# N68058: 1972 Mcdonnell-Douglas DC-10-10F, registration cancelled 2013-03-08

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: March 8, 2013
- Status when cancelled: Valid registration
- Airframe: [Mcdonnell-Douglas DC-10-10F](https://openairdocs.org/model/mcdonnell-douglas-dc-10-10f) (registry code 3022111)
- 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: 46705
- Year built: 1972
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 22, 1991
- Certificate issued: June 30, 2008
- Last registry action: July 18, 2011
- Mode S code: A9065F
- 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/N68058
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=68058
- Page: https://openairdocs.org/deregistered/N68058-2013-03-08

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

## Service difficulty reports (58, newest 50)

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

- [SDR 07FDEA04612](https://openairdocs.org/sdr/07FDEA04612), Oct 16, 2007: SEAT TRACK. CORRODED. SEAT TRACK (EQUIPMENT TIE DOWN TRACK) AT APPROX BL 91 LT AND BETWEEN FS 392 AND 25 HAS CORROSION. REMOVED, FAB'D AND INSTALLED SEAT TRACK IAW SRM 53-70-00 FIG 5
- [SDR 07FDEA04611](https://openairdocs.org/sdr/07FDEA04611), Oct 16, 2007: SEAT TRACK. CORRODED. MAIN CABIN STA 880, RBL 76 SEAT TRACK CORRODED. REMOVED, FAB'D AND INSTALLED SEAT TRACK IAW DC/MD 10 SRM 51-31-01 VOL II PAGE 1 AND DAC DRAWING AFA 7433 REV AD.
- [SDR 07FDEA04570](https://openairdocs.org/sdr/07FDEA04570), Oct 11, 2007: SEAT TRACK. CORRODED. CORROSION ON SEAT TRACK BETWEEN STA 420 TO STA 448 RBL 27 REMOVED AND REPLACED SEAT TRACK ABA7684-507, STA 421.5 TO STA 484.7, RBL 27.5, IN REF TO DC10/MD10 SRM
- [SDR 07FDEA04566](https://openairdocs.org/sdr/07FDEA04566), Oct 10, 2007: SEAT TRACK. GOUGED. MAIN CABIN, STN 1360 - STN 1364, RBL 46, "SEAT TRACK GOUGED" SCALLOPS ELONGATED CHECKED LIMITS, BLENDOUT AREA IS .510 OUT OF .500 MAX OUT OF LIMITS IAW DC/MD-10
- [SDR 07FDEA04565](https://openairdocs.org/sdr/07FDEA04565), Oct 10, 2007: SEAT TRACK. CORRODED. CABIN/CORROSION ON SEAT TRACK (EQUIPMENT TIE DOWN TRACK) AT BL 78 LT AND BETWEEN FS 374 AND 420 REMOVED CORROSION IAW MD/DC-10 SRM 53-70-00 FIG 5 SHEET 2 VOL I 
- [SDR 07FDEA04564](https://openairdocs.org/sdr/07FDEA04564), Oct 10, 2007: SEAT TRACK. GOUGED. MAIN CABIN, STN 1358, RBL 46, "SEAT TRACK GOUGED," SCALLOPS ELONGATED CHECKED LIMITS: REMAINING MATERIAL IS .170, .260 MIN REQ OUT OF LIMITS IAW DC/MD-10 SRM 53
- [SDR 07FDEA04563](https://openairdocs.org/sdr/07FDEA04563), Oct 10, 2007: FRAME. CHAFED. NR 1 AIR CONDITIONING COMPT BYPASS VALVE PUSH-PULL CABLE CHAFING AGAINST FRAME TOP CHORD STA 588. REPAIRED FRAME IAW EA 8-5310-10920B, FUSELAGE-AIR CONDITIONING
- [SDR 07FDEA02662](https://openairdocs.org/sdr/07FDEA02662), Jul 29, 2007: SUPPORT BRACKET. CRACKED. RT WING O/B FLAP, I/B HINGE, O/B ATTACH BRACE CRACKED AT REAR SPAR. REMOVED AND REPLACED CRACKED SUPPORT ARB0029-506. REF SRM 57-00-01.
