# N10060: 1979 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 CF6-6D](https://openairdocs.org/engine/ge-cf6-6d) (registry code 30076)
- Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE), [TCDS E23EA](https://openairdocs.org/tcds/E23EA) (OpenAirDocs)
- Serial number: 46970
- Year built: 1979
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 8, 1994
- Certificate issued: January 30, 2006
- Last registry action: August 4, 2023
- Mode S code: A007F7
- 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/N10060
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=10060
- Page: https://openairdocs.org/deregistered/N10060-2024-03-02

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

## Service difficulty reports (235, newest 50)

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

- [SDR FDEA202004130737](https://openairdocs.org/sdr/FDEA202004130737), Apr 13, 2020: STATIC WICK. OUT OF TOLERANCE. PDIS 060 23-10 4976 13APR20 FLL FACT U LOGPAGES:3208974 LOST ALL THREE COM'S PASSING THRU FL310. AFTER PASSING FL350 #1 STARTED TO WORK, ONE BY ONE THEN ON OTHE
- [SDR FDEA201909072149](https://openairdocs.org/sdr/FDEA201909072149), Sep 7, 2019: VIA. MALFUNCTIONED. DURING TAKEOFF ROLL SEVERAL OF THE DU'S STARTED TO FLASH ON AND OFF. ALSO RECEIVED A CONFIGURATION WARNING. ABORTED TAKEOFF AT APPOX 90 KTS. R&R #3 VIA PRECAUTI
- [SDR FDEA201905020983](https://openairdocs.org/sdr/FDEA201905020983), May 2, 2019: WARNING SYSTEM. FALSE ACTIVATION. RECEIVED LEVEL 1 ALERT "AIR SYS 2 OFF". 2 MINUTES LATER RECEIVED LEVEL 3 ALERT "AIR MANF 2 FAIL". RAN QRH. LEVEL 3 ALERT EXTINGUISHED WHEN NR 2 THROTTLE PULLED 
- [SDR FDEA201812270126](https://openairdocs.org/sdr/FDEA201812270126), Dec 27, 2018: STRINGER. DAMAGED. LT STA.1156 HAS AN OVERSIZE HOLE REF PART # ARB0323-1 REPAIR WILL BE REPAIRED ON E.A. 8-5310-T0344334 REPAIRED PER EA#8-5310-T0344334 FUSELAGE-MAINFRAME-STA.115
- [SDR FDEA201812263609](https://openairdocs.org/sdr/FDEA201812263609), Dec 26, 2018: SUPPORT. CORRODED. VERTICAL STAB, BOTTOM SUPPORT BRACE FOR PANEL 374FR IS CORRODED. REPLACED BOTTOM SUPPORT WITH NEW SERVICEABLE SUPPORT ANGLE PER MD-10 SRM 51- 31-01 VOL. 2. AND 
- [SDR FDEA2018121083483](https://openairdocs.org/sdr/FDEA2018121083483), Dec 8, 2018: SKIN. DAMAGED. L/H WING, #3 SPOILER, UPPER SURFACE AT STA. XOSP3 609, HAS AN EXISTING SKIN DOUBLER, APPROX. 4' DIA. REPAIRE PER SRM 57-00-01 FIG.4 SHT.1
- [SDR FDEA201811303403](https://openairdocs.org/sdr/FDEA201811303403), Nov 30, 2018: SKIN. DAMAGED. [R/H WING, I/B FLAP HAS DAMAGE ON TOP OF SKIN BY STA. XIFH 155., 2018-11-30] REPAIRED THE R/H WING, I/B FLAP UPPER SURFACE PER SRM 57-10-00 FIG 85 SHEET 4 VOL 1
- [SDR FDEA201811303399](https://openairdocs.org/sdr/FDEA201811303399), Nov 30, 2018: SKIN. DAMAGED. [RH INBD FLAP DAMAGED ON TOP SIDE OF FLAP., 2018-11-30] REPAIRED DAMAGE ON THE R/H FLAP, UPPER SURFACE PER SRM 57-10-00 FIG 85 SHEET 4 VOL1 & TRACKING EA # 8-57
