# N577FE: 1992 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: 48469 - Year built: 1992 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: November 9, 2005 - Certificate issued: October 29, 2004 - Last registry action: June 3, 2023 - Mode S code: A768EC - 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/N577FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=577FE - Page: https://openairdocs.org/deregistered/N577FE-2024-03-02 From the FAA registry file of October 29, 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 (256, newest 50) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR FDEA201310022380](https://openairdocs.org/sdr/FDEA201310022380), Oct 2, 2013: WINDOW. LOOSE. LEFT SIDE COCKPIT ESCAPE ROPE VIEWING DOOR GLASS IS LOOSE. CORRECTLY INSTALLED VIEWING GLASS. - [SDR FDEA201204241541](https://openairdocs.org/sdr/FDEA201204241541), Apr 24, 2012: SKIN. MISREPAIRED. RT WING NR 5 SLAT AFT SURFACE OTBD LOWER CORNER STA XORS 682 MISREPAIRED. REPAIRED IAW EA 1-5750-160032. CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 114. - [SDR FDEA201204241539](https://openairdocs.org/sdr/FDEA201204241539), Apr 24, 2012: SKIN. MISREPAIRED. RT WING NR 8 SLAT UPPER SURFACE STATION XORS 995 MISREPAIRED. REPAIRED IAW EA 1-5750-160031 PART 1. CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 114. - [SDR FDEA201204191487](https://openairdocs.org/sdr/FDEA201204191487), Apr 19, 2012: SKIN. MISREPAIRED. NR 2 PYLON EXTERIOR APPROX STA Y = 2334 FOUND MISREPAIRED. REPAIRED IAW EO E1-5100-7-5001B PT1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114. - [SDR FDEA201204171449](https://openairdocs.org/sdr/FDEA201204171449), Apr 17, 2012: SKIN. MISREPAIRED. LT WING SKIN AT NR 3 SLAT LOWER SURFACE XORS 372. REPAIRED IAW EA1-5750-159830. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114. - [SDR FDEA201204161431](https://openairdocs.org/sdr/FDEA201204161431), Apr 16, 2012: SKIN. MISREPAIRED. SKIN AT BS 2147 - 2160, L33L MISREPAIRED. REPAIRED IAW SRM 53-70-01 FIGURE 201 REPAIR 3 REVISION 49 & EO E1-5100-7-5001B PT1. MAJOR REPAIR. - [SDR FDEA201204141399](https://openairdocs.org/sdr/FDEA201204141399), Apr 14, 2012: ATTACH FITTING. CRACKED. DURING HIGH FREQUENCY EDDY CURRENT INSPECTION AROUND STOP DRILL HOLE OF LT NOSE LANDING GEAR TRUNNION FITTING FOUND ONE NEW ADDITIONAL CRACK PROPAGATED FROM THE - [SDR FDEA201204121373](https://openairdocs.org/sdr/FDEA201204121373), Apr 12, 2012: LONGERON. CRACKED. FOUND LONGERON 49 LT FASTENER HOLE (COMMON TO NLG TRUNNION FITTING) CRACKED , APPROX 0.025". LONGERON REMOVED IAW SRM 51-31-01, REV 49. NEW LONGERON FABRICATED - [SDR FDEA201204101337](https://openairdocs.org/sdr/FDEA201204101337), Apr 10, 2012: FRAME. MISREPAIRED. FRAME STA 535 AT LONGERON 19 LT MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 49. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 114. - [SDR FDEA201204101335](https://openairdocs.org/sdr/FDEA201204101335), Apr 10, 2012: SKIN. MISREPAIRED. RT WING INBD FLAP UPPER SURFACE MISREPAIRED. REPAIRED IAW SRM 57-00-01, FIG 201, REPAIR 1, REV 49. - [SDR FDEA201204101334](https://openairdocs.org/sdr/FDEA201204101334), Apr 10, 2012: FRAME. MISREPAIRED. CABIN AT FRAME BS 535, LONGERON 23L FOUND MISREPAIRED. REPAIRED IAW SRM 53-20-07, FIG 201 REPAIR 1, REV 49. CLASSIFIED MAJOR IAW GMM 6-2-100, REV 114. - [SDR FDEA201204101344](https://openairdocs.org/sdr/FDEA201204101344), Apr 