# N571FE: 1980 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 CF6-6 series](https://openairdocs.org/engine/ge-cf6-6-series) (registry code 30020)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 47830
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 16, 2005
- Certificate issued: March 27, 2002
- Last registry action: September 22, 2023
- Mode S code: A752A2
- 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/N571FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=571FE
- Page: https://openairdocs.org/deregistered/N571FE-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-10-10F: https://openairdocs.org/model/mcdonnell-douglas-md-10-10f.md

## Service difficulty reports (127, newest 50)

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

- [SDR FDEA2020061981277](https://openairdocs.org/sdr/FDEA2020061981277), Jun 18, 2020: LINE. BROKEN. LEVEL 2 HYD 3 FAIL SYSTEM DOWN TO 0.1 GALLONS. COMPLED WITH QRH PROCEDURES AND EMERGENCY/MANUAL GEAR EXTENSION. FOUND BROKEN HYD LINE BEHIND PANEL 616GB, WILL B
- [SDR FDEA2020061981270](https://openairdocs.org/sdr/FDEA2020061981270), Jun 18, 2020: LINE. DAMAGED. LEVEL 2 HYD 3 FAIL SYSTEM DOWN TO 0.1 GALLONS. COMPLED WITH QRH PROCEDURES AND EMERGENCY/MANUAL GEAR EXTENSION. REMOVED DAMAGED SECTION OF HYDRAULIC LINE AND RE
- [SDR FDEA201912043168](https://openairdocs.org/sdr/FDEA201912043168), Dec 4, 2019: SLIDE. DEFECTIVE. 1 LEFT DOOR SLIDE/RAFT LIGHT REMAINS ON. REMOVED AND REPLACED SLIDE RAFT ASSEMBLY.
- [SDR FDEA201908302046](https://openairdocs.org/sdr/FDEA201908302046), Aug 30, 2019: UNKNOWN. ODOR. A/C PACKS EMIT A STRONG ODOR. OPERATED ALL THE PACKS AND UNABLE TO DETECT ANY ODORS IAW MM 21-53-00-7 A/C OK TO CONTINUE.
- [SDR FDEA2019060651218](https://openairdocs.org/sdr/FDEA2019060651218), Jun 5, 2019: SWITCH. MALFUNCTIONED. LEVEL 3 ALERT "AIR MANF 3 FAIL" REMOVED & REPLACED #3 WING MANIFOLD FAIL DETECTOR SWITCH IAW MD10 MM36-23-03-4 & 36-23-03-5. RAN #3 ENGINE FOR LEAK TEST OF MANI
- [SDR FDEA201808071944](https://openairdocs.org/sdr/FDEA201808071944), Aug 7, 2018: RIB. DAMAGED. DURING EXTENSION OF THE INBD SLATS, DROOPED SLAT CONTACTED PANEL 616EB, CAUSING DAMAGE TO PANEL AND RIB. REMOVED AND REPLACED THE NUT PLATE STRIP IAW SRM 51-30-
- [SDR FDEA201709142561](https://openairdocs.org/sdr/FDEA201709142561), Sep 14, 2017: SLIDE. DAMAGED. DURING WALK AROUND POST FLIGHT CHECK L1 DOOR WAS INADVERTENLY ARMED AND SLIDE ACCIDENTLY FELL OUT. REMOVED AND REPLACED L1 DOOR SLIDE IAW AMM 25-61-01-2-4, A/C 
- [SDR FDEA201709142560](https://openairdocs.org/sdr/FDEA201709142560), Sep 14, 2017: BOTTLE. LOW PRESSURE. L1 DOOR AIR BOTTLE REQUIRES SERVICE. SERVICED L1 DOOR AIR RESERVOIR BOTTLE IAW M/M 52-10-01-2. A/C OK FOR SERVICE.
- [SDR FDEA201606081891](https://openairdocs.org/sdr/FDEA201606081891), Jun 8, 2016: LIGHT. INOPERATIVE. L1 DOOR REMOTE SLIDE PRESSURE LIGHT IS INOPERATIVE. RELAMPED LIGHT ASSY IAW SMP. ACFT OK FOR SERVICE.
