# N567FE: 1979 Mcdonnell Douglas MD-10-10F, registration cancelled 2024-01-29

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: January 29, 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: 46994
- Year built: 1979
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 11, 2006
- Certificate issued: July 11, 2001
- Last registry action: April 1, 2023
- Mode S code: A7416D
- 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/N567FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=567FE
- Page: https://openairdocs.org/deregistered/N567FE-2024-01-29

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-10-10F: https://openairdocs.org/model/mcdonnell-douglas-md-10-10f.md

## Service difficulty reports (232, newest 50)

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

- [SDR FDEA201708112177](https://openairdocs.org/sdr/FDEA201708112177), Aug 11, 2017: LIGHT. MISSING. POST-FLT CK, LT FUSELAGE LANDING LIGHT MISSING FROM THE A/C WITH ASSOCIATED C/B TRIPPED.
- [SDR FDEA201708112180](https://openairdocs.org/sdr/FDEA201708112180), Aug 11, 2017: LIGHT. MISSING. DURING A POST FLIGHT CHECK, THE LT FUSELAGE LANDING LIGHT MISSING FROM THE ACFT. WITH AN ASSOCIATED CIRCUIT BREAKER TRIPPED.
- [SDR FDEA201608082842](https://openairdocs.org/sdr/FDEA201608082842), Aug 8, 2016: WIRE. CHAFED. NR 1 ENGINE FIRE AGENT LOW DURING CRUISE AND DECENT. CLEARED AFTER BLOCK IN TO GATE FOUND SHEILD ON WIRE TO P1-1261 WORN TO CENTER CONTACT IAW WDM 23-33-01. REP
- [SDR FDEA201607232607](https://openairdocs.org/sdr/FDEA201607232607), Jul 23, 2016: SEAT TRACK. WORN. MAIN DECK LT SEAT TRACK AT LBL 47.5 BETWEEN BS 1256 AND 1561, HAD SEVERAL AREAS OF WEAR. FOUND TO BE OUT OF LIMITS IAW SRM 53-70-00. REMOVED AND REPLACED THE SE
- [SDR FDEA201607232606](https://openairdocs.org/sdr/FDEA201607232606), Jul 23, 2016: FLOOR PANEL. DENTED. FLOOR PANEL AT BS 791 BETWEEN LBL 27.5 - 45 DENTED IN 3 AREAS. REMOVED AND REPLACED THE FLOOR PANEL IAW SRM 51-40-02 AND SRM 51-31-01 VOL II. MAJOR REPAIR.
- [SDR FDEA201607232605](https://openairdocs.org/sdr/FDEA201607232605), Jul 23, 2016: FLOOR PANEL. DENTED. FLOOR PANEL AT BS 791 BETWEEN LBL 27.5 - 45 DENTED IN 3 AREAS. REMOVED AND REPLACED THE FLOOR PANEL IAW SRM 51-40-02, AND SRM 51-31-01 VOL II. MAJOR REPAIR.
- [SDR FDEA201607232604](https://openairdocs.org/sdr/FDEA201607232604), Jul 23, 2016: FLOOR PANEL. CHAFED. FLOOR PANEL AT BS 791 BETWEEN LBL 8.5 AND RBL 8.5 IS CHAFED AND WORN. REMOVED AND REPLACED THE FLOOR PANEL IAW SRM 51-40-02, AND SRM 51-31-01 VOL II. MAJOR REPA
- [SDR FDEA201510143211](https://openairdocs.org/sdr/FDEA201510143211), Oct 14, 2015: ENGINE. FAULTY. DURING CLIMB OUT PASSING FL 260, NR 3 N1 WENT TOWARD ZERO WHILE ACFT EXPERIENCED MODERATE VIBRATION. MOVED THROTTLE TO IDLE EGT & N2 APPEARED NORMAL & WERE SIMI
- [SDR FDEA201507302438](https://openairdocs.org/sdr/FDEA201507302438), Jul 30, 2015: INDICATOR. INOPERATIVE. R1 REMOTE SLIDE PACK PRESSURE INDICATOR INOPERATIVE. REPLACED SLIDE REMOTE PRESSURE INDICATOR IAW MM 25-61-03-2. OPERATIONS CHECKED NORMAL.
