# N645FE: 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: 48446
- Year built: 1991
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 4, 2011
- Certificate issued: January 21, 2011
- Last registry action: September 30, 2023
- Mode S code: A87850
- 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/N645FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=645FE
- Page: https://openairdocs.org/deregistered/N645FE-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-11F: https://openairdocs.org/model/mcdonnell-douglas-md-11f.md

## Service difficulty reports (74, newest 50)

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

- [SDR FDEA201501310398](https://openairdocs.org/sdr/FDEA201501310398), Jan 31, 2015: LENS. BROKEN. EVACUATION SLIDE REMOTE PRESS TO TEST INDICATING SYS INOPERATION COVER BROKEN. REPLACED PTT LENS AND LAMP REATAINER. OPS CHECK GOOD
- [SDR FDEA201307041478](https://openairdocs.org/sdr/FDEA201307041478), Jul 4, 2013: TRANSMITTER. INOPERATIVE. SHORTLY AFTER BEGINNING TAKEOFF ROLL, NR 1 FUEL FLOW SHOWED AMBER X. REJECTED TAKEOFF AT ABOUT 60 TO 70 KTS. FUEL FLOW INDICATING NORMAL AGAIN WHILE TURNING OFF
- [SDR FDEA201307021466](https://openairdocs.org/sdr/FDEA201307021466), Jul 2, 2013: SKIN. SEPARATED. RIGHT WING INBD AILERON T/E FOUND SKIN SEPARATED. REPAIRED RIGHT WING INBOARD AILERON TRAILING EDGE AS PER SRM 57- 50-02 REPAIR 3 FIGURE 201 REVISION 52 AND EA 
- [SDR FDEA201307011428](https://openairdocs.org/sdr/FDEA201307011428), Jul 1, 2013: SKIN. DELAMINATED. LEFT WING OTBD FLAP LOWER SURFACE T/E FOUND DELAMINATED XOFH 681.500 TO XOFH 689.500. REPAIRED IAW EA 1-5750-T0300982. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-10
- [SDR FDEA201307011427](https://openairdocs.org/sdr/FDEA201307011427), Jul 1, 2013: SKIN. DELAMINATED. LEFT WING OTBD FLAP LOWER SURFACE T/E FOUND DELAMINATED XOFH 553.00 TO XOFH 568.00. REPAIRED IAW EA 1-5750-T0300982. REPAIR CLASSIFIED AS MINOR IAW GMM 6-2-100 
- [SDR FDEA201307011426](https://openairdocs.org/sdr/FDEA201307011426), Jul 1, 2013: SKIN. DELAMINATED. RIGHT WING OTBD FLAP LOWER SURFACE FOUND DELAMINATED XOFH 673.542 TO XOFH 667.542. REPAIRED IAW EA 1-5750-T0300985 PART 1. REPAIR CLASSIFIED AS MINOR IAW GMM 6-
- [SDR FDEA201307011425](https://openairdocs.org/sdr/FDEA201307011425), Jul 1, 2013: SKIN. DELAMINATED. RIGHT WING OTBD FLAP T/E, LOWER SURFACE FOUND DELAMINATED XOFH 527.690 TO XOFH 552.690. REPAIRED IAW EA 1-5750-T0300985, PART 1. REPAIR CLASSIFIED AS MINOR IAW 
- [SDR FDEA201307011424](https://openairdocs.org/sdr/FDEA201307011424), Jul 1, 2013: SKIN. DELAMINATED. RIGHT WING OTBD FLAP T/E, UPPER SURFACE FOUND DELAMINATED AT XOFH 524.690 TO XOFH 554.690. REPAIRED IAW EA 1-5750-T0300985, PART 1. REPAIR CLASSIFIED AS MINOR I
- [SDR FDEA201306241379](https://openairdocs.org/sdr/FDEA201306241379), Jun 24, 2013: SKIN. CRACKED. TEN FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION, RT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN XORS=