- [SDR FDEA201606081890](https://openairdocs.org/sdr/FDEA201606081890), Jun 8, 2016: INDICATOR. INOPERATIVE. L1 DOOR REMOTE SLIDE PRESSURE LIGHT IS INOPERATIVE. RELEASED FOR SERVICE IAW MEL: 25-61-01. EVAC SLIDE REMOTE PRESS INDICATOR INOPERATIVE IAW MEL 25-61-01, VERI
- [SDR FDEA201606031797](https://openairdocs.org/sdr/FDEA201606031797), Jun 3, 2016: VALVE. FAILED. AFTER FUEL DUMP LT DUMP VALVE FAILED IN OPEN POSITION. R & R FUEL DUMP VALVE IAW 28-30-02. OPERATIONS & LEAK CHECK GOOD.
- [SDR FDEA201605311767](https://openairdocs.org/sdr/FDEA201605311767), May 31, 2016: SKIN PANEL. DENTED. LEFT WING, TOP OTBD TE PANEL BETWEEN SPOILER 4 & 5, APPROX STATION XW619 & XW692. R & R SKIN PANEL IAW EA T8-5720-T-0325706 P1.
- [SDR FDEA201605291752](https://openairdocs.org/sdr/FDEA201605291752), May 29, 2016: SMOKE DETECTOR. FAILED. CENTER CARGO AFT SMOKE DETECTOR FAILED. TEST REPLACED LOWER CTR CARGO SMOKE DETECTOR IAW AMM 26-14-01-4. PERFORMED CARGO SMOKE DETECTOR OPERATIONS TEST IAW AMM 
- [SDR FDEA201605271746](https://openairdocs.org/sdr/FDEA201605271746), May 27, 2016: PLACARD. DAMAGED. MAIN DECK FLOOR, FWD BALL MAT AREA FROM BS 608 - 792, LT SIDEWALL TO RT SIDEWALL, DECALS FOR CARGO LOADING PART NUMBERS & LOCATION REFERENCE ARE EITHER WORN, DA
- [SDR FDEA201605271744](https://openairdocs.org/sdr/FDEA201605271744), May 27, 2016: BULKHEAD. CRACKED. RIGHT STATION 595, BULKHEAD WEB HAS APPROX .500 CRACK AT LONGERON 43R, 2016-05-27. REMOVED DAMAGED AREA, FABRICATED FILLER, DOUBLER & FINGER DOUBLER & INSTALLED
- [SDR FDEA201605271743](https://openairdocs.org/sdr/FDEA201605271743), May 27, 2016: BULKHEAD. CRACKED. RIGHT STATION 595, BULKHEAD WEB HAS APPROX .500 CRACK AT LONGERON 39R, 2016-05-27. REMOVED DAMAGED AREA, FABRICATED FILLER & DOUBLER, INSTALLED IAW SRM 51-40-00
- [SDR FDEA201605221715](https://openairdocs.org/sdr/FDEA201605221715), May 22, 2016: SKIN. CRACKED. NUMBER 2 PYLON AFT FAIRING, BOAT TAIL, RT SIDE HAS MULTIPLE CRACKS IN SKIN CTR SECTION AREA. REPAIRED IAW SRM 54-20-00 FIG 9 VOL 1 & SRM 57-00-01 FIG 4, SHEET 2
- [SDR FDEA201605221714](https://openairdocs.org/sdr/FDEA201605221714), May 22, 2016: SKIN. CRACKED. NUMBER 2 PYLON AFT FAIRING, BOAT TAIL, RT SIDE HAS MULTIPLE CRACKS IN SKIN CTR SECTION AREA. REPAIRED IAW SRM 54-20-00 FIG 9 VOL 1.
- [SDR FDEA201605181655](https://openairdocs.org/sdr/FDEA201605181655), May 18, 2016: SKIN. CRACKED. LEFT WING PYLON LE, LOWER OTBD SURFACE IS CRACKED. INSTALLED DOUBLER & FILLER IAW EA 8-5710-T0325368.
- [SDR FDEA201605181654](https://openairdocs.org/sdr/FDEA201605181654), May 18, 2016: SEAT TRACK. DAMAGED. SEAT TRACK DAMAGED AT STATION 755, RBL 8 R & R DAMAGED SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1 VOL 1.