- [SDR FDEA201502060463](https://openairdocs.org/sdr/FDEA201502060463), Feb 6, 2015: WARNING SYSTEM. FALSE ACTIVATION. AFTER PREFLIGHT SET UP, RECEIVED LEVEL 1 ALERT, EMER PWR ON, RETRIED EMER POWER CHECK WITH NO RESULTS. TROUBLESHOOT CHECKED IAW FIM 24-24-00. PULLED POWER FROM 
- [SDR FDEA201409062500](https://openairdocs.org/sdr/FDEA201409062500), Sep 6, 2014: SUPPORT. CRACKED. DURING OK TO CLOSE LT WING PANEL 531AT FOUND CRACKED AT BOTTOM FASTENER, APPROX 1 1/2 INCHES PROTRUDING ON THE FASTENER AT 2ND WEB RIB FROM STATION 118.200. REP
- [SDR FDEA201409032437](https://openairdocs.org/sdr/FDEA201409032437), Sep 3, 2014: SKIN PANEL. DELAMINATED. PANEL 635DR, OUTER SKIN HAS DELAMINATION ON OUTER SURFACE, APPROX AREA IS 4 INCHES X 6 INCHES. REPAIRED DELAMINATION TO OUTER SKIN & DOUBLER IAW SRM 51-71-00 PA
- [SDR FDEA201408302375](https://openairdocs.org/sdr/FDEA201408302375), Aug 30, 2014: FLOORBEAM. CORRODED. AFT CARGO COMPARTMENT FLOOR SUPPORT HAS SEVERAL PLACES OF CORROSION BETWEEN STATION X=-56 & X=56 STATION Y-1964. REMOVED FLOOR SUPPORT IN AFT CARGO COMPARTMENT 
- [SDR FDEA201408302374](https://openairdocs.org/sdr/FDEA201408302374), Aug 30, 2014: SUPPORT. CRACKED. NUMBER 1 ENG OTBD CORE COWL, AFT HINGE FITTING, AFT FACE HAS GOUGES. REMOVED & INSTALLED GUSSET IAW SRM 51-31-01. REMOVED & INSTALLED HINGE FITTING IAW CMM 71-3
- [SDR FDEA201408292359](https://openairdocs.org/sdr/FDEA201408292359), Aug 29, 2014: SKIN. CHAFED. RIGHT INBD AILERON LE SKIN LOWER SURFACE, ENTIRE LENGTH HAS CHAFED. R & R SKIN PN ARC1286-6 IAW SRM 51-31-01. FABRICATED SKIN ON STAM TRAVELER T14 1086055. TRAC
- [SDR FDEA201408282344](https://openairdocs.org/sdr/FDEA201408282344), Aug 28, 2014: SKIN. CHAFED. RIGHT INBD AILERON INBD LOWER LE SKIN HAS CHAFED. FOUND SKIN TO BE OUT OF LIMITS, ORIGINAL MATERIAL .040 INCHES, MATERIAL REMAINING .027 INCHES, MATERIAL LOSS .