- [SDR FDEA201306241378](https://openairdocs.org/sdr/FDEA201306241378), Jun 24, 2013: SKIN. CRACKED. EIGHT FASTENER HOLES FOUND TO HAVE CRACK INDICATIONS. DURING OPEN HOLE HIGH FREQUENCY EDDY CURRENT INSPECTION ONE LT WING LOWER SKIN ACCESS DOOR CUT-OUT BETWEEN
- [SDR FDEA201306211363](https://openairdocs.org/sdr/FDEA201306211363), Jun 21, 2013: FITTING. CORRODED. LEFT WING INBD FLAP DRIVE ARM SUPPORT BORE FOUND CORRODED. BORE REWORKED IAW SRM 51-21-01 REVISION 52 REPAIRED IAW EA 1-5750-T0300933A PART 1. REPAIR CLASSIFIED
- [SDR FDEA201306211362](https://openairdocs.org/sdr/FDEA201306211362), Jun 21, 2013: HINGE. CORRODED. RIGHT INBD FLAP, OTBD HINGE (FLAP MOUNTED) PIVOT ATTACHMENT OTBD LUG BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. RE
- [SDR FDEA201306211361](https://openairdocs.org/sdr/FDEA201306211361), Jun 21, 2013: HINGE. CORRODED. RIGHT INBD FLAP, OTBD HINGE (FLAP MOUNTED) PIVOT ATTACHMENT INBD LUG BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. RE
- [SDR FDEA201306211360](https://openairdocs.org/sdr/FDEA201306211360), Jun 21, 2013: HINGE BRACKET. CORRODED. LEFT INBD FLAP, OTBD HINGE (FLAP MOUNTED) PIVOT ATTACHMENT INBOARD LUG BORE FOUND CORRODED. BORE REWORKED AND FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. 
- [SDR FDEA201306211359](https://openairdocs.org/sdr/FDEA201306211359), Jun 21, 2013: HINGE BRACKET. CORRODED. LT INBD FLAP, OTBD HINGE (FLAP MOUNTED) PIVOT ATTACHMENT OTBD LUG, BORE FOUND CORRODED. BORE REWORKED FOUND EXCEED LIMITS IAW CMM 57-52-03 REVISION 76. REPAIRED
- [SDR FDEA201306191343](https://openairdocs.org/sdr/FDEA201306191343), Jun 19, 2013: FRAME. DENTED. FRAME BS 1761, LONGERON 12L FOUND DENTED. REPAIRED IAW SRM 53- 00-07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR AS IAW GMM 6-2-100 REVISION 116
- [SDR FDEA201306181332](https://openairdocs.org/sdr/FDEA201306181332), Jun 18, 2013: FRAME. DENTED. FRAME, BS 1701, LONGERON 12R FOUND DENTED. REPAIR CARRIED OUT IAW SRM 53-00 07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVIS
- [SDR FDEA201306181328](https://openairdocs.org/sdr/FDEA201306181328), Jun 18, 2013: FRAME. DENTED. FRAME BS 1721, LONGERON 12R, FOUND DENTED. REPAIR CARRIED OUT IAW SRM 53-00 07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVIS
- [SDR FDEA201306181326](https://openairdocs.org/sdr/FDEA201306181326), Jun 18, 2013: FRAME. DENTED. RIGHT FRAME BS 1641, LONGERON 12R FOUND DENTED. REPAIR CARRIED OUT IAW SRM 53-00 07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 
- [SDR FDEA201306181322](https://openairdocs.org/sdr/FDEA201306181322), Jun 18, 2013: FRAME. CHAFED. CABIN - LEFT SUPPORT YOKE, BS 535, LONGERON 19L, FRAME FOUND CHAFED. REPAIRED IAW SRM 53-20-07 FIGURE 202 REPAIR 1 REVISION 52. CLASSIFIED A MAJOR REPAIR IAW GM
- [SDR FDEA201306181331](https://openairdocs.org/sdr/FDEA201306181331), Jun 18, 2013: FRAME. DENTED. FRAME BS 1681, LONGERON 12L FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306181329](https://openairdocs.org/sdr/FDEA201306181329), Jun 18, 2013: FRAME. DENTED. FRAME BS 1701, LONGERON 12L FOUND DENTED. REPAIRED IAW SRM 53-00-07 FIGURE 201 REPAIR 2 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REVISION 116.