- [SDR FDEA201811303397](https://openairdocs.org/sdr/FDEA201811303397), Nov 30, 2018: SKIN. GOUGED. [R/H WING I/B FLAP...TOP FWD SURFACE..APPROX C/L....WEAR MARK/GOUGE ON FLAP SKIN... REFERENCE...SNRM #203, 2018-11-30] REPAIRED THE DAMAGE PER SRM 57-10-00 FIG 
- [SDR FDEA201811280209](https://openairdocs.org/sdr/FDEA201811280209), Nov 28, 2018: SPAR. OUT OF ALIGNMENT. RT HORIZ SPAR CAP BARREL NUT BOLT HOLE IS MISALIGNED. REPAIRED PER EA 8-5510-T0343409 "HORIZONTAL STABILIZER- RT UPPER REAR SPAR REPAIR"
- [SDR FDEA201811270125](https://openairdocs.org/sdr/FDEA201811270125), Nov 27, 2018: FITTING. CRACKED. LT STA. 1156 FWD HOZ LEG HAS 4 EA. OPEN HOLES BETWEEN LONGERON 38L-39L IN SKIN AND AYB7000-1 FITTING AND 1 EA. OPEN HOLE ON AFT HORZ LEG IN SKIN HAVE CRACK INDI
- [SDR FDEA201811273417](https://openairdocs.org/sdr/FDEA201811273417), Nov 27, 2018: FLOOR SUPPORT. CORRODED. MAIN DECK FLOOR SUPPORT ATTACHED ANGLE CLIP IS SHOW SIGN OF CORROSION AT STATION 1972 RBL40. INSTALLED NEW FLOOR SUPPORT AGA7091-50 PER DWG AGA7091 REF SRM 51-3
- [SDR FDEA201811273416](https://openairdocs.org/sdr/FDEA201811273416), Nov 27, 2018: FLOOR SUPPORT. CORRODED. MAIN DECK FLOOR SUPPORT ATTACHED ANGLE CLIP IS SHOW SIGN OF CORROSION AT STATION 1972 LBL40. INSTALLED NEW FLOOR SUPPORT AGA7091-49 PER DWG AGA7091 REF SRM 51-3
- [SDR FDEA201811153476](https://openairdocs.org/sdr/FDEA201811153476), Nov 15, 2018: SKIN. CRACKED. RT WING LE INTERNAL STRUCTURE BEADED DOUBLER CRACKED, THREE (3) PLACES, LOCATION APPROX XORS 817, OUTBD OF NR 14 SLAT TRACK, ACCESS THROUGH FUEL VALVE PANEL 626
- [SDR FDEA201811143429](https://openairdocs.org/sdr/FDEA201811143429), Nov 14, 2018: FLOOR PANEL. DELAMINATED. MAIN CABIN, STA 435 - 475 FLOOR IS SPONGY AND DELAMINATED. FABRICATED NEW FLOOR PANEL 225BF, STA 435 TO STA 475 REF DWG SRZ-25-005.
- [SDR FDEA201811133430](https://openairdocs.org/sdr/FDEA201811133430), Nov 13, 2018: FLOOR SUPPORT. CRACKED. MAIN DECK FLOOR SUPPORT ATTACHED ANGLE CLIP IS SHOW SIGN OF CRACKED AT STA 455 RBL 10. REPLACED FLOOR SUPPORT ABA7423-1 PER SRM 51-31-01 VOL 2, AND DWG ABA7423.
- [SDR FDEA201811113437](https://openairdocs.org/sdr/FDEA201811113437), Nov 11, 2018: FITTING. CRACKED. RIGHT WING LEADING EDGE STA 1159 AT APPROX LONG 30 T-CAP ANGLE FITTING IS CRACKED MARKED 23 STATION 1159 RBL. LONG 30 AT LEADING EDGE REMOVED AND REPLACED T-CAP
- [SDR FDEA201811113415](https://openairdocs.org/sdr/FDEA201811113415), Nov 11, 2018: SEAT TRACK. CORRODED. MAIN CARGO COMPT CENTER FLOOR SUPPORT APPROX STA 392 TO 435, X=0. FLOOR SUPPORT SHOWS CORROSION. INSTALLED NEW SEAT TRACK PER SRM 51-31-01 VOL 2 AND DAC DWG NBA
- [SDR FDEA201811113412](https://openairdocs.org/sdr/FDEA201811113412), Nov 11, 2018: SEAT TRACK. CORRODED. MAIN CARGO COMPT APPROX STA 455 TO 475, X=-47.50 SEAT TRACK CHANNEL CORRODED. INSTALLED SEAT TRACK PER SRM 51-31-01 VOL 2 AND DRAWING NBA6018.