- [SDR FDEA201408282342](https://openairdocs.org/sdr/FDEA201408282342), Aug 28, 2014: SKIN. CORRODED. UPPER AFT RUDDER, LT SIDE, EXTERNAL SURFACE AT UPPER STATIC BASE HAS CORROSION. R & R UPPER AFT RUDDER IAW AMM 27-20-02-4 & IAW WC E8-1110-7-4304 01. OPERATIONS
- [SDR FDEA201408272328](https://openairdocs.org/sdr/FDEA201408272328), Aug 27, 2014: CARGO TRACK. CORRODED. AFT CARGO COMPARTMENT TRACK HAS MULTIPLE SCRATCHES & SEVERAL SPOTS OF CORROSION AT STATION X=20, BETWEEN STATION Y 1781 - 1964. REMOVED CORROSION FROM AFT CARGO
- [SDR FDEA201408242302](https://openairdocs.org/sdr/FDEA201408242302), Aug 24, 2014: SEAT TRACK. WORN. UPPER CARGO SEAT TRACK RBL 8, FS 1260 HAS 2 WORN LOBES. REMOVED DAMAGED & WORN SEAT TRACK & REPLACED SEAT TRACK IAW SRM 53-70-00 FIG 1 AT FS 1260 RBL 8. FABRICA
- [SDR FDEA201408212283](https://openairdocs.org/sdr/FDEA201408212283), Aug 21, 2014: FLOOR SUPPORT. CORRODED. AFT CARGO COMPARTMENT RT FLOOR SUPPORT HAS SEVERAL SPOTS OF CORROSION AT STATION X- -64 BETWEEN STATION Y 1781 - 1841. FLOOR SUPPORT FOUND OUT OF LIMITS, 100% M
- [SDR FDEA201408142162](https://openairdocs.org/sdr/FDEA201408142162), Aug 14, 2014: SKIN. BULGED. LEFT INBD FLAP HAS SKIN BULGE AT UPPER CTR TE. REPAIRED LT INBD FLAP IAW SRM 57-20-00 FIG 13. CURRENTLY BEING TRACKED ON EA 8-5710-T0310431. FABRICATED FILLER 2
- [SDR FDEA201408122152](https://openairdocs.org/sdr/FDEA201408122152), Aug 12, 2014: SEAT TRACK. WORN. UPPER CARGO SEAT TRACK LBL 45 FS 755 HAS WORN LOBE. FOUND TO BE OUT OF LIMIT IAW SRM 53-70-00 FIG 5 SHEET1. REMOVED AND REINSTALLED FLOOR PANELS (FOM) IAW SRM 5
- [SDR FDEA201408122150](https://openairdocs.org/sdr/FDEA201408122150), Aug 12, 2014: SEAT TRACK. WORN. UPPER CARGO SEAT TRACK LBL 8 FS 1401 HAS WORN LOBE. REMOVED SEAT TRACK FOUND OUT OF LIMITS IAW SRM 53-70-00, FIG 1. ORG MAT .260, LOSS .015, REMAINING MAT.245. 
- [SDR FDEA201408122151](https://openairdocs.org/sdr/FDEA201408122151), Aug 12, 2014: SEAT TRACK. WORN. UPPER CARGO SEAT TRACK LBL 08, FS 1810 HAS WORN LOBE. REPAIRED SEAT TRACK AT STA 1810-1890, LBL 8 IAW ARM 53-70-00 FIG 1. SEAT TRACK P/N 60-10964. HAT T14/10854
- [SDR FDEA201408062095](https://openairdocs.org/sdr/FDEA201408062095), Aug 6, 2014: FLOORBEAM. CORRODED. AFT CARGO COMPARTMENT AFT INTERMEDIATE FLOOR SUPPORT BEAM HAS CORROSION AT STATION X=58, LT LONGERON 43 STATION Y 1781. REMOVED CORROSION FROM STA 1781 FLOORBEA
- [SDR FDEA201211284194](https://openairdocs.org/sdr/FDEA201211284194), Nov 28, 2012: BULKHEAD WEB. CRACKED. CENTER LANDING GEAR WHEEL WELL SPACE, LT WALL, UPPER AFT CORNER HAS THREE CRACKS. TWO RUNNING THROUGH RIVETS AND ONE COMING FROM A HOLE DOUBLER. VERIFIED USING 
- [SDR FDEA201207222636](https://openairdocs.org/sdr/FDEA201207222636), Jul 22, 2012: SKIN. MISREPAIRED. CARGO DOOR SKIN MISREPAIRED. REPAIRED AS PER EA 8-5230-159867.