- [SDR FDEA201605151585](https://openairdocs.org/sdr/FDEA201605151585), May 15, 2016: ANGLE. CRACKED. LEFT WING, LT FUELING STATION DOOR, OTBD LANDING IS CRACKED. REPAIRED CRACK IAW SRM 57-00-01 FIG 140.
- [SDR FDEA201605131579](https://openairdocs.org/sdr/FDEA201605131579), May 13, 2016: TEE FITTING. CRACKED. RIGHT STATION 595, BULKHEAD TEE CAP VERTICAL FLANGE AT LONGERON 43R, HAS A 2 INCH CRACK. REPAIRED THE RT STA 595 BULKHEAD TEE CAP AT LONGERONS 39R AND 43R IN RE
- [SDR FDEA201605131577](https://openairdocs.org/sdr/FDEA201605131577), May 13, 2016: TEE FITTING. CRACKED. RIGHT STATION 595, BULKHEAD TEE CAP VERTICAL FLANGE AT LONGERON 39R, HAS A 2 INCH CRACK. REPAIRED TEE CAP IN REF TO EA 8-5310-T0324747
- [SDR FDEA201605051473](https://openairdocs.org/sdr/FDEA201605051473), May 5, 2016: PANEL. DELAMINATED. RIGHT MAIN WW PANEL ARC 0269-504 IS DELAMINATED, AREA MARKED NR 15 ON BOTTOM SIDE OF PANEL. REPAIRED IAW SRM 51-71-00 VOL II & PREPPED. PAINTED IAW SRM 51-21-02
- [SDR FDEA201604221351](https://openairdocs.org/sdr/FDEA201604221351), Apr 22, 2016: SKIN. DAMAGED. NUMBER 2 ACM DOOR, LOWER FWD CORNER DAMAGED. REPAIRED DOOR IAW DPS 3.69-5 & SRM 52-00-01 VOL 1 FIG 4 SHEET 2.
- [SDR FDEA201604211332](https://openairdocs.org/sdr/FDEA201604211332), Apr 21, 2016: SEAT TRACK. CORRODED. AFT CARGO COMPARTMENT, FOUND EXFOLIATION CORROSION ON THE NR 3 SEAT TRACK AT STATION 1841 - 1877, RBL 30R. R & R SECTION OF SEAT TRACK IAW SRM 53-70-00 FIG 1A S
- [SDR FDEA201604201313](https://openairdocs.org/sdr/FDEA201604201313), Apr 20, 2016: FORMER. CRACKED. RIGHT HORIZONTAL STABILIZER INBD, LE FIXED SEGMENT HAS A 1" CRACK AT THE NOSE RIB LOWER AFT CORNER, EMANATING FROM ONE FASTENER TO THE EDGE OF THE NEXT, JUST IN
- [SDR FDEA201604191281](https://openairdocs.org/sdr/FDEA201604191281), Apr 19, 2016: FINGER DOUBLER. CRACKED. CAC FINGER DOUBLER CORRODED & CRACKED AT SPLICE STATION 1129, MARKED OTBD OF LONGERON 48L. REPAIR IAW SRM 53-20-00 FIG 6.
- [SDR FDEA201604191280](https://openairdocs.org/sdr/FDEA201604191280), Apr 19, 2016: FLOORBOARD. DAMAGED. FORWARD CARGO BAY FLOORBOARD AT STATION 735, LBL 20, HAS A DAMAGED CORNER & NEEDS TO BE REPLACED. FABRICATED A NEW FLOORBOARD IAW SRZ-25-005.
- [SDR FDEA201604191279](https://openairdocs.org/sdr/FDEA201604191279), Apr 19, 2016: FLOORBOARD. DAMAGED. FORWARD CARGO PIT FLOORBOARD PANEL AT STATION 959, LBL 70, HAS A DAMAGED CORNER & NEEDS TO BE REPLACED. FABRICATED A NEW FLOOR PANEL IAW SRZ-25-005.
