# N374FE: 1972 Mcdonnell Douglas MD-10-10F, registration cancelled 2017-03-22 - Type: Cancelled registration (FAA registry, deregistered aircraft) - Cancelled: March 22, 2017 - 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: 46612 - Year built: 1972 - Type of aircraft: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 29, 2004 - Certificate issued: June 16, 1998 - Last registry action: February 16, 2017 - Mode S code: A44329 - Owner when cancelled: [Federal Express Corporation](https://openairdocs.org/faa-owner/FEDERAL%20EXPRESS%20CORPORATION) - 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/N374FE - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=374FE - Page: https://openairdocs.org/deregistered/N374FE-2017-03-22 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 (46) Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. - [SDR 08FDEA00738](https://openairdocs.org/sdr/08FDEA00738), Mar 5, 2008: REDUCER. LEAKING. HYD 3 ELEV OFF AND HYD 3 QTY LOW ALERT ANNUNCIATED. HYDRAULIC QUANTITY STABILIZED AT 3.9 GALLON. TIGHTENED "B" NUT UNION (REDUCER) ON RT MAIN LANDING GEAR SWIVE - [SDR 08FDEA00522](https://openairdocs.org/sdr/08FDEA00522), Feb 20, 2008: INTERCOSTAL. CORRODED. LOWER AFT CARGO COMPARTMENT CORROSION ON INTERCOSTAL BETWEEN STRINGERS 44 AND 45 LT AT FS 1781. FABRICATED NEW INTERCOSTAL PER DAC DAW AFA 3870 REV F AND INSTAL - [SDR 08FDEA00515](https://openairdocs.org/sdr/08FDEA00515), Feb 19, 2008: SKIN. CORRODED. CENTER WHEEL WELL LOWER SKIN HAS CORROSION FROM FS 1501 TO 1521 BETWEEN STR 50L TO51R. REMOVED, FABRICATED AND INSTALLED REPAIR PER E8-5330-113024" FUSELAGE-SKI - [SDR 08FDEA00450](https://openairdocs.org/sdr/08FDEA00450), Feb 15, 2008: WEB. CRACKED. CENTER CARGO COMP AT STA 1781 BELOW THE FLOOR AREA FROM L 52 - L 44 L WEB P/N AFA0154-5 1S CRACKED. FABRICATED NEW WEB PER REF. DAC DWG AFA 0154 REV. AT. INSTAL - [SDR 08FDEA00449](https://openairdocs.org/sdr/08FDEA00449), Feb 15, 2008: SKIN. CORRODED. CENTER WHEEL WELL LOWER INTERIOR SKIN HAS CORROSION BETWEEN STR 47 R AND STR 48 R FROM FS 1501 TO FS 1520. REMOVED, FABRICATED AND INSTALLED REPAIR PER E8-5330- - [SDR 08FDEA00451](https://openairdocs.org/sdr/08FDEA00451), Feb 15, 2008: SKIN. CORRODED. RIGHT WING UPPER TRAILING EDGE PANEL HAS CORROSION ON THE UPPER SURFACE, APPROXIMATELY XORS 345. REMOVED CORROSION; OUT OF LIMITS IAW 10 SRM 51-21-01, VOL II & - [SDR 08FDEA00339](https://openairdocs.org/sdr/08FDEA00339), Jan 31, 2008: SHEAR TIE. DAMAGED. FWD PIT AT STA 808 BETWEEN STR 42L AND STR 43L SHEARTIE HAS TOOL MARKS. FABBED NEW SHEARTIE IN REF TO FEDEX GMM 7-0-1001 AND DAC DWG RAM1470. REMOVED AND INSTAL - [SDR 08FDEA00328](https://openairdocs.org/sdr/08FDEA00328), Jan 30, 2008: SKIN. MISREPAIRED. FOUND REPAIR DOUBLER R/W O/B FLAP LOWER SKIN STA XOF 458. REPAIR REQUIRES EVALUATION FOR MAJOR/MINOR DETERMINATION AND IF REPAIR WAS ACCOMPLISHED USING FAA APPR - [SDR 08FDEA00329](https://openairdocs.org/sdr/08FDEA00329), Jan 30, 2008: SKIN. FAILED. LT I/B FLAP LOWER EXTERNAL SURFACE HAS ERRODED DENT FILLER. REMOVED FILLER,FABRICATED AND INSTALLED NEW REPAIR IAW MD/DC10 SRM 57-10-00 FIG 85 VOLI , 51-21-01 V - [SDR 08FDEA00315](https://openairdocs.org/sdr/08FDEA00315), Jan 28, 2008: ANGLE. CORRODED. LWW, SLANT BULKHEAD PANEL LWR ATTACH ANGLE CORRODED AT SEVERAL AREAS BET LT AND RT CORNERS, FWD AND AFT FACES, STA 1381. REMOVED