# N580FE: 1993 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: 48471
- Year built: 1993
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 13, 2002
- Certificate issued: February 5, 2002
- Last registry action: September 22, 2023
- Mode S code: A7766A
- 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/N580FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=580FE
- Page: https://openairdocs.org/deregistered/N580FE-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-11F: https://openairdocs.org/model/mcdonnell-douglas-md-11f.md

## Service difficulty reports (128, newest 50)

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

- [SDR FDEA201505081433](https://openairdocs.org/sdr/FDEA201505081433), May 8, 2015: BOTTLE. DISCHARGED. L1 DOOR EMER DOOR OPENING BOTTLE WAS DISCHARGED & SLIDE WAS DISCONNECTED FROM DOOR DURING THE L1 DOOR EMER OPENING. THE SLIDE DID NOT INFLATE.
- [SDR FDEA201502190547](https://openairdocs.org/sdr/FDEA201502190547), Feb 19, 2015: BOTTLE. LOW PRESSURE. L1 DOOR ASSIST BOTTLE INDICATES LOW PRESS. SERVICED L1 DOOR ASSIST BOTTLE IAW AMM 12-25-04-3-0. OK FOR SERVICE.
- [SDR FDEA201409232715](https://openairdocs.org/sdr/FDEA201409232715), Sep 23, 2014: HYDRAULIC LINE. LEAKING. LEVEL ONE HYD 3 OFF PASSING FL 200 LEVEL TWO HYD 3 FAIL AT FL 370, LOWERED GEAR MANUALLY. FOUND HYD PRESS HOSE THAT CONNECTS FROM THE PYLON TO THE ENG HYD MANIF
- [SDR FDEA201404080697](https://openairdocs.org/sdr/FDEA201404080697), Apr 8, 2014: CONTROL UNIT. FAILED. ON TAXI OUT RECEIVED LVL 1, FIRE DET 2 FAIL. AFTER STOPPING ACFT, RAN A FIRE TEST & THEN RECEIVED LVL 3, ENG 2 FIRE, ALERT. RAN QRH PROCEDURES, FOR ENG FIRE SEV
- [SDR FDEA201305070928](https://openairdocs.org/sdr/FDEA201305070928), May 7, 2013: SKIN. MISREPAIRED. FUSELAGE SKIN, BS 979, LONGERON 47-48R MISREPAIRED. REPAIRED IAW SRM 53-00-01, FIG 201, REPAIR 1 REV 52. EO 1-5100-7- 5001B3, PART 1. REPAIR CLASSIFIED AS MAJOR
- [SDR FDEA201305060915](https://openairdocs.org/sdr/FDEA201305060915), May 6, 2013: SKIN. CRACKED. NR 3 AIRCONDITIONING COMPARTMENT AFT UPPER CORNER CUT-OUT SKIN FOUND CRACKED. NR 3 AIRCONDITIONING COMPARTMENT AFT UPPER CORNER CUT-OUT SKIN CARRIED OUT REPAIR 
- [SDR FDEA201305060919](https://openairdocs.org/sdr/FDEA201305060919), May 6, 2013: SKIN. CORRODED. RIGHT WING UPPER SURFACE FOUND CORROSION AT XORS 255 DURING SPOILER, UPPER SURFACE INSPECTION. CORROSION REMOVED AND FOUND EXCEED LIMITS IAW SRM 57-20-01, FIG 1
- [SDR FDEA201305060916](https://openairdocs.org/sdr/FDEA201305060916), May 6, 2013: RIB. WORN. RT WING NR 4 L/E SLAT INBD SLAT TRACK RIB FWD HOLE FOUND WORN AFTER REMOVAL OF NR 3 SLAT. NR 4 SLAT REWORKED IAW SRM 57-40-02 REPAIR 10, FIGURE 201, REVISION 52
- [SDR FDEA201305040910](https://openairdocs.org/sdr/FDEA201305040910), May 4, 2013: CAP. MISREPAIRED. LT WING T/E LOWER ACCESS PANEL 541JB CUT-OUT FWD EDGE LOWER CAP MISREPAIRED. REPAIRED IAW EA 1-5710-167609. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201305030903](https://openairdocs.org/sdr/FDEA201305030903), May 3, 2013: RIB. CRACKED. RIGHT WING NR 5 SLAT FOUND INBD INNER RIB CRACKED. NR 5 SLAT FABRICATED AND INSTALLED IAW EA 1-5750-166127, STEP 2 AND 3. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2