10, 2012: SKIN. CORRODED. MAIN DECK UPPER CARGO COMPARTMENT UNDER FLOOR AT CENTER WING TANK BETWEEN BS 1219 TO 1239, "X" = -90 TO "X" = -107.5 FOUND SURFACE CORROSION AT FASTENERS AREA. - [SDR FDEA201204101343](https://openairdocs.org/sdr/FDEA201204101343), Apr 10, 2012: SKIN. CORRODED. MAIN DECK UPPER CARGO COMPARTMENT UNDER FLOOR AT CENTER WING TANK BETWEEN BS 1219 TO 1239, "X" = -75.25 TO "X" = -90 FOUND SURFACE CORROSION AT FASTENERS AREA. - [SDR FDEA201204101342](https://openairdocs.org/sdr/FDEA201204101342), Apr 10, 2012: SKIN. CORRODED. MAIN DECK UPPER CARGO COMPARTMENT UNDER FLOOR AT CENTER WING TANK BETWEEN STATION 1219 TO STATION 1239, "X" = -75.25. FOUND SURFACE CORROSION AT FASTENERS AREA. - [SDR FDEA201204101341](https://openairdocs.org/sdr/FDEA201204101341), Apr 10, 2012: SKIN. CORRODED. MAIN DECK UPPER CARGO COMPARTMENT, UNDER FLOOR AT CENTER WING TANK BETWEEN STATION 1219 TO STATION 1239, "X" = -27.5 FOUND SURFACE CORROSION AT FASTENERS AREA. - [SDR FDEA201204101340](https://openairdocs.org/sdr/FDEA201204101340), Apr 10, 2012: SKIN. CORRODED. MAIN DECK UPPER CARGO COMPARTMENT, UNDER FLOOR AT CTR WING TANK BETWEEN BS 1219 TO 1239, "X" = -8.5 TO "X = -27.5. FOUND SURFACE CORROSION AT FASTENERS AREA. CO - [SDR FDEA201204101339](https://openairdocs.org/sdr/FDEA201204101339), Apr 10, 2012: LONGERON. CORRODED. CENTER CARGO COMPARTMENT, BILGE AREA BS 1646 LONGERON 50 LT FOUND WITH SURFACE CORROSION. REPAIR CARRIED OUT AT CENTER CARGO COMPARTMENT BILGE AREA STA 1646, LO - [SDR FDEA201204101338](https://openairdocs.org/sdr/FDEA201204101338), Apr 10, 2012: LONGERON. CORRODED. CENTER CARGO COMPARTMENT BS 1676 LONGERON 51 LT FOUND WITH SURFACE CORROSION. REPAIRED IAW SRM 53-00-05, FIG 201, REPAIR 1, REV 49. REPAIR CLASSIFIED MAJOR IAW - [SDR FDEA201204101333](https://openairdocs.org/sdr/FDEA201204101333), Apr 10, 2012: SKIN. CRACKED. LOWER VERTICAL STABILIZER FOUND RT SIDE REAR CENTER SPAR TO REAR SPAR LOWER PANEL CRACKED. REPAIR CARRIED OUT IAW SRM 55-30-02, FIG 201, REPAIR 2, REV 49. REPAI - [SDR FDEA201204101332](https://openairdocs.org/sdr/FDEA201204101332), Apr 10, 2012: SKIN. CORRODED. AFT ACCESSORY COMPARTMENT, FOUND CORROSION ON RT SKIN BS 2163 BODY FAIRING CUTOUT LOCATION. CORROSION REMOVED IAW SRM 51-21-01, REV 49. ORIGINAL THICKNESS: 0.95 - [SDR FDEA201204091326](https://openairdocs.org/sdr/FDEA201204091326), Apr 9, 2012: LONGERON. CORRODED. CENTER ACCESSORY COMPARTMENT STA 6-95, LONGERON 43 RT FOUND WITH CORROSION. REPAIRED IAW EA 1-5310-157171, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV - [SDR FDEA201204091324](https://openairdocs.org/sdr/FDEA201204091324), Apr 9, 2012: BUSHING. WORN. RT WING (FLAP SIDE) OTBD FLAP, OTBD HINGE, OTBD PIVOT HOLE BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.152" AND FOUND - [SDR FDEA201204091323](https://openairdocs.org/sdr/FDEA201204091323), Apr 9, 2012: HINGE FITTING. CORRODED. RT WING (WING SIDE) OTBD FLAP, OTBD HINGE, OTBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEED LIMIT IAW CMM 57-44-09, REV 72. EXISTING BORE DIAMETER 1 - [SDR FDEA201204091322](https://openairdocs.org/sdr/FDEA201204091322), Apr 9, 2012: HINGE FITTING. CORRODED. RT WING (WING SIDE) OTBD FLAP, OTBD HINGE, INBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-09, REV 72. EXISTING BORE DIAMETER - [SDR FDEA201204091321](https://openairdocs.org/sdr/FDEA201204091321), Apr 9, 2012: HINGE FITTING. CORRODED. RT WING (WING SIDE) OTBD FLAP, OTBD HINGE, LOWER MOUNT, OTBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. OTBD BORE REWORKED AND FOUND EXCEEDE - [SDR FDEA201204091320](https://openairdocs.org/sdr/FDEA201204091320), Apr 9, 2012: HINGE FITTING. CORRODED. RT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT, INBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. INBOARD HOLE REWORKED AND FOUND EXCEE - [SDR FDEA201204091319](https://openairdocs.org/sdr/FDEA201204091319), Apr 9, 2012: HINGE FITTING. CORRODED. LT WING (WING SIDE) OTBD FLAP, INBD HINGE, OTBD ACTUATOR HOLE FOUND CORRODED. REWORKED AND FOUND EXCEEDED LIMIT IAW CMM 57-44-08, REV 72. ORIGINAL BORE DIAMETER - [SDR FDEA201204091318](https://openairdocs.org/sdr/FDEA201204091318), Apr 9, 2012: BUSHING. WORN. LT WING (WING SIDE) OTBD FLAP, INBD HINGE, INBD ACTUATOR HOLE BUSHING FOUND WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, DIAMETER = 1.231" AND - [SDR FDEA201204091317](https://openairdocs.org/sdr/FDEA201204091317), Apr 9, 2012: HINGE FITTING. CORRODED. LT WING (WING SIDE) OTBD FLAP, INBD HINGE LOWER MOUNT OTBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE REWORKED AND FOUND EXCEEDED LIMIT - [SDR FDEA201204091316](https://openairdocs.org/sdr/FDEA201204091316), Apr 9, 2012: HINGE FITTING. CORRODED. LT WING (WING SIDE) OTBD FLAP, INBD HINGE SIDE LOAD FITTING SURFACE FOUND CORRODED. REWORKED IAW CMM 20-11-02, REV 72. UPPER EXISTING THICKNESS: 0.400", MATERIA - [SDR FDEA201204091314](https://openairdocs.org/sdr/FDEA201204091314), Apr 9, 2012: BUSHING. WORN. LT WING (WING SIDE) OTBD FLAP, OTBD HINGE, INBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE DIAMETER 1.251" AND FOUND EXCEEDED LI - [SDR FDEA201204091312](https://openairdocs.org/sdr/FDEA201204091312), Apr 9, 2012: HINGE FITTING. CORRODED. LT WING (WING SIDE) OTBD FLAP, OTBD HINGE SIDE LOAD FITTING SURFACE FOUND CORROSION. REWORKED IAW CMM 20-11-02, REVISION 72. UPPER EXISTING THICKNESS: 0.425", M - [SDR FDEA201204091311](https://openairdocs.org/sdr/FDEA201204091311), Apr 9, 2012: HINGE FITTING. CORRODED. LT WING (WING SIDE) OTBD FLAP, OTBD HINGE, SIDE LOAD FITTING LOWER HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE REWORKED AND FOUND EXCEED - [SDR FDEA201204091310](https://openairdocs.org/sdr/FDEA201204091310), Apr 9, 2012: HINGE FITTING. CORRODED. LT WING (WING SIDE) OTBD FLAP, OTBD HINGE SIDE LOAD FITTING UPPER HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. UPPER HOLE REWORKED AND FOUND E - [SDR FDEA201204091309](https://openairdocs.org/sdr/FDEA201204091309), Apr 9, 2012: HINGE FITTING. CORRODED. LT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT, OTBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. OTBD BORE REWORKED AND FOUND EXCEEDED - [SDR FDEA201204091308](https://openairdocs.org/sdr/FDEA201204091308), Apr 9, 2012: HINGE FITTING. CORRODED. LT WING (WING SIDE) OTBD FLAP, OTBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. INBD BORE REWORKED AND FOUND EXCEEDED - [SDR FDEA201204091307](https://openairdocs.org/sdr/FDEA201204091307), Apr 9, 2012: BUSHING. WORN. RT WING (WING SIDE) OTBD FLAP, INBD HINGE, OTBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, DIAMETER 1.252" FOUND EXCEE - [SDR FDEA201204091306](https://openairdocs.org/sdr/FDEA201204091306), Apr 9, 2012: HINGE FITTING. DAMAGED. RT WING (WING SIDE) OTBD FLAP, INBD HINGE, INBD ACTUATOR HOLE BUSHING WORN. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED DIAMETER 1.253" AND FOUND EX - [SDR FDEA201204091305](https://openairdocs.org/sdr/FDEA201204091305), Apr 9, 2012: HINGE FITTING. CORRODED. RT WING (WING SIDE) OTBD FLAP, INBD HINGE LOWER MOUNT INBD HOLE FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. LOWER MOUNT INBD BORE REWORKED AND FOU - [SDR FDEA201204091304](https://openairdocs.org/sdr/FDEA201204091304), Apr 9, 2012: HINGE FITTING. CORRODED. RT WING (WING SIDE) OTBD FLAP, INBD HINGE LOWER MOUNT OTBD HOLE, FOUND CORRODED. BUSHING REMOVED IAW CMM 20-20-07, REV 72. LOWER MOUNT OTBD BORE REWORKED AND FO - [SDR FDEA201204091303](https://openairdocs.org/sdr/FDEA201204091303), Apr 9, 2012: HINGE FITTING. CORRODED. RT WING (WING SIDE) OTBD FLAP, INBD HINGE SIDE LOAD FITTING SURFACE, FOUND CORRODED. REWORKED IAW CMM 20-11-02 REV 72. UPPER EXISTING THICKNESS: 0.412", MATERIA - [SDR FDEA201204091301](https://openairdocs.org/sdr/FDEA201204091301), Apr 9, 2012: HINGE FITTING. DAMAGED. LEFT WING (FLAP SIDE), INBD FLAP OTBD HINGE, OTBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, OTBD LUG DIAMETER 1.254" - [SDR FDEA201204091300](https://openairdocs.org/sdr/FDEA201204091300), Apr 9, 2012: HINGE FITTING. DAMAGED. LEFT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, INBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURE, INBD LUG, DIAMETER 1.283" - [SDR FDEA201204091299](https://openairdocs.org/sdr/FDEA201204091299), Apr 9, 2012: HINGE FITTING. DAMAGED. RT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, OTBD PIVOT HOLE, FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURED, OTBD LUG DIAMETER 1.250", - [SDR FDEA201204091298](https://openairdocs.org/sdr/FDEA201204091298), Apr 9, 2012: HINGE FITTING. DAMAGED. RT WING (FLAP SIDE) INBD FLAP, OTBD HINGE, INBD PIVOT HOLE FOUND STEP HOLE. BUSHING REMOVED IAW CMM 20-20-07, REV 72. BORE MEASURE, INBD LUG DIAMETER 1.252 IN, - [SDR FDEA201204071285](https://openairdocs.org/sdr/FDEA201204071285), Apr 7, 2012: SKIN. CRACKED. HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON LT WING FUEL TANK LOWER ACCESS DOOR PANEL NR 536AB CUTOUT AND FOUND CRACK INDICATION ON 04 EACH FASTENER HOLES. RE - [SDR FDEA201204071284](https://openairdocs.org/sdr/FDEA201204071284), Apr 7, 2012: SKIN. CRACKED. HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSP ON RT WING FUEL TANK LOWER ACCESS DOOR PANEL NR 636AB CUTOUT AND FOUND CRACK INDICATION ON 06 EACH FASTENER HOLES. RE - [SDR FDEA201204061275](https://openairdocs.org/sdr/FDEA201204061275), Apr 6, 2012: SKIN. CRACKED. RIGHT WING LOWER FIXED L/E AT REFUELING PANEL CUTOUT INBD FORWARD CORNER AREA FOUND CRACKED. REPAIR CARRIED OUT IAW SRM 57-40-02. REPAIR 7 FIG 201 REV 49. REPAI - [SDR FDEA201204051266](https://openairdocs.org/sdr/FDEA201204051266), Apr 5, 2012: SKIN. MISREPAIRED. LT WING DROOP L/E UPPER SURFACE FOUND MISREPAIRED IAW SRM 57-40-01, REPAIR 5, FIGURE 201. REPAIRED IAW EA 1-5730-159836, CLASSIFIED MAJOR IAW GMM 6-2-100, REV 1 - [SDR FDEA201204051270](https://openairdocs.org/sdr/FDEA201204051270), Apr 5, 2012: SKIN. CRACKED. RT WING FIXED L/E LOWER SURFACE AT NR 14 SLAT TRACK LOWER CUTOUT FOUND CRACKED. REPAIR CARRIED OUT AT RT WING FIXED L/E LOWER SURFACE AT NR 14 SLAT TRACK LOWER All 256: https://openairdocs.org/deregistered/N577FE-2024-03-02/reports.md --- 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.