- [SDR FDEA201306181324](https://openairdocs.org/sdr/FDEA201306181324), Jun 18, 2013: FRAME. CHAFED. LEFT SUPPORT YOKE BS 535, LONGERON 21L FRAME FOUND CHAFED. REPAIRED IAW SRM 53-20-07 FIGURE 201 REPAIR 1 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100
- [SDR FDEA201306181319](https://openairdocs.org/sdr/FDEA201306181319), Jun 18, 2013: SKIN. CHAFED. LEFT INBD AILERON LOWER SKIN CHAFED AT TWO LOCATIONS. DAMAGED SKIN REMOVED AND FABRICATED NEW SKIN AS PER EA 1-5750-T0300853 AND REPLACED. REPAIR CLASSIFIED AS 
- [SDR FDEA201302210403](https://openairdocs.org/sdr/FDEA201302210403), Feb 21, 2013: UNKNOWN. UNKNOWN. REJECT TAKE OFF AT 85 KTS FOR FLAP WARNING ON EAD. PERFORMED R-T-S OF NR 1 AND NR 2 FCC'S IAW MM 27-54-00-5. RAN FLAPS FULL TRAVEL DOWN AND UP ALL INDICATIONS N
- [SDR FDEA201301200151](https://openairdocs.org/sdr/FDEA201301200151), Jan 20, 2013: LANDING GEAR. MALFUNCTIONED. ON APPROACH, THE EAD DISPLAYED A WHITE BOX WITH "LANDING GEAR." THE "GEAR UNSAGE INDICATION WITH GEAR HANDLE DOWN," QRH CHECKLIST WAS ACCOMPLISHED. ON SECOND AP
- [SDR FDEA201107192789](https://openairdocs.org/sdr/FDEA201107192789), Jul 19, 2011: SKIN. CORRODED. MAIN DECK INTERIOR , FOUND UNDERFLOOR STRUCTURE AT STA. 1230, LBL 103" WTH CORROSION. EXCEEDED LIMIT PER SRM57-10-01 FIG 101 REV 46. HFEC INSPECTION FOUND NO CR
- [SDR FDEA201107192788](https://openairdocs.org/sdr/FDEA201107192788), Jul 19, 2011: SKIN. CORRODED. MAIN DECK INTERIOR, FOUND UNDERFLOOR STRUCTURE AT STA.1203", LBL 103" WITH CORROSION. CORROSION REMOVED PER SRM51-21-01 REV 46. EXCEEDED LIMIT PER SRM57-10-01 F
- [SDR FDEA201107192787](https://openairdocs.org/sdr/FDEA201107192787), Jul 19, 2011: SKIN. CORRODED. MAIN DECK INTERIOR, FOUND UNDERFLOOR STRUCTURE AT STA 1235,RBL 51" WITH CORROSION. CORROSION REMOVED PER SRM51-21-01 REV 46. FOUND EXCEEDED LIMIT PER SRM 57-10-
- [SDR FDEA201107192786](https://openairdocs.org/sdr/FDEA201107192786), Jul 19, 2011: SKIN. CRACKED. RT WING FIXED L/E TELESCOPIC DUCT DOOR CUTOUT CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-01, FIG 202. REPAIR 10, REV 46. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-
- [SDR FDEA201107192785](https://openairdocs.org/sdr/FDEA201107192785), Jul 19, 2011: SKIN. CRACKED. LT WING FIXED L/E TELESCOPIC DUCT DOOR CUTOUT CORNER FOUND CRACKED. REPAIRED IAW SRM 57-40-01 FIG 202, REV 46. REPAIR 10. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2