- [SDR FDEA201305030902](https://openairdocs.org/sdr/FDEA201305030902), May 3, 2013: SUPPORT FITTING. DAMAGED. MAIN CARGO DOOR LOWER FRAME SUPPORT FITTING NR 6 HOLE DIAMETER (D ) ABOVE THE LIMIT (0.580). R & R IAW SRM 51-31-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2
- [SDR FDEA201305030901](https://openairdocs.org/sdr/FDEA201305030901), May 3, 2013: SUPPORT FITTING. DAMAGED. MAIN CARGO DOOR LOWER FRAME SUPPORT FITTING NR 1 HOLE DIAMETER ABOVE THE LIMIT (0.580). R & R IAW SRM 51-31-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100,
- [SDR FDEA201305030900](https://openairdocs.org/sdr/FDEA201305030900), May 3, 2013: SUPPORT FITTING. DAMAGED. MAIN CARGO DOOR LOWER FRAME SUPPORT FITTING NR 7 HOLE DIAMETER (A & C ) ABOVE THE LIMIT (0.580). R & R IAW SRM 51-31-01, REV 52. REPAIR CLASSIFIED MAJOR IAW GMM
- [SDR FDEA201305030899](https://openairdocs.org/sdr/FDEA201305030899), May 3, 2013: SKIN. CRACKED. NR 3 AIR CONDITIONING COMPARTMENT AFT UPPER CORNER CUT-OUT SKIN FOUND CRACKED. REPAIRED IAW SRM 53-20-15, REPAIR 3, FIG 201 REV 52. REPAIR CLASSIFIED AS MAJOR I
- [SDR FDEA201305010893](https://openairdocs.org/sdr/FDEA201305010893), May 1, 2013: BEAM. CORRODED. CENTER WHEEL WELL BS 1461 TO 1490 RT DIAGONAL I-BEAM FOUND CORRODED. R & R WITH NEW FABRICATED I-BEAM IAW SRM 51-31-01, REV 52 AND EA 1-53-167608. REPAIR CLASSI
- [SDR FDEA201305010892](https://openairdocs.org/sdr/FDEA201305010892), May 1, 2013: BULKHEAD. CANNING. OIL CANNING AT CENTER LANDING GEAR RT VERTICAL WEB BETWEEN BS 1401 TO 1441, Z= -119 TO Z= -83. REPAIRED IAW EO 1-5100-7- 5001B3. REPAIR CLASSIFIED AS MAJOR IAW 
- [SDR FDEA201305010891](https://openairdocs.org/sdr/FDEA201305010891), May 1, 2013: BULKHEAD. CANNING. OIL CANNING AT CENTER LANDING GEAR LT VERTICAL WEB BETWEEN BS 1401 TO 1441, Z= -119 TO Z= -80. CARRIED OUT INSPECTION IAW EA 1-5310-167604, REPAIRED IAW EO 1-51
- [SDR FDEA201304280879](https://openairdocs.org/sdr/FDEA201304280879), Apr 28, 2013: SKIN. CRACKED. RIGHT WING - L/E LOWER SURFACE NR 12 SLAT TRACK CUT-OUT SKIN FOUND CRACKED AT XOS 777. DURING OTBD SLAT DRIVE CABLES INSPECTION. REPAIRED IAW SRM 57-40-02, FIG 
- [SDR FDEA201304280878](https://openairdocs.org/sdr/FDEA201304280878), Apr 28, 2013: FRAME. DENTED. BS 1661 LONGERON 12R FRAME FOUND DENTED. REPAIRED IAW SRM 53-00-07, FIG 201, REPAIR 2, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304280877](https://openairdocs.org/sdr/FDEA201304280877), Apr 28, 2013: DOOR FRAME. CRACKED. L3 DOOR FORWARD FRAME LOWER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15 FIGURE 201 REPAIR 3 REVISION 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304280876](https://openairdocs.org/sdr/FDEA201304280876), Apr 28, 2013: DOOR FRAME. CRACKED. R3 DOOR AFT FRAME LOWER WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304280875](https://openairdocs.org/sdr/FDEA201304280875), Apr 28, 2013: DOOR FRAME. CRACKED. R3 DOOR FORWARD FRAME WEB FOUND CRACKED. REPAIRED IAW SRM 53-40-15, FIG 201, REPAIR 3, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304260865](https://openairdocs.org/sdr/FDEA201304260865), Apr 26, 2013: SKIN. CRACKED. LEFT WING INBD FLAP UPPER SURFACE FOUND CRACKED AT XIFH 177 AND 58" FROM T/E. REPAIRED IAW EA 1-5750-166124. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 116.
- [SDR FDEA201304260863](https://openairdocs.org/sdr/FDEA201304260863), Apr 26, 2013: SKIN. LOOSE. LEFT WING INBD FLAP UPPER SURFACE, SEVERAL FASTENERS AT XIFH 159 FOUND LOOSE. R & R WITH NEW FASTENERS IAW SRM 51-35-01, REV 52. REPAIR CLASSIFIED AS MINOR IAW 
- [SDR FDEA201304260862](https://openairdocs.org/sdr/FDEA201304260862), Apr 26, 2013: SEAT TRACK. CORRODED. EXFOLIATION CORROSION FOUND ON SEAT TRACK BASE AT BS 491 TO 502, X= -27.5. REPAIRED IAW SRM 53-00-52, FIG 201, REPAIR 1, REV 52. REPAIR CLASSIFIED AS MAJOR IAW 
- [SDR FDEA201304240840](https://openairdocs.org/sdr/FDEA201304240840), Apr 24, 2013: SKIN. MISREPAIRED. RT WING FIXED L/E SURFACE TELESCOPIC DUCT CUT-OUT AREA MISREPAIRED. REPAIRED IAW SRM 57-40-01, REPAIR 10, FIGURE 201, REV 52 AND EA 1-5730-166121. REPAIR CLASSI
- [SDR FDEA201304240843](https://openairdocs.org/sdr/FDEA201304240843), Apr 24, 2013: SKIN. DELAMINATED. RIGHT WING OTBD FLAP T/E WEDGE INBD EDGE FORM DELAMINATED FROM XOFH 458.690 TO XOFH 468.690. REPAIRED IAW EA 1-5750-166120. REPAIR CLASSIFIED AS MAJOR AS PER GM
- [SDR FDEA201304240842](https://openairdocs.org/sdr/FDEA201304240842), Apr 24, 2013: SKIN. CRACKED. LT WING INBD FLAP UPPER SKIN AT XIFH= 171, 52" FROM T/E FOUND WITH 1 INCH CRACK. REPAIRED IAW EA 1-5750-166124. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 
- [SDR FDEA201304240841](https://openairdocs.org/sdr/FDEA201304240841), Apr 24, 2013: SKIN. CRACKED. RT WING NR 5 SLAT LOWER SURFACE FOUND CRACK ABOUT 5 INCHES LONG AT XOS 717. REPAIRED IAW EA 1-5750-166127, REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304240839](https://openairdocs.org/sdr/FDEA201304240839), Apr 24, 2013: ACCESS PANEL. CORRODED. RT WING T/E LOWER ACCESS PANEL 641JB CUT-OUT FWD EDGE LOWER CAP SURFACE FOUND CORRODED. REPAIRED IAW EA 1-5710-166116. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-10
- [SDR FDEA201304230831](https://openairdocs.org/sdr/FDEA201304230831), Apr 23, 2013: FRAME. MISREPAIRED. FRAME MISREPAIRED AT CABIN BS 535, L24L. REPAIRED IAW SRM 53-20-07, FIG 201, REPAIR 1, REV 52. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 116.
- [SDR FDEA201304230830](https://openairdocs.org/sdr/FDEA201304230830), Apr 23, 2013: FRAME. MISREPAIRED. FRAME MISREPAIRED AT CABIN STATION 535, L19L. REPAIRED IAW SRM 53-20-07, FIG 202, REPAIR 1, REV 52. EO 1-5100-7-5001B3, PART 1. REPAIR CLASSIFIED AS MAJOR IAW G
- [SDR FDEA201201260347](https://openairdocs.org/sdr/FDEA201201260347), Jan 26, 2012: PRESSURE SWITCH. FAILED. MAX POWER TAKE OFF, NR 2 ENGINE LOW OIL PRESSURE LIGHT ILLUMINATED. OIL PRESSURE INDICATED NORMAL ON GAUGES. ABORT WAS ACCOMPLISHED AT 20 KIAS. LIGHT WENT OUT W
- [SDR FDEA201108243450](https://openairdocs.org/sdr/FDEA201108243450), Aug 24, 2011: HINGE. CRACKED. RIGHT MLG DOOR-CENTER HINGE ASSY FOUND CRACKED. CRACKED HINGE REMOVED AND REPLACED WITH NEW HINGE AT RIGHT HAND DOOR CENTER AREA AS PER SRM 51-35-01 REV 47. REP
- [SDR FDEA201108173313](https://openairdocs.org/sdr/FDEA201108173313), Aug 17, 2011: SKIN. CORRODED. RT FUSELAGE SKIN BENEATH AFT BODY FAIRING (UPPER SIDE) FROM BS 2155 TO 2164, FOUND CORRODED AT SEVERAL LOCATIONS. CORROSION REMOVED IAW SRM 51-70-01, FIG 201. R
- [SDR FDEA201108173312](https://openairdocs.org/sdr/FDEA201108173312), Aug 17, 2011: SKIN. CORRODED. RT FUSELAGE BENEATH AFT BODY FAIRING (LOWER SIDE) FROM STA 2155 TO 2164 FOUND CORRODED AT SEVERAL LOCATIONS. CORROSION REMOVED, ORIGINAL THICKNESS 0.095", MATER
- [SDR FDEA201006262195](https://openairdocs.org/sdr/FDEA201006262195), Jun 26, 2010: PROBE. FAILED. AT LEVEL OFF CALM AIR GOT A FUEL QTY/FUEL USED LEVEL 2 POSSIBLE FUEL LEAK ALERT. FOLLOWED QRH PROCEEDURE S AND ISOLATED PROBLEM TO NR 2 MAIN TANK ERRONEOUS QTY 
- [SDR FDEA201002170442](https://openairdocs.org/sdr/FDEA201002170442), Feb 17, 2010: BRAKE. FAILED. AFTER TAKEOFF NR 8 BRAKE TEMP CLIMBED TO OVER 400 DEGREES BEFORE DECREASING. AFTER LANDING NR 8 BRAKE RAN HOTTER THAN THE OTHERS. GEAR WAS LOWERED TO COOL BRAKE
- [SDR FDEA200909183325](https://openairdocs.org/sdr/FDEA200909183325), Sep 18, 2009: SKIN. CORRODED. CORROSION - RT UPPER WING SURFACE AT XORS197. REPAIRED IAW EA 1-5710-132215.