CORROSION FOUND TO BE OUT OF LI - [SDR 08FDEA00313](https://openairdocs.org/sdr/08FDEA00313), Jan 28, 2008: SKIN. CORRODED. LWW, UPPER CTR TANK SKIN CORRODED, STA 1381, LBL 49. REMOVED AND REINSTALLED FASTENERS IAW SRM 51-31-01, VOL II. REMOVED CORROSION, FOUND TO BE WITHIN LIMITS IA - [SDR 08FDEA00311](https://openairdocs.org/sdr/08FDEA00311), Jan 28, 2008: SKIN. CORRODED. LWW, CTR TANK UPPER SKIN CORRODED STA 1381, LBL 76. REMOVED AND REINSTALLED FASTENERS IAW 51-31-01 VOL II. REMOVED CORROSION, FOUND TO BE WITHIN LIMITS IAW SRM - [SDR 08FDEA00281](https://openairdocs.org/sdr/08FDEA00281), Jan 25, 2008: FLOORBEAM. CORRODED. FWD PIT AT STA 879 RBL 57 FLOORBEAM HAS CORROSION. FOUND TO BE OUT OF LIMITS AND REPAIRED BY SPLICING IN NEW SECTION OF FLOORBEAM IAW SRM 53-00-01 VOL I FIG 7. - [SDR 08FDEA00280](https://openairdocs.org/sdr/08FDEA00280), Jan 25, 2008: FRAME. CORRODED. FWD PIT AT STA 919 BETWEEN STR 51R AND 51L LOWER FLANGE, FRAME HAS CORROSION. REPAIRED LOWER FLANGE AT STA 919, LONG 51R & 51L IAW DC/MD10-10 SRM 53-30-00, VOL - [SDR 08FDEA00282](https://openairdocs.org/sdr/08FDEA00282), Jan 25, 2008: DOOR FRAME. CRACKED. NR 3 MCD LOWER JAMB SUPPORT FITTING HOLES A, B, C AND D HAS CRACK INDICATIONS FOUND WITH BHE (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHINGS IN REFERENCE WITH - [SDR 08FDEA00286](https://openairdocs.org/sdr/08FDEA00286), Jan 25, 2008: DOOR FRAME. CRACKED. NR 6 MCD LOWER JAMB SUPPORT FITTING HOLES A, C AND D HAS CRACK INDICATIONS FOUND WITH BHEC (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHINGS IN REFERENCE WITH D - [SDR 08FDEA00285](https://openairdocs.org/sdr/08FDEA00285), Jan 25, 2008: DOOR FRAME. CRACKED. NR 6 MCD LOWER JAMB SUPPORT FITTING HOLES A, C AND D HAS CRACK INDICATIONS FOUND WITH BHEC (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHINGS IN REFERENCE WITH D - [SDR 08FDEA00284](https://openairdocs.org/sdr/08FDEA00284), Jan 25, 2008: DOOR FRAME. CRACKED. NR 4 MCD LOWER JAMB SUPPORT FITTING HOLES A, B, C AND D HAS CRACK INDICATIONS FOUND WITH BHEC (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHINGS IN REFERENCE WIT - [SDR 08FDEA00283](https://openairdocs.org/sdr/08FDEA00283), Jan 25, 2008: DOOR FRAME. CRACKED. NR 1 MCD LOWER JAMB SUPPORT FITTING HOLE "C" HAS CRACK INDICATIONS, FOUND WITH BHEC (SEE ATTACHED DRAWING). INSTALLED REPAIR BUSHING IN REFERENCE WITH DC/MD10-1 - [SDR 08FDEA00276](https://openairdocs.org/sdr/08FDEA00276), Jan 25, 2008: SHEAR TIE. DAMAGED. FWD PIT AT STA.808 BETWEEN STRINGER 34R AND 35R SHEAR TIE DAMAGED ON RADIUS. REMOVED, FABRICATED AND INSTALLED SHEAR TIE PER DC/MD10-10 SRM 53-13-01 VOL III FIG - [SDR 08FDEA00245](https://openairdocs.org/sdr/08FDEA00245), Jan 23, 2008: SHEAR TIE. CORRODED. LOWER FORWARD CARGO, STA 1099 BETWEEN L33L AND L35L, SHEAR TIE HAS CORROSION ON LOWER FLANGE, PART ADA0003-19 REMOVED CORROSION IAW DC/MD10-10 SRM, VOLUME II, 5 - [SDR 08FDEA00222](https://openairdocs.org/sdr/08FDEA00222), Jan 22, 2008: FRAME. CORRODED. FOUND CORROSION ON FRAME LOWER SURFACE, FS 1099 BETWEEN L34L AND L35L. REMOVED CORROSION IAW SRM VOL II 51-21-01 PG 28A. FOUND TO BE OUT OF LIMITS IAW SRM VOL I - [SDR 08FDEA00210](https://openairdocs.org/sdr/08FDEA00210), Jan 21, 2008: SHEAR TIE. CORRODED. CAC, CORROSION, SHEAR TIE, FS 1099 BETWEEN L51 R AND L50R REMOVED CORROSION IN REFERENCE WITH DC/MD10-10 SRM, VOLUME