- [SDR 07FDEA02436](https://openairdocs.org/sdr/07FDEA02436), Jul 5, 2007: INU. FAILED. NR 1 INU FAILED AFTER PUSH BACK. REPLACED NR 1 INU GRD, OPS CK NORMAL MM 34-43-04-2, OFF MFG 463001-6130-0413, POS 1 SRL 0341, TAG 0357A9, ON MFG 463001-6130-04
- [SDR 06FDEA1942](https://openairdocs.org/sdr/06FDEA1942), May 17, 2006: FILLER. CRACKED. NR2 ENGINE SAIL TAIL FILLER AT EXHAUST NOZZLE HAS NUMEROUS CRACKS AS MARKED, 2 DEEP CHAF MARKS AND RIGHT FWD CORNER IS BROKEN. REMOVED SAIL TAIL FILLER IAW SRM 
- [SDR 06FDEA1940](https://openairdocs.org/sdr/06FDEA1940), May 17, 2006: WEDGE. CRACKED. LT WING I/B FLAP UPPER SKIN HAS A CRACK NEAR O/B END. CLEANED AREA IAW M/M 12-22-02-7, HFEC INSP PER NTM 51-00-00 CRACK FOUND 3 EA. REMOVED T/E SECTION IAW SRM 
- [SDR 06FDEA0920](https://openairdocs.org/sdr/06FDEA0920), Mar 2, 2006: CONNECTOR. DAMAGED. AT FL 290 A/C DOOR LIGHT ILLUMINATED ON SECOND OFFICERS PANEL. CREW RAN RED TAB CHECKLIST AND LANDED AT MEMPHIS. DOOR LIGHT EXT DESCENDING THROUGH 16,000 FT. AI
- [SDR 05FDEA03180](https://openairdocs.org/sdr/05FDEA03180), Sep 28, 2005: WARNING LIGHT. ILLUMINATED. WHILE IN FLIGHT CLIMBING-OUT OF 15000 FT, THE NR 2 THRUST REVERSER UNLOCK LIGHT WAS FLICKERING ON AND OFF. THRUST REV CHECKLIST WAS COMPLETED AND RETURN AND LAN
- [SDR 05FDEA00504](https://openairdocs.org/sdr/05FDEA00504), Mar 10, 2005: SKIN. TORN. INSPECTED DAMAGED AREA, FOUND A LARGE TEAR IN SKIN APPROX 16 X 6 INCH FWD OF FR959 L AND ABOVE STRINGER 41L. STOP DRILLED TEARS AND CUT OUT DAMAGE PER DC10 SRM 
- [SDR 04FDEA03388](https://openairdocs.org/sdr/04FDEA03388), Dec 7, 2004: CONNECTOR. DIRTY. AFTER TAKEOFF R1 DOOR LIGHT CAME ON AND WOULD NOT PRESSURIZE. ATB TO MEM. MEL 52-04-02: FWD CABIN DOOR CAUTION LIGHT INOPERATIVE. CHECKED WIRING ON R-1 DOOR, CL
- [SDR 04FDEA02886](https://openairdocs.org/sdr/04FDEA02886), Oct 7, 2004: LONGERON. CORRODED. LOWER FUSELAGE UNDERWING LONGERON 48R IS CORRODED FROM STATION 1368 TO STATION 1521. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS IAW DC10 SRM 53-00-01 VOL I PA
- [SDR 04FDEA02885](https://openairdocs.org/sdr/04FDEA02885), Oct 7, 2004: LONGERON. CORRODED. LOWER FUSELAGE UNDERWING LONGERON 49R IS CORRODED FROM STATION 1368 TO 1521. REMOVED CORROSION LONGERON 49R, FOUND TO BE OUT OF LIMITS. REMOVED LONGERON 49R FRO
- [SDR 04FDEA02884](https://openairdocs.org/sdr/04FDEA02884), Oct 7, 2004: FITTING. MIGRATED. LEFT HORIZONTAL STABILIZER INBOARD TRAILING EDGE, STABILIZER TO STABILIZER BOX SAFETY LINK, OUTBOARD ATTACH CLEVIS BUSHING WORN AND MIGRATED THROUGH STABILIZER 
- [SDR 04FDEA02883](https://openairdocs.org/sdr/04FDEA02883), Oct 7, 2004: PANEL. DELAMINATED. LEFT HORIZONTAL STABILIZER 1 EACH PANEL AT STATION XE122 COMPOSITE PANEL AT AFT SPAR TOP SIDE IS DELAMINATED. REPAIRED PANEL BY FABRICATING AND BONDING NEW OUTE