- [SDR FDEA201107042559](https://openairdocs.org/sdr/FDEA201107042559), Jul 4, 2011: SKIN. DAMAGED. CABIN - DOOR 4 LT AFT CUTOUT INBD SKIN BETWEEN LONGERON 20 LT TO 21 LT SKIN PUNCTURED. DAMAGED AREA TRIMMED OUT PER SRM53-00-00 FIG 204 REV 46. HFEC INSPECTION 
- [SDR FDEA201107012522](https://openairdocs.org/sdr/FDEA201107012522), Jul 1, 2011: SEAT TRACK. CORRODED. CABIN - LT STRUCTURE UNDER DADO SUPPORT FROM FRAME 5-113 TO 1541 FOUND CORRODED. CARRIED OUT SEAT TRACK SECTIONAL REPAIR PER SRM53-00-52 FIG 101 REV 46. REPAIR 
- [SDR FDEA201107012521](https://openairdocs.org/sdr/FDEA201107012521), Jul 1, 2011: SHROUD. CRACKED. AFT CARGO COMPARTMENT - TAIL TANK TRANSFER FUEL LINE SHROUD FOUND CRACKED AT STATION Y=2005 DURING CHECK. REPAIRED LINE, LEAK CHECK CARRIED OUT AS PER AMM 28-25
- [SDR FDEA201106202342](https://openairdocs.org/sdr/FDEA201106202342), Jun 20, 2011: BULKHEAD. MISREPAIRED. REPAIR FOUND AT RT MLG WW HORIZONTAL PANEL CTR AREA SPLICE PLATE. FOUND MISREPAIRED. CARRIED OUT REPAIR AS PER EA1-5310-147672 REPAIR CLASSIFIED MAJOR AS PER GM
- [SDR FDEA201106132216](https://openairdocs.org/sdr/FDEA201106132216), Jun 13, 2011: INTERCOSTAL. CORRODED. LONGERON NR 20R BETWEEN STA 1341 TO STA 1361 CORRODED INTERCOSTAL REMOVED. NEW INTERCOSTAL FABRICATED IAW DWG AEA0163 REV 'C'. FPI CARRIED OUT ON NEW FABRICATED
- [SDR FDEA201106122209](https://openairdocs.org/sdr/FDEA201106122209), Jun 12, 2011: STRUCTURE. CORRODED. UPON REMOVAL OF LT WINDSHIELD, CUTOUT AREA FOUND CORRODED. CARRIED OUT REPAIR IAW EA 1-5310-147652, REPAIR CLASSIFIED AS MINOR IAW GMM6-2-100, REV 112.
- [SDR FDEA201106102197](https://openairdocs.org/sdr/FDEA201106102197), Jun 10, 2011: SPAR. CRACKED. VERTICAL STABILIZER REAR SPAR NR 4 BANJO FITTING SUSPECT CRACK AT STA 2164 AND ZID 54.5 AREA. (REFER TO SRM 55-30-02, FIG 201). REPAIRED AS PER SRM 55-30-02 FIG
- [SDR FDEA201106072141](https://openairdocs.org/sdr/FDEA201106072141), Jun 7, 2011: LONGERON. CORRODED. FWD CARGO COMPARTMENT, DURING REPAIR OF CORROSION LONG.48R STA 1059-1079 FOUND OUT CORROSION AT STA 1099 OF LONG 48R. CORRODED AREA REMOVED IAW SRM 51-21-01, RE
- [SDR FDEA201106072139](https://openairdocs.org/sdr/FDEA201106072139), Jun 7, 2011: SEAT TRACK. CORRODED. LT SEAT TRACK UNDER DADO SUPPORT FROM FRAME 5-53 TO 5-73 FOUND CORRODED. CARRIED OUT SEAT TRACK SECTION REPAIR. REPAIR CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-10
- [SDR FDEA201106022094](https://openairdocs.org/sdr/FDEA201106022094), Jun 2, 2011: HINGE FITTING. CORRODED. RT WING OTBD FLAP INBD HINGE (WING SIDE) PIVOT HOLE FOUND CORRODED. REPAIRED IAW EA1-5740-147656. EXISTING HOLE: 2.252" FINAL HOLE: 2.3185" MAX HOLE: 2.3135" . 