- [SDR FDEA201604171240](https://openairdocs.org/sdr/FDEA201604171240), Apr 17, 2016: SKIN PANEL. CRACKED. RIGHT UPPER AFT HORIZONTAL STABILIZER SKIN PANEL INBD AFT CORNER HAS A .400 INCH CRACK. CRACK STOP DRILLED IAW WC 55X1203ALI-P4 FIGURE 2 TABLE 1. CRACK FOUND TO
- [SDR FDEA201604131205](https://openairdocs.org/sdr/FDEA201604131205), Apr 13, 2016: SPAR CAP. CRACKED. RIGHT WING REAR SPAR LOWER CAP, CRACK LOCATED AT STATION XORS 412. CRACK STARTS ON AFT EDGE & CONTINUES ALONG HORIZONTAL AFT FLANGE THRU ONE BOLT HOLE FWD INTO 
- [SDR FDEA201604091315](https://openairdocs.org/sdr/FDEA201604091315), Apr 9, 2016: PANEL. DELAMINATED. LEFT WING, PANEL 541JB HAS A DENT & IS DELAMINATING AT THE CORNER. REPAIRED LT WING PANEL 541JB IAW SRM 51-71-00 VOL 2.
- [SDR FDEA201604091207](https://openairdocs.org/sdr/FDEA201604091207), Apr 9, 2016: SKIN. DENTED. RIGHT WING INBD FLAP, LOWER SURFACE AT STATION XIFH 253, THERE IS A DENT. REPAIRED IAW SRM 57-00-01 FIG 4 SHT 2 SRC TRACKING 8-5750-T0324796.
- [SDR FDEA201604091206](https://openairdocs.org/sdr/FDEA201604091206), Apr 9, 2016: SKIN. DENTED. RIGHT WING INBD FLAP, LOWER SURFACE AT STATION XIFH 245, THERE IS A DENT. REPAIRED IAW SRM 57-00-01 FIG 4 SHT 2 SRC TRACKING 8-5750-T0324796.
- [SDR FDEA201502270611](https://openairdocs.org/sdr/FDEA201502270611), Feb 27, 2015: BOTTLE. LOW PRESSURE. R1 DOOR PNEUMATIC EMER ASSIST BOTTLE PRESS LOW ON PREFLIGHT. SERVICED R1 DOOR AIR RESERVOIR.
- [SDR FDEA201408162188](https://openairdocs.org/sdr/FDEA201408162188), Aug 16, 2014: STANCHION. CORRODED. AFT CARGO COMPARTMENT STANCHION FOUND WITH CORROSION AT STATION 1781 X=10 RT LOWER SECTION. AFT CARGO COMPARTMENT STANCHION FOUND WITH CORROSION AT STA 1781 X= 
- [SDR FDEA201408162183](https://openairdocs.org/sdr/FDEA201408162183), Aug 16, 2014: FITTING. CORRODED. LOWER CTR CARGO COMPARTMENT BILGE AREA STA=1721 X=5 SHEAR CLIP SURFACE FOUND WITH MINOR CORROSION. CORROSION ON SHEAR CLIP AT LOWER CENTER CARGO COMPARTMENT BIL
- [SDR FDEA201408162187](https://openairdocs.org/sdr/FDEA201408162187), Aug 16, 2014: FITTING. CORRODED. AFT CARGO COMPARTMENT SHEAR CLIP ANGLE, TWO EACH, AT STATION 1821 BETWEEN L51L TO L51R BILGE AREA FOUND WITH SURFACE CORROSION. CORROSION ON SHEAR CLIP 02 EACH 
- [SDR FDEA201408162185](https://openairdocs.org/sdr/FDEA201408162185), Aug 16, 2014: FITTING. CORRODED. LOWER CTR CARGO COMPARTMENT BILGE AREA AT STATION Y=1781 X=-5 SHEAR CLIP SURFACE FOUND MINOR CORROSION. CORRODED SHEAR CLIP AT LOWER CENTER CARGO COMPARTMENT BI
- [SDR FDEA201408162189](https://openairdocs.org/sdr/FDEA201408162189), Aug 16, 2014: FITTING. CORRODED. LOWER FWD CARGO COMPARTMENT BILGE AREA AT STATION = 939 X = 5 SHEAR CLIP SURFACE FOUND MINOR CORROSION. CORRODED SHEAR CLIP AT LOWER FORWARD CARGO COMPARTMENT B
- [SDR FDEA201408162186](https://openairdocs.org/sdr/FDEA201408162186), Aug 16, 2014: FITTING. CORRODED. LOWER CTR CARGO COMPARTMENT BILGE AREA AT STATION =1776 X=-35 SHEAR CLIP SURFACE FOUND MINOR CORROSION. CORRODED SHEAR CLIP AT LOWER CENTER CARGO BILGE AREA STA
- [SDR FDEA201408162184](https://openairdocs.org/sdr/FDEA201408162184), Aug 16, 2014: FITTING. CORRODED. LOWER CTR CARGO COMPARTMENT BILGE AREA AT STATION Y=1741 X=5 SHEAR CLIP SURFACE FOUND MINOR CORROSION. CORROSION AT LOWER CENTER CARGO COMPARTMENT BILGE AREA SH
- [SDR FDEA201408162182](https://openairdocs.org/sdr/FDEA201408162182), Aug 16, 2014: FITTING. CORRODED. LOWER CTR CARGO COMPARTMENT BILGE AREA AT STATION Y=1761 X= 5 SHEAR CLIP SURFACE FOUND WITH MINOR CORROSION. CORROSION ON SHEAR CLIP AT LOWER CENTER CARGO COMPA
- [SDR FDEA201408162181](https://openairdocs.org/sdr/FDEA201408162181), Aug 16, 2014: FITTING. CORRODED. LOWER CARGO COMPARTMENT BILGE AREA AT STATION Y= 1761 X= -25 SHEAR CLIP SURFACE FOUND WITH MINOR CORROSION. CORRODED SHEAR CLIP AT LOWER CENTER CARGO COMPARTMEN
- [SDR FDEA201408082117](https://openairdocs.org/sdr/FDEA201408082117), Aug 8, 2014: DOOR FRAME. CRACKED. MAIN DECK R3 DOOR FORWARD JAMB BOX LOWER WEB FOUND CRACKED ON EXISTING REPAIR. AREA CRACKED EXISTING REPAIR DOUBLER AT MAIN DECK R3 DOOR JAMB REMOVED AS PER SRM
- [SDR FDEA201408082116](https://openairdocs.org/sdr/FDEA201408082116), Aug 8, 2014: SKIN. CRACKED. DUE TO EXISTING REPAIR DOUBLER REMOVED FOR ACCESS, FOUND CRACK AT LT WING FIXED LEADING SKIN XOS 906. CRACK SKIN AT LEFT HAND WING FIXED LEADING SKIN XOS 906 CA
- [SDR FDEA201408062085](https://openairdocs.org/sdr/FDEA201408062085), Aug 6, 2014: HINGE FITTING. CORRODED. LEFT WING INBD FLAP OTBD FWD HINGE BRACKET PIVOT BORE FOUND MINOR SURFACE CORROSION. REWORKED AND FOUND EXCEED LIMITS AS PER CMM 57-44-07 REVISION 62. EXISTING 
- [SDR FDEA201408062084](https://openairdocs.org/sdr/FDEA201408062084), Aug 6, 2014: FLOOR SUPPORT. CRACKED. AFT CARGO COMPARTMENT WEB FLOOR SUPPORT AT STATION 1900 X=18 LT CRACKED & CORRODED. FLOOR SUPPORT BEAM (WEB) TRIMMED AND REMOVED AS PER SRM 53-00-01 FIGURE 8 VO
- [SDR FDEA201408062083](https://openairdocs.org/sdr/FDEA201408062083), Aug 6, 2014: FRAME. CORRODED. LOWER CARGO COMPARTMENT BILGE AREA AT STATION Y=1781 X=16 FRAME ANGLE FOUND CORROSION. ACCOMPLISHED REPAIR AS PER SRM 53-30-00 FIGURE 5 VOLUME I REVISION 101. R

All 127: https://openairdocs.org/deregistered/N571FE-2024-03-02/reports.md

## FAA accident and incident reports (1)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20060205002429I](https://openairdocs.org/incident/20060205002429I), Feb 5, 2006: Doug MD1010F (N571FE), Austin, TX. (-23) A ballast cargo can container was loaded on an all cargo aircraft and the container locks were not set. The aircraft was flown from kelp to kaus with…

---
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.