- [SDR 04FDEA02859](https://openairdocs.org/sdr/04FDEA02859), Oct 1, 2004: PANEL. DELAMINATED. PANEL 66CT HAS SEVERAL AREAS OF DELAMINATION. REPAIRED BY REMOVING DAMAGE, FABRICATING AND BONDING NEW SKIN, CORE AND DOUBLERS IAW DAC DWG ARC0627 AND EA 8-5710
- [SDR 04FDEA02856](https://openairdocs.org/sdr/04FDEA02856), Oct 1, 2004: STATIC PORT. FAILED. LEFT PRIMARY STATIC PORT FAILS WAVINESS CHECK. REMOVED LEFT HAND STATIC PORT AND REPLACED HEAT SINK IAW FEDEX DC10 MM 34-11-01-2. REMOVED STATIC PORT AND BLENDE
- [SDR 04FDEA02855](https://openairdocs.org/sdr/04FDEA02855), Oct 1, 2004: VENTILATOR PANEL. CRACKED. NR 3 PYLON TOP PANEL 487DR HAS THREE AREAS OF CRACKS. REPAIRED VENTILATOR ASSY P/N AUB7054-501 IAW FEDEX EA 8-5480-77611. LOCATED AND DRILLED VENTILATOR ASSY IA
- [SDR 04FDEA02861](https://openairdocs.org/sdr/04FDEA02861), Oct 1, 2004: SKIN PANEL. CORRODED. LOWER FUSELAGE CENTER SKIN REQUIRES REMOVAL DUE TO CORROSION FROM STATION 1350 TO 1521, L48L TO L48R. COMPLIED WITH FEDEX EA 8-5330-77624, SKIN SPLICE REPAIR AT
- [SDR 04FDEA02819](https://openairdocs.org/sdr/04FDEA02819), Sep 27, 2004: PANEL. DELAMINATED. PANEL 541EB HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL BY FABRICATING AND BONDING NEW INNER SKIN, OUTERSKIN, DOUBLER AND CORE IAW DC10 DRAWING ARC0264 AN
- [SDR 04FDEA02818](https://openairdocs.org/sdr/04FDEA02818), Sep 27, 2004: TUBE. CRACKED. LEFT WING LEADING EDGE UPPER PYLON FUEL SAXAPHONE LINE IS CRACKED AT MOUNTING POINT. REMOVED, REPAIRED, REINSTALLED FUEL LINE IAW FEDEX EA 8-2822-77635.
- [SDR 04FDEA02823](https://openairdocs.org/sdr/04FDEA02823), Sep 27, 2004: PANEL. DELAMINATED. PANEL 641CR HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77617. REFERENCE NON ROUTINE N00169.
- [SDR 04FDEA02822](https://openairdocs.org/sdr/04FDEA02822), Sep 27, 2004: HINGE. CORRODED. LEFT HAND INBOARD FLAP OUTBOARD SUPPORT PIVOT ATTACH POINT OUTBOARD BORE CORRODED. CORROSION EXCEEDS CMM 57-52-01 LIMITS. REPAIRED IAW FEDEX EA 8-5750-77622. RE
- [SDR 04FDEA02821](https://openairdocs.org/sdr/04FDEA02821), Sep 27, 2004: FRAME. CORRODED. MAIN CABIN FUSELAGE STATION 1821 HAS CORROSION AT LOWER FRAME END, AS SEEN FROM BULK PIT UPPER TORQUE BOX. CORROSION EXCEEDS LIMITS IAW DC10 SRM 53-00-01 VOL 1.
- [SDR 04FDEA02820](https://openairdocs.org/sdr/04FDEA02820), Sep 27, 2004: SKIN. CORRODED. LOWER FUSELAGE CENTER SKIN REQUIRES REMOVAL DUE TO CORROSION, FROM STATION 1350 TO 1521 L48L TO L48R. COMPLIED WITH FEDEX EA 8-5330-77624, SKIN SPLICE REPAIR AT
- [SDR 04FDEA02832](https://openairdocs.org/sdr/04FDEA02832), Sep 27, 2004: PANEL. CORRODED. RIGHT HORIZONTAL STABILIZER PANEL 344JB HAS CORROSION ON NUMEROUS SPOTS ON INTERIOR SURFACE. REPAIRED PANEL BY FABRICATING AND BONDING NEW OUTER SKIN, INNER SKI