II, 51-21-01, PAGE 28A. ORIGINAL THICKNESS - [SDR 08FDEA00203](https://openairdocs.org/sdr/08FDEA00203), Jan 18, 2008: SEAT TRACK. GOUGED. MCD STA 1239 RBL 48 SEAT TRACK GOUGED AND WORN EVALUATED SEAT TRACK; SEVERAL BROKEN SCALLOPS, OUT OF LIMITS IAW DC/MD10-10 SRM 53-70-00 VOL I PG 21. REMOVED AND - [SDR 08FDEA00201](https://openairdocs.org/sdr/08FDEA00201), Jan 18, 2008: SHEAR TIE. DAMAGED. FWD PIT AT STA 808 BETWEEN LONG 34R AND LONG 35R SHEAR TIE DAMAGED ON RADIUS. REMOVED, FABRICATED, AND INSTALLED SHER TIE PER SRM 53-13-01, VOL III FIG 8A AND S - [SDR 08FDEA00200](https://openairdocs.org/sdr/08FDEA00200), Jan 18, 2008: SHEAR TIE. CORRODED. LOWER FORWARD CARGO, STA 1099 BETWEEN L33L AND L35, SHEAR TIE HAS CORROSION ON LOWER FLANGE. REMOVED CORROSION IAW SRM VOLUME II, 51-21-01 PAGE 28. FOUND TO BE - [SDR 08FDEA00198](https://openairdocs.org/sdr/08FDEA00198), Jan 18, 2008: SUPPORT FITTING. CRACKED. NR 2 MCD LOWER JAMB SUPPORT FITTING HOLES A, B AND C HAS CRACK INDICATIONS, FOUND WITH BHEC. INSTALLED REPAIR BUSHINGS AT LOCATION NR 2 FITTING HOLES A, B AND C - [SDR 08FDEA00195](https://openairdocs.org/sdr/08FDEA00195), Jan 18, 2008: SUPPORT FITTING. CRACKED. NR 5 MCD LOWER JAMB SUPPORT FITTING HOLES A AND D HAS CRACK INDICATIONS FOUND WITH BHEC. INSTALLED REPAIR BUSHINGS IAW SRM 53-50-00 VOL I PG 81 FIG 17 AT NR 5 F - [SDR 08FDEA00159](https://openairdocs.org/sdr/08FDEA00159), Jan 15, 2008: FITTING. CRACKED. UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 7 IS CRACKED IN HOLES "A, B, D" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NR 7 MAIN CARGO DOOR SPOOL LOCA - [SDR 08FDEA00158](https://openairdocs.org/sdr/08FDEA00158), Jan 15, 2008: FITTING. CRACKED. UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 6 IS CRACKED IN HOLE "A" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NUMBER 6 MAIN CARGO DOOR SPOOL LOCATIO - [SDR 08FDEA00157](https://openairdocs.org/sdr/08FDEA00157), Jan 15, 2008: SUPPORT FITTING. CRACKED. UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 4 IS CRACKED IN HOLES "A, C, D" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NR 4 MAIN CARGO DOOR SPOOL LOCA - [SDR 08FDEA00156](https://openairdocs.org/sdr/08FDEA00156), Jan 15, 2008: SUPPORT FITTING. CRACKED. UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 3 IS CRACKED IN HOLE "B" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NUMBER 3 MAIN CARGO DOOR SPOOL LOCATIO - [SDR 08FDEA00155](https://openairdocs.org/sdr/08FDEA00155), Jan 15, 2008: SUPPORT FITTING. CRACKED. UPPER MAIN CARGO DOOR, LOWER JAMB SUPPORT FITTING NR 1 IS CRACKED IN HOLE "C" BEYOND SRM LIMITS. REPLACED SUPPORT FITTING NR 1 MAIN CARGO DOOR SPOOL LOCATION IA - [SDR 08FDEA00122](https://openairdocs.org/sdr/08FDEA00122), Jan 14, 2008: SKIN. CRACKED. 1 5/8" CRACK LOCATED ON THE RT HORIZONTAL STABILIZER AT THE INBOARD AFT CORNER OF THE OUTER SECTION UPPER AFT SKIN PANEL. END OF CRACK MARKED AND VERIFIED WITH - [SDR 08FDEA00121](https://openairdocs.org/sdr/08FDEA00121), Jan 14, 2008: SKIN. CRACKED. LT HORIZONTAL STAB UPPER REAR SKIN PANEL CRACKED, INITIATING FROM AFT EDGE OF SKIN AND PROCEDING FWD 21/4" (APPROXIMATELY). VERIFIED BY HFEC INSPECTION MARKED E - [SDR 06FDEA3066](https://openairdocs.org/sdr/06FDEA3066), Aug 23, 2006: PRESSURE SWITCH. FAILED. NR 3 MANF FAIL INFLIGHT WHEN WING ANTI ICE SELECTED. FL340. COMPLIED WITH QRH. