. CORRODED. CABIN BETWEEN STA 5-113 TO 1541, X =7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. TRIMMED OFF IAW SRM 52-00-52, REV 46, FIG 201. NEW SEAT TRACK RE
- [SDR FDEA201105121812](https://openairdocs.org/sdr/FDEA201105121812), May 12, 2011: SEAT TRACK. CORRODED. CABIN BETWEEN STA 5-113 TO 1541, X = 7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. TRIMMED OFF CORROSION IAW SRM 52-00-52, REV 46, FIG 201. NEW SE
- [SDR FDEA201105121811](https://openairdocs.org/sdr/FDEA201105121811), May 12, 2011: SEAT TRACK. CORRODED. CABIN BETWEEN STA 5-93 TO 5-113, X =7.5 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPA
- [SDR FDEA201105121809](https://openairdocs.org/sdr/FDEA201105121809), May 12, 2011: SEAT TRACK. CORRODED. CABIN BETWEEN STA 5-53 TO 5-73, X = 10 SEAT TRACK FLOOR PANEL ATTACHMENT HOLES FOUND CORRODED. DAMAGED SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRA
- [SDR FDEA201105121808](https://openairdocs.org/sdr/FDEA201105121808), May 12, 2011: SEAT TRACK. CORRODED. CABIN BETWEEN STA 5-113 TO 1541, X =10 SEAT TRACK FLOOR PANEL ATTACHMENT HOLE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. NEW SEAT
- [SDR FDEA201105041746](https://openairdocs.org/sdr/FDEA201105041746), May 4, 2011: ACCESS PANEL. WORN. NR 2 PYLON ACCESS PANEL 475GR FOUND ONE (1) EACH WORN MOUNTING HOLE. ACCOMPLISHED EA 1-5480-142549, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201105031708](https://openairdocs.org/sdr/FDEA201105031708), May 3, 2011: BULKHEAD. CRACKED. AFT FUSELAGE COMPARTMENT - STA 2033 BULKHEAD, LT SIDE FORGING FOUND CRACK LINE NEAR TO UPPER CEILING CUT-OUT. ACCOMPLISHED EA 1-5310-149742, REPAIR CLASSIFIED A
- [SDR FDEA201105031707](https://openairdocs.org/sdr/FDEA201105031707), May 3, 2011: STOP FITTING. CRACKED. LT WING T/E OTBD FLAP UP-STOP FITTING FOUND CRACKED, R & R IAW SRM 51-33-01, REV 46. FLAP OPS CHECK C/OUT IAW AMM 27-50-30-5, REV 69.2 FOUND SATISFACTORY.
- [SDR FDEA201105031706](https://openairdocs.org/sdr/FDEA201105031706), May 3, 2011: STOP FITTING. CRACKED. RT WING T/E OTBD FLAP UP-STOP FITTING FOUND CRACKED. R & R IAW SRM 51-33-01, REV 46. FLAP OPS CHECK C/OUT IAW AMM 27-50-30-5, REV 69.2. REPAIR CLASSIFIED AS MAJ
- [SDR FDEA201105031705](https://openairdocs.org/sdr/FDEA201105031705), May 3, 2011: SPAR CAP. CRACKED. CRACK INDICATION FOUND ON THE LWR VERTICAL STAB ON THE RT UPPER FWD FLANGE OF THE REAR SPAR CAP FITTING. ACCOMPLISHED EA 1-5530-149805, REPAIR CLASSIFIED AS MAJ
- [SDR FDEA201105021689](https://openairdocs.org/sdr/FDEA201105021689), May 2, 2011: CHANNEL. DAMAGED. LOWER CTR CARGO COMPARTMENT BOTH AFT STA 1711 AND STA 1831, X= 38 AND X= -38 SHUTTLE BEAM LT AND RT CHAIN PROTECTIVE HATS BROKEN LOWER CTR CARGO COMPARTMENT AT 
- [SDR FDEA201105011686](https://openairdocs.org/sdr/FDEA201105011686), May 1, 2011: SKIN. CHAFED. LT WING FIXED L/E OTBD EXTERIOR SURFACE ABOVE PYLON FOUND CHAFED SKIN. REMOVED AS PER SRM 51-33-01 REV 46 AND SRM 51-35-01 REV 46. FABRICATED AS PER DWG ARB2363
- [SDR FDEA201105011685](https://openairdocs.org/sdr/FDEA201105011685), May 1, 2011: SKIN. CHAFED. RT WING FIXED L/E OTBD EXTERIOR SURFACE ABOVE PYLON FOUND CHAFED SKIN. REMOVED IAW SRM 51-33-01 AND SRM 51-35-01, REV 46. NEW SKIN FABRICATED IAW DWG ARB236 AND
- [SDR FDEA201104261624](https://openairdocs.org/sdr/FDEA201104261624), Apr 26, 2011: SEAT TRACK. CORRODED. CABIN BETWEEN STA 457 AND 495, X = -29 SEAT TRACK UPPER AND LOWER FLANGE FOUND CORRODED. SEAT TRACK REMOVED IAW SRM 51-31-01, REV 46. NEW SEAT TRACK REPAIR SECT
- [SDR FDEA201104261623](https://openairdocs.org/sdr/FDEA201104261623), Apr 26, 2011: STRINGER. CRACKED. LT WING UPPER AUX TANK AT STA XCW 46.500 STRINGER 9 FOUND CRACKED. ACCOMPLISHED EA 1-5710-149709. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201104261622](https://openairdocs.org/sdr/FDEA201104261622), Apr 26, 2011: STRINGER. CRACKED. RT WING UPPER AUX TANK AT STA XCW 17 STRINGER 9 FOUND CRACKED. ACCOMPLISHED EA 1-5710-149709, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201104261621](https://openairdocs.org/sdr/FDEA201104261621), Apr 26, 2011: STRINGER. CRACKED. RT WING UPPER AUX TANK AT STA XCW 46.500 STRINGER 9 FOUND CRACKED. ACCOMPLISHED EA 1-5710-149709. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 112.
- [SDR FDEA201104261620](https://openairdocs.org/sdr/FDEA201104261620), Apr 26, 2011: SUPPORT BRACKET. CRACKED. LT WING L/E COMPARTMENT NR 16 SLAT TRACK INBD SUPPORT BRACKET FOUND CRACKED. SUPPORT REMOVED IAW SRM 51-33-01 & 51-35-01, REV 46. FABRICATED IAW DWG ARB2850, RE
- [SDR FDEA201104211542](https://openairdocs.org/sdr/FDEA201104211542), Apr 21, 2011: SKIN. CRACKED. LT WING L/E DROOP SLAT UPPER SKIN FOUND WITH APPROX 0.375 INCH AND 0.3125 INCH CRACK. STOP DRILLED IAW SRM 57-40-01, REV 46, REPAIR 5 FIG 201. REPAIR DOUBLER FA
- [SDR FDEA201104211541](https://openairdocs.org/sdr/FDEA201104211541), Apr 21, 2011: SKIN. CRACKED. RT WING L/E DROOP SLAT UPPER SKIN FOUND WITH APPROX 1.75 INCH CRACKED. STOP DRILLED IAW SRM 57-40-01 REV 46, REPAIR 5, FIG 201. REPAIR DOUBLER FABRICATED IAW SR
- [SDR FDEA201104201525](https://openairdocs.org/sdr/FDEA201104201525), Apr 20, 2011: SEAT TRACK. CORRODED. CABIN BETWEEN STA 1661 TO STA 1669, X = 73 SEAT TRACK FLOOR PANEL ATTACHMENT FLANGE FOUND CORRODED. SEAT TRACK TRIMMED OFF IAW SRM 53-00-52, REV 46, FIG 201. FA

All 117: https://openairdocs.org/deregistered/N644FE-2024-03-02/reports.md

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