- [SDR FDEA201207192613](https://openairdocs.org/sdr/FDEA201207192613), Jul 19, 2012: FRAME. MISREPAIRED. FRAME FOUND MISREPAIRED AT BS 1975 BETWEEN L46L-49R. REPAIRED AS PER SRM 53-30-00 FIGURE 5 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVI
- [SDR FDEA201207192612](https://openairdocs.org/sdr/FDEA201207192612), Jul 19, 2012: FRAME. MISREPAIRED. FRAME FOUND MISREPAIRED AT BS 1986 BETWEEN L46 L/R. REPAIRED AS PER SRM 53-30-00 FIGURE 5 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVIS
- [SDR FDEA201207172593](https://openairdocs.org/sdr/FDEA201207172593), Jul 17, 2012: FLOORBEAM. MISREPAIRED. FORWARD CARGO BAY FLOORBEAM BS 808, "X"= -22 TO "X" = -35 MISREPAIRED. REPAIRED AS PER EA 8-5310-159866. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115
- [SDR FDEA201207172592](https://openairdocs.org/sdr/FDEA201207172592), Jul 17, 2012: SKIN. MISREPAIRED. CENTER CARGO DOOR FRAME FWD CUT OUT SKIN MISREPAIRED AT BS 1701 BETWEEN LONGERON 39 AND LONGERON 42 RT. REPAIR CARRIED OUT PER SRM 53-50-00 FIGURE 26 VOLUME I R
- [SDR FDEA201207122552](https://openairdocs.org/sdr/FDEA201207122552), Jul 12, 2012: SKIN. MISREPAIRED. SKIN APPROX STATION 1220 TO STATION 1234 BETWEEN LONGERON 51 LT AND LONGERON 51 RT MISREPAIRED. REPAIRED IAW EA 8-5330-160977
- [SDR FDEA201207102528](https://openairdocs.org/sdr/FDEA201207102528), Jul 10, 2012: LONGERON. MISREPAIRED. LONGERON 52 LEFT MISREPAIRED BETWEEN BS 826 AND 840. REPAIRED IAW SRM 51-31-01 VOLUME II REVISION 99. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100 REVISION 115.
- [SDR FDEA201207102527](https://openairdocs.org/sdr/FDEA201207102527), Jul 10, 2012: LONGERON. MISREPAIRED. LONGERON 50 LEFT MISREPAIRED BETWEEN BS 808 AND 825. REPAIRED AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVI
- [SDR FDEA201207102526](https://openairdocs.org/sdr/FDEA201207102526), Jul 10, 2012: LONGERON. MISREPAIRED. LONGERON 51 RT MISREPAIRED BETWEEN BS 780 AND 825. REPAIRED IAW SRM 51-31-01 VOLUME II REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REVISION 115.
- [SDR FDEA201207102525](https://openairdocs.org/sdr/FDEA201207102525), Jul 10, 2012: LONGERON. MISREPAIRED. LONGERON 51 LT MISREPAIRED, BETWEEN STA 780 AND STA 825. REPAIRED IAW SRM 53-10-00 FIGURE 2 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJOR AS PER GMM 6-2-100 REV
- [SDR FDEA201207102529](https://openairdocs.org/sdr/FDEA201207102529), Jul 10, 2012: LONGERON. CRACKED. ON REMOVAL OF FUSELAGE SKIN, FOUND LONGERON 49 LT CRACKED AT BS 808. CARRIED OUT REPAIR AS PER SRM 53-10-00 FIGURE 2 VOLUME I REVISION 99. REPAIR CLASSIFIED MAJ
- [SDR FDEA201207042480](https://openairdocs.org/sdr/FDEA201207042480), Jul 4, 2012: RIB. MISREPAIRED. LT WING AILERON LOWER SKIN RIB MISREPAIRED, REPAIRED IAW EA 8-5750-160989, PART 1. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201207042479](https://openairdocs.org/sdr/FDEA201207042479), Jul 4, 2012: SKIN. MISREPAIRED. LT WING NR 3 SLAT AFT SKIN INBD OF NR 7 TRACK MISREPAIRED. REPAIRED IAW SRM 57-10-00, FIG 3, VOL I, REV 98. REPAIR CLASSIFIED MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201207042481](https://openairdocs.org/sdr/FDEA201207042481), Jul 4, 2012: SKIN. CRACKED. LEFT WING INBD FLAP ASSY UPPER SURFACE MID SEGMENT STA XIFH 165, FOUND CRACKED. FOUND CRACKED. CRACKED SKIN AT LEFT HAND WING INBOARD FLAP ASSEMBLY UPPER SURFAC
- [SDR FDEA201207022440](https://openairdocs.org/sdr/FDEA201207022440), Jul 2, 2012: SKIN. MISREPAIRED. RT WING NR 1 SLAT AFT SKIN MISREPAIRED. REPAIR CARRIED OUT IAW SRM 57-10-00, FIG 31, VOL I, REV 99. . REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100, REV 115.