- [SDR 04FDEA02831](https://openairdocs.org/sdr/04FDEA02831), Sep 27, 2004: LINER. PUNCTURED. AFT PIT DOOR JAMB AFT SIDE THRESHOLD PANEL HAS HOLE PUNCTURES ON IT. WELD REPAIRED IAW FEDEX EA 8-5320-77632, REFERENCE NON-ROUTINE.
- [SDR 04FDEA02830](https://openairdocs.org/sdr/04FDEA02830), Sep 27, 2004: BEAM. DAMAGED. DURING REMOVAL OF ZERT FITTING BUSHING ON LEFT HAND MAIN LANDING GEAR TRUCK BEAM, FOUND BUSHING TO BE THREADED BUSHINGS, NOT PRESS BUSHING. INSTALLED NEW ZERK F
- [SDR 04FDEA02829](https://openairdocs.org/sdr/04FDEA02829), Sep 27, 2004: PANEL. DELAMINATED. PANEL 541CR HAS MANY AREA OF DELAMINATION. REPAIRED PANEL 541CR BY FABRICATING AND BONDING NEW SKINS, DOUBLERS AND CORE IAW TPS 1001 REV E, DAC DWG ARC2906 AND 
- [SDR 04FDEA02828](https://openairdocs.org/sdr/04FDEA02828), Sep 27, 2004: PANEL. DELAMINATED. LEFT HORIZONTAL STABILIZER, 1 EACH PANEL AT STA XE203.5, COMPOSITE PANEL AT AFT SPAR TOP DELAMINATED. REPAIRED BY FABRICATION AND BONDING NEW OUTER AND INNER SK
- [SDR 04FDEA02827](https://openairdocs.org/sdr/04FDEA02827), Sep 27, 2004: PANEL. CORRODED. RIGHT HORIZONTAL STABILIZER PANEL 344JB HAS CORROSION ON NUMEROUS SPOTS ON INTERIOR SURFACE. REPAIRED PANEL IAW FEDEX EA 8-5510-81466.
- [SDR 04FDEA02826](https://openairdocs.org/sdr/04FDEA02826), Sep 27, 2004: PANEL. DELAMINATED. RIGHT WING TRAILING EDGE PANEL 641BB DELAMINATED. REPAIRED PANEL IAW FEDEX EA 8-5710-77621, REFERENCE NON ROUTINE N00419.
- [SDR 04FDEA02825](https://openairdocs.org/sdr/04FDEA02825), Sep 27, 2004: PANEL. DELAMINATED. PANEL 636HL HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77614. REFERENCE NON ROUTINE N00323.
- [SDR 04FDEA02824](https://openairdocs.org/sdr/04FDEA02824), Sep 27, 2004: PANEL. DELAMINATED. PANEL 541EB HAS SEVERAL AREAS OF DELAMINATION. REPAIRED PANEL IAW FEDEX EA 8-5710-77620, REFERENCE NON ROUTINE N00125.
- [SDR 04FDEA02637](https://openairdocs.org/sdr/04FDEA02637), Sep 4, 2004: SKIN. DAMAGED. LEFT WING TRAILING EDGE SKIN AFT OF MAIN LANDING GEAR LOWER SURFACE REQUIRES FABRICATION. FABRICATED DOUBLER AND SKIN IAW DAC DWG ARC0468, BONDED SKIN AND DOUBL
- [SDR 04FDEA02644](https://openairdocs.org/sdr/04FDEA02644), Sep 4, 2004: PAN. GOUGED. NR 2 ENGINE RT FAN COWL INTERIOR HAS RUBBING APPROXIMATELY 8 INCHES ABOVE CENTER U-BOLT. REMOVED CENTER U-BOLT FITTING TO FOM. REMOVED DAMAGED SECTION OF PAN IA
- [SDR 04FDEA02643](https://openairdocs.org/sdr/04FDEA02643), Sep 4, 2004: PAN. GOUGED. NR 2 ENGINE RIGHT HAND FAN COWL INTERIOR HAS RUBBING APPROXIMATELY 8 INCHES ABOVE CENTER "U" BOLT. REMOVED CENTER "U" BOLT FITTING TO FOM. REMOVED DAMAGED SECTI
- [SDR 04FDEA02642](https://openairdocs.org/sdr/04FDEA02642), Sep 4, 2004: PANEL. DELAMINATED. PANEL 636 DL HAS SEVERAL AREA OF DELAMINATION. REPAIRED PANEL P/N ARC0566-2 BY FABRICATING AND BONDING NEW SKIN, DOUBLERS AND CORE IAW FEDEX EA 8-5710-77513, DA