- [SDR FDEA201106022093](https://openairdocs.org/sdr/FDEA201106022093), Jun 2, 2011: HINGE FITTING. CORRODED. RT WING OTBD FLAP INBD HINGE (WING SIDE) SIDE LINK HOLE FOUND SURFACE CORRODED. REWORKED IAW CMM 20-11-02, REV 70. UPPER FACE EXISTING THICKNESS 0.481", MATERIA
- [SDR FDEA201106022092](https://openairdocs.org/sdr/FDEA201106022092), Jun 2, 2011: HINGE FITTING. CORRODED. RT WING OTBD FLAP, OTBD HINGE (WING SIDE) SIDE LINK HOLE, FOUND SURFACE CORRODED. REWORKED IAW EA 1-5740-147651. EXISTING THICKNESS 0.3845", MATERIAL REMOVED 0.
- [SDR FDEA201106022091](https://openairdocs.org/sdr/FDEA201106022091), Jun 2, 2011: HINGE FITTING. CORRODED. LEFT WING OTBD FLAP, INBD HINGE (WING SIDE) SIDE LINK HOLE SPOT FACE, FOUND CORRODED. REPAIRED IAW EA 1-5740-147655. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100,
- [SDR FDEA201106022090](https://openairdocs.org/sdr/FDEA201106022090), Jun 2, 2011: HINGE FITTING. CORRODED. LEFT WING OTBD FLAP, OTBD HINGE (WING SIDE) SIDE LINK HOLE SPOT FACE, FOUND CORRODED. REWORKED IAW CMM 20-11-02 REV 70. REMOVED: 0.003", FOUND THE REMAINING THI
- [SDR FDEA201106022089](https://openairdocs.org/sdr/FDEA201106022089), Jun 2, 2011: HINGE FITTING. CORRODED. LEFT WING OTBD FLAP, OTBD HINGE (WING SIDE) LOWER INBD MOUNT HOLE SPOT FACE FOUND CORRODED. REPAIRED IAW EA 1-5740-147654. EXISTING THICKNESS: 0.439", MATERIAL 
- [SDR FDEA201106022088](https://openairdocs.org/sdr/FDEA201106022088), Jun 2, 2011: HINGE FITTING. CORRODED. LEFT WING OTBD FLAP, OTBD HINGE (WING SIDE) UPPER OTBD MOUNT HOLE FOUND CORRODED. REWORKED IAW EA 1-5740-147654, PART 1(B). EXISTING HOLE: 0.881", FINAL HOLE: 0
- [SDR FDEA201106022087](https://openairdocs.org/sdr/FDEA201106022087), Jun 2, 2011: HINGE FITTING. CORRODED. LEFT WING OTBD FLAP, OTBD HINGE (WING SIDE) PIVOT HOLE FOUND CORRODED. REWORKED IAW EA 1-5740-147654 PART 1 A. EXISTING HOLE 2.251", FINAL HOLE 2.352", NEW BUSH
- [SDR FDEA201106022086](https://openairdocs.org/sdr/FDEA201106022086), Jun 2, 2011: FLOOR SUPPORT. CORRODED. RT FLOOR STRUCTURE BELOW DADO PANEL SUPPORT FROM STATION 1501 TO STATION 1521 FOUND CORRODED. REPAIRED IAW SRM 53-00-52, FIG 101, REV 46.
- [SDR FDEA201106022085](https://openairdocs.org/sdr/FDEA201106022085), Jun 2, 2011: SUPPORT. CORRODED. LEFT STRUCTURE UNDER DADO SUPPORT FROM STATION 1481 TO STATION 1501, FOUND CORRODED. CORROSION REMOVED IAW SRM 51-21-01, REV 46. ORIGINAL THICKNESS : 0.080", MA

All 74: https://openairdocs.org/deregistered/N645FE-2024-03-02/reports.md

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