- [SDR FDEA201811113391](https://openairdocs.org/sdr/FDEA201811113391), Nov 11, 2018: SEAT TRACK. CORRODED. MAIN CARGO COMPT: APPROX STA 435 TO 455, X=-8.50 SEAT TRACK SHOWS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT SEAT TRACK IN MAIN CARGO COMPT APPROX STATION 43
- [SDR FDEA201811113387](https://openairdocs.org/sdr/FDEA201811113387), Nov 11, 2018: SEAT TRACK. CORRODED. MAIN CARGO COMPT: APPROX STA 435 TO 455, X=8.50 FLOOR SUPPORT SEAT TRACK SHOWS CORROSION. REMOVED AND REPLACED FLOOR SUPPORT SEAT TRACK IN MAIN CARGO COMPT APPR
- [SDR FDEA201811093386](https://openairdocs.org/sdr/FDEA201811093386), Nov 9, 2018: FLOOR PANEL. DAMAGED. MAIN DECK- FOUND EXISTENT FLOOR PANEL REPAIR IS COMING OFF AT STA 775 LBL 100. FABRICATED NEW FLOOR PNL AT STA 775 LBL 100 REF DWG SRZ-25-005.
- [SDR FDEA201811093271](https://openairdocs.org/sdr/FDEA201811093271), Nov 9, 2018: SKIN. NONE. #3 AIR COND. COMPT. DOOR, STA. 496-525, HAS AN EXISTING DOUBLER ON TOP EDGE. EXISTING MAJOR REPAIR PREVIOUSLY INSTALLED PER SRM 52-10-00 FIG. 2, SHT. 2, VOL. 1.
- [SDR FDEA201811093171](https://openairdocs.org/sdr/FDEA201811093171), Nov 9, 2018: FLOORBOARD. CORRODED. MAIN CABIN FLOORBOARD SHOWS EVIDENCE OF CORROSION, STA 435 TO STA 475 AT RBL 17 AND NEEDS TO BE REPLACED. REMOVED AND REPLACED FLOORBOARD IN REF TO DWG SRZ-25-0
- [SDR FDEA201811093169](https://openairdocs.org/sdr/FDEA201811093169), Nov 9, 2018: FLOORBOARD. CORRODED. MAIN CABIN FLOORBOARD DELAMINATED, STA 475 TO STA 495 AT RBL 17 AND NEEDS TO BE REPLACED. REMOVED AND REPLACED FLOORBOARD IN REF TO DWG SRZ-25-005.
- [SDR FDEA2018110983129](https://openairdocs.org/sdr/FDEA2018110983129), Nov 8, 2018: SKIN. CRACKED. R/H FUSELAGE SKIN AT STA. 1156 HAS A .400 IN. CRACK AT THE AFT FASTENER HOLE COMMON TO THE TEE CAP (2 FASTENERS ABOVE LONGERON 39R) PROPAGATING AFT TO THE EDGE 
- [SDR FDEA201811073377](https://openairdocs.org/sdr/FDEA201811073377), Nov 7, 2018: SEAT TRACK. WORN. MAIN DECK COMPT STA1260 48RBL SEAT TRACK LOBE WORN. REMOVED AND REPLACED SEAT TRACK ON MAIN DECK COMPT AT EXISTING SPLICE FROM APPROX STATION 1246 TO STATION 13
- [SDR FDEA201811073317](https://openairdocs.org/sdr/FDEA201811073317), Nov 7, 2018: SEAT TRACK. WORN. MAIN DECK COMPT STA1260 48LBL SEAT TRACK LOBE WORN (MARKED) INSTALLED AND SEAL NEW SEAT TRACK REF. SRM 53-70-00 FIG. 1 VOL. 1 AND SRM 51-31-01 VOL. 2.