- [SDR 04FDEA02638](https://openairdocs.org/sdr/04FDEA02638), Sep 4, 2004: PANEL. DELAMINATED. RIGHT WING TRAILING EDGE PANEL 641 EB HAS MANY AREA OF DELAMINATION. REPAIRED RIGHT WING TRAILING EDGE PANE 641EB BY FABRICATING AND BONDING INNER AND OUTER SKI
- [SDR 04FDEA02538](https://openairdocs.org/sdr/04FDEA02538), Aug 21, 2004: FLOORBEAM. CORRODED. AFT PIT, FLOORBEAM CAP BEAM AT STATION 1887.0 HAS EXFOLIATION. REMOVED FLOORBEAM IAW SRM 51-33-01 VOL II. INSTALLED NEW FLOORBEAM AGA 3849-15, (FABRICATED ON NO
- [SDR 04FDEA02491](https://openairdocs.org/sdr/04FDEA02491), Aug 17, 2004: DUCT. GOUGED. SEVERAL GOUGES ON FORWARD COMPARTMENT COOLING DUCT INSIDE NR 1 OUTBOARD THRUST REVERSER AT NR 1 ENGINE, (NR 1 OUTBOARD THRUST REVERSER UPPER COOLING DUCT). REMO
- [SDR 04FDEA02484](https://openairdocs.org/sdr/04FDEA02484), Aug 16, 2004: SKIN. DAMAGED. RIGHT HAND PRIMARY STATIC PORT HAS EXTERNAL DOUBLER WITHIN 18 INCHES OF CONTROLLED AREA AT FOUR O'CLOCK POSITION AT FUSELAGE STATION 869 AT LONGERON 48 RIGHT. R
- [SDR 04FDEA02348](https://openairdocs.org/sdr/04FDEA02348), Aug 2, 2004: FITTING. CORRODED. LOWER SFT WING TO CENTER BOX ATTACH SKI FITTING IS EXFOILATED. RIGHT WHEEL WELL STATION 1341 TO 1360 AT XCW 118. REMOVED ATTACHED STRUCTURE IAW DC10 SRM 51-33-0
- [SDR 04FDEA02347](https://openairdocs.org/sdr/04FDEA02347), Aug 2, 2004: FITTING. CRACKED. CRACKED FITTING, CENTER WING SECTION TO FUSELAGE SPLICE, STATION 1157, LEFT HAND SIDE AT LONGERON 37L, EXTERNAL FITTING. REMOVED DAMAGED FITTING IAW DC10 SRM 51
- [SDR 04FDEA02346](https://openairdocs.org/sdr/04FDEA02346), Aug 2, 2004: FITTING. CORRODED. CORROSION AT THE INTERIOR OF AFT CARGO DOOR UPPER BOX AT LONGERON 27L FITTING AND SEVERAL HARDWARE, STA 1787 TO STA 1841, LONGERON 27L, LBL 101.0 TO LBL 106.0. 
- [SDR 04FDEA02345](https://openairdocs.org/sdr/04FDEA02345), Aug 2, 2004: SKIN. CORRODED. LOWER FUSELAGE UNDER WING BARREL SKIN IS CORRODED FROM STATION 1368 TO 1288 FROM LONGERON 47R TO 52R. REMOVED CORROSION IAW DC10 SRM 51-21-01 VOL II. ORIGINAL T

All 58: https://openairdocs.org/deregistered/N68058-2013-03-08/reports.md

## NTSB investigations (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB MIA99LA220](https://openairdocs.org/ntsb/MIA99LA220), Aug 7, 1999: McDonnell Douglas DC-10-10F (N68058), Memphis, TN, substantial damage. Probable cause: The inadequate design by the airplane manufacturer for using bolts to secure the inboard trailing edge flap that are susceptible to stress corrosion cracking. Also, the stress corrosion cracking…

## 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.

- [Accident 19990807043899A](https://openairdocs.org/incident/19990807043899A), Aug 7, 1999: Doug DC1010F (N68058), Memphis, TN, No damage. (-23)No narrative given

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