- [SDR FDEA201207022436](https://openairdocs.org/sdr/FDEA201207022436), Jul 2, 2012: SKIN. MISREPAIRED. RT WING NR 5 SLAT AFT SKIN MISREPAIRED. REPAIRED IAW EA 8-5100-162351. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100 REV 115.
- [SDR FDEA201207022435](https://openairdocs.org/sdr/FDEA201207022435), Jul 2, 2012: SKIN. MISREPAIRED. LT WING NR 8 SLAT INBD LOWER SKIN MISREPAIRED. LT WING NR 8 SLAT R & R AMM 27-80-01-04, REV 14.3. OPS AND GAP CHECK CARRIED OUT IAW AMM 27-80-01-04, REV 14.3 FO
- [SDR FDEA201207022443](https://openairdocs.org/sdr/FDEA201207022443), Jul 2, 2012: FUEL CELL. CORRODED. CENTER WING TANK UPPER SKIN SURFACE FOUND WITH CORROSION AT STRINGER 6, RBL 1. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II REVISION 99. FOUND ACCEPTABLE AS 
- [SDR FDEA201207022442](https://openairdocs.org/sdr/FDEA201207022442), Jul 2, 2012: FUEL CELL. CORRODED. CENTER WING TANK UPPER SKIN SURFACE FOUND WITH CORROSION AT STRINGER 6, RBL 40. AFTER CORROSION REMOVAL, FOUND ACCEPTABLE AS PER EA 8-5730-159860. REPAIR CLASSI
- [SDR FDEA201207022441](https://openairdocs.org/sdr/FDEA201207022441), Jul 2, 2012: FUEL CELL. CORRODED. CENTER WING TANK UPPER SKIN SURFACE FOUND WITH CORROSION AT STRINGER 6, LBL 102. CORROSION REMOVED AS PER SRM 51-21-01 VOLUME II REVISION 99. ORIGINAL MATERIAL 
- [SDR FDEA201207022438](https://openairdocs.org/sdr/FDEA201207022438), Jul 2, 2012: SKIN. DAMAGED. BULK CARGO DOOR EXTERIOR SKIN LOWER FORWARD CORNER DAMAGED. CARRIED OUT REPAIR AS PER EA 8-5230-162350 PART 1. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-100 REVISI
- [SDR FDEA201207022437](https://openairdocs.org/sdr/FDEA201207022437), Jul 2, 2012: SKIN. MISREPAIRED. LT INBD ELEVATOR UPPER SKIN XE 111.75 MISREPAIRED. REPAIR ACCOMPLISHED PER SRM 55-10-00 FIGURE 8 VOLUME I REVISION 99. REPAIR CLASSIFIED AS MAJOR PER GMM 6-2-10
- [SDR FDEA201207022434](https://openairdocs.org/sdr/FDEA201207022434), Jul 2, 2012: SKIN. MISREPAIRED. HORIZONTAL STABILIZER INBD ELEVATOR UPPER SKIN FROM XE 148 TO XE 153 MISREPAIRED. REPAIR ACCOMPLISHED PER SRM 55-10-00 FIGURE 8 VOLUME I REVISION 99. REPAIR CLA
- [SDR FDEA201207022446](https://openairdocs.org/sdr/FDEA201207022446), Jul 2, 2012: SKIN. CORRODED. CORROSION BETWEEN FUSELAGE SKIN AND BARE STRAP AT BS 1139, BETWEEN LT STRINGER 46 AND 45. REPAIRED IAW SRM 53-20-00, FIG 18 AND FIG 6, VOLUME I, REV 99. REPAIR 

All 232: https://openairdocs.org/deregistered/N567FE-2024-01-29/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 20110201001209I](https://openairdocs.org/incident/20110201001209I), Feb 1, 2011: Mcdonnell D MD-10-10F (N567FE), Newark, NJ, Minor damage. At 0923 local time in ewr, N567FE an MD10 was parked on fedx spot 1 at ewr. N399FE another MD10 was parked on the center line and being deiced by a bucket…

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