- [SDR FDEA2018111973303](https://openairdocs.org/sdr/FDEA2018111973303), Nov 7, 2018: SEAT TRACK. WORN. MAIN DECK COMPT STA1541 22RBL SEAT TRACK LOBE WORN (MARKED) REPLACED DAMAGED SECTION OF SEAT TRACK FROM STATION 1541 TO STATION 1581. REFERENCE SRM 53-70-00 FIG
- [SDR FDEA201811073186](https://openairdocs.org/sdr/FDEA201811073186), Nov 7, 2018: FLOOR SUPPORT. CORRODED. MAIN DECK STA 735 LBL 28-48 FLOOR BOARD SUPPORT HAS CORROSION DAMAGE. REMOVE AN REPLACED NEWLY FABRICATED FLOOR BOARD SUPPORT ACA7417-17 STA 735 LBL 28-48. REF 
- [SDR FDEA201811073118](https://openairdocs.org/sdr/FDEA201811073118), Nov 7, 2018: SPAR CAP. CRACKED. RT HORIZONTAL STAB, OUTER SECTION UPPER AFT SPAR CAP HAS A CRACK APPROX .400" LONG ORIGINATING AFT OF AFT BARREL NUT HOLE CONTINUING TO AFT EDGE OF SPAR CAP. RE
- [SDR FDEA2018111963306](https://openairdocs.org/sdr/FDEA2018111963306), Nov 6, 2018: SKIN. CORRODED. RH WING UPPER SURFACE APPROX XORS 264 STRINGER 12 - CORROSION AROUND FASTENER. REMOVED CORROSION AT APPROX XORS264 STRINGER 12 RH WING UPPER SURFACE AROUND FAST
- [SDR FDEA201711183272](https://openairdocs.org/sdr/FDEA201711183272), Nov 18, 2017: APU. SMOKE. APU SMOKE. APU SHUTDOWN (AUTO). OBSERVED SMOKE FROM APU. DEPLOYED FIRE AGENT TO APU.
- [SDR FDEA201611013784](https://openairdocs.org/sdr/FDEA201611013784), Nov 1, 2016: TEE FITTING. CRACKED. BS 1156 BULKHEAD TEE FITTING VERTICAL LEG CRACKED ABOVE LONGERON 39L. REPAIRED IAW EA 8-5310-T0328855
- [SDR FDEA201610193663](https://openairdocs.org/sdr/FDEA201610193663), Oct 19, 2016: WEB. CRACKED. NR 3 PYLON UPPER WEB OTBD SIDE HAS A CRACK INDICATION. REPAIRED IAW EA 8-5400-T0329061.
- [SDR FDEA201610193662](https://openairdocs.org/sdr/FDEA201610193662), Oct 19, 2016: FITTING. CRACKED. NR 3 PYLON AFT BULKHEAD FITTING HAS A CRACK INDICATION AT THE FOURTH HOLE FROM OTBD SIDE. REPAIRED IAW EA 8-5400-T0329061.
- [SDR FDEA201610193661](https://openairdocs.org/sdr/FDEA201610193661), Oct 19, 2016: BOLT. LOOSE. NR 3 PYLON, UPPER AFT SECTION OF SPAR WEB, HAS 15 LOOSE BOLTS. REAMED HOLES TO FIRST OVERSIZE AND INSTALLED B/P BOLTS IAW SRM 54-20-00 F. 27, VOL I
- [SDR FDEA201610183652](https://openairdocs.org/sdr/FDEA201610183652), Oct 18, 2016: WEB. CRACKED. NR 3 PYLON, UPPERWEB , FOUND CRACK APPROX 1.75 INCH FROM EDGE OF UPPER SPAR WEB THRU 1 FASTENER HOLE TERMINATING AT I/B FASTENER HOLE OF AUB7031-11 DOUBLER. R&R
- [SDR FDEA201610173646](https://openairdocs.org/sdr/FDEA201610173646), Oct 17, 2016: SKIN. CRACKED. RT WING STAT TRACK NR 14 CUT OUT AFT O/B CORNER HAS A .300 IN CRACK. INSTALLED A DOUBLER PER SRM 57-10-00 FIG 68 VOL 1.
- [SDR FDEA201610173645](https://openairdocs.org/sdr/FDEA201610173645), Oct 17, 2016: SKIN. CRACKED. RT WING STAT TRACK NR 14 CUT OUT AFT O/B CORNER HAS A .300 IN CRACK. INSTALLED A DOUBLER PER SRM 57-10-00 FIG 68 VOL 1.
- [SDR FDEA201610133609](https://openairdocs.org/sdr/FDEA201610133609), Oct 13, 2016: SKIN. WORN. RT WING LOWER LEADING EDGE, AREAS COMMON TO PYLON, SKIN IS WORN. INSTALLED REPAIR DOUBLER IAW SRM 57-10-00 FIG 87.
- [SDR FDEA201610123548](https://openairdocs.org/sdr/FDEA201610123548), Oct 12, 2016: SKIN. DELAMINATED. RIGHT WING INBD FLAP O/B HINGE PANEL 641CR DELAMINATED. REPAIRED THE DAMAGE IAW SRM 51-71-00 VOL II
- [SDR FDEA201610113544](https://openairdocs.org/sdr/FDEA201610113544), Oct 11, 2016: SKIN. DENTED. RIGHT ELEVATOR LOWER SURFACE CREASED. CUT OUT DAMAGE AND INSTALLED REPAIR DOUBLER IAW SRM 55-10-00 FIG. 8 VOL. I
- [SDR FDEA201610043455](https://openairdocs.org/sdr/FDEA201610043455), Oct 4, 2016: FLOORBEAM. CORRODED. AFT CARGO BAY BS 1841 FLOORBEAM HAS SEVERAL AREAS WITH CORROSION. LBL TO RBL 18. REPAIRED IAW DWG AGA3874
- [SDR FDEA201610033647](https://openairdocs.org/sdr/FDEA201610033647), Oct 3, 2016: ACOUSTIC PANEL. CRACKED. NR 1 ENGINE NOSE COWL AT 12 O'CLOCK POSITION BETWEEN NOSE COWL LEADING EDGE AND ACOUSTIC PANEL HAS A CRACK. INSTALLED REPAIR DOUBLER PER SRM 54-11-00 FIG 1A.
- [SDR FDEA201610033528](https://openairdocs.org/sdr/FDEA201610033528), Oct 3, 2016: ROLLER TRAY. CRACKED. FWD CARGO ROLLER TRAY AT BS 920 DOOR ENTRY AREA CRACKED. REPLACED THE ROLLER TRAY IAW NDJ6030.
- [SDR FDEA201610023428](https://openairdocs.org/sdr/FDEA201610023428), Oct 2, 2016: TEE FITTING. CRACKED. RT STA 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43R HAS A .5 IN CRACK AT THE LOWER FASTENER. REPAIRED IAW EA 8-5310-T0328704.
- [SDR FDEA201610023427](https://openairdocs.org/sdr/FDEA201610023427), Oct 2, 2016: TEE FITTING. CRACKED. RT STA 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 39R HAS A .5 IN CRACK AT THE UPPER AND LWR FASTENER. REPAIRED IAW EA 8-5310-T0328704.
- [SDR FDEA201610023426](https://openairdocs.org/sdr/FDEA201610023426), Oct 2, 2016: TEE FITTING. CRACKED. LEFT BS 595 BULKHEAD TEE CAP AT LONGERON 39L HAS A .5 IN CRACK AT THE LWR FASTENER. REPAIRED IAW EA 8-5310-T0328709.
- [SDR FDEA201610013904](https://openairdocs.org/sdr/FDEA201610013904), Oct 1, 2016: BOLT. SHEARED. NR 3 PYLON UPPER WEB SURFACE OTBD SIDE, ALONG THE EDGE HAS A SHEARED BOLT. REPAIRED IAW EA 8-5400-T0329061 AND SRM 54-20-00 FIG. 27, VOL. I.

All 235: https://openairdocs.org/deregistered/N10060-2024-03-02/reports.md

## Other aircraft with N10060

- [Cancelled 1984-06-08](https://openairdocs.org/deregistered/N10060-1984-06-08): Sikorsky S62A, S/N 62081. Administratively canceled. Owner: [Briles Wing & Helicopter Inc](https://openairdocs.org/faa-owner/BRILES%20WING%20%26%20HELICOPTER%20INC), [Medford, OR](https://openairdocs.org/faa-place/OR/Medford)

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