- [SDR FDEA200909063264](https://openairdocs.org/sdr/FDEA200909063264), Sep 6, 2009: SKIN. CORRODED. LT WING UPPER SKIN AT STA, XORS 378 FOUND CORROSION. REPAIR IAW EA 1-5710-132212 TITLE: "WINGS-LT WING UPPER SKIN SURFACE CORROSION - REPAIR"
- [SDR FDEA200909063263](https://openairdocs.org/sdr/FDEA200909063263), Sep 6, 2009: SKIN. CORRODED. LT WING UPPER SKIN AT STA, XORS 130 TO XORS 197 FOUND CORROSIONS. REPAIR IAW EA 1-5710-132213 TITLE: "WINGS-LT WING UPPER SKIN SURFACE CORROSION - REPAIR"
- [SDR FDEA200909063262](https://openairdocs.org/sdr/FDEA200909063262), Sep 6, 2009: SKIN. CORRODED. LT WING UPPER SKIN AT STA. XORS 402 TO XORS 433 FOUND CORROSIONS. REPAIR IAW EA 1-5710-132212.
- [SDR FDEA200909013226](https://openairdocs.org/sdr/FDEA200909013226), Sep 1, 2009: SKIN. CORRODED. RIGHT UPPER WING SKIN HAS CORROSION AT STA XORS 150. REPAIRED IAW EA 1-5750-132215.
- [SDR FDEA200909013225](https://openairdocs.org/sdr/FDEA200909013225), Sep 1, 2009: SKIN. CORRODED. RIGHT UPPER WING SKIN HAS CORROSION, STA XORS 163. REPAIRED IAW EA 1-5710-132215.
- [SDR FDEA200909013224](https://openairdocs.org/sdr/FDEA200909013224), Sep 1, 2009: SKIN. CORRODED. RIGHT UPPER WING SKIN HAS CORROSION, STA XORS 298. REPAIRED IAW EA 1-5710-132215. MAJOR REPAIR.
- [SDR FDEA200909013223](https://openairdocs.org/sdr/FDEA200909013223), Sep 1, 2009: SKIN. CORRODED. LEFT UPPER WING SKIN STA XORS 317 TO 360 HAS CORROSION. REPAIR IAW EA 1-5750-132209.
- [SDR FDEA200909013222](https://openairdocs.org/sdr/FDEA200909013222), Sep 1, 2009: LONGERON. CORRODED. LONGERON 45R BS879 LWR OTBD SURFACE CORRODED IN FWD CARGO. COMPLIED WITH EA 1-5310-132210: FUSELAGE - LONGERON 45R CRACK AT APPROX STA 879 - REPAIR. REPAIR CLAS
- [SDR FDEA200909013201](https://openairdocs.org/sdr/FDEA200909013201), Sep 1, 2009: LONGERON. CORRODED. FWD CARGO - LONGERON 45R AT BS 879 LWR OTBD SURFACE CORRODED. COMPLIED WITH EA 1-5310-132210: FUSELAGE - LONGERON 45R CRACK AT APPROX STA 879 - REPAIR. REPAIR C
- [SDR FDEA200908313193](https://openairdocs.org/sdr/FDEA200908313193), Aug 31, 2009: SKIN PANEL. CRACKED. 25EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN INSP AT RT LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. REPAIR IAW EA 1-5710-1
- [SDR FDEA200908313192](https://openairdocs.org/sdr/FDEA200908313192), Aug 31, 2009: SKIN PANEL. CRACKED. 21 EA FASTENER HOLES FOUND CRACK INDICATION DURING HFEC OPEN HOLE INSPECTION AT LT W LWR SKIN ACCESS DOOR CUTOUT BETWEEN STA XORS=690 AND STA XORS=700. REPAIR I

All 128: https://openairdocs.org/deregistered/N580FE-2024-03-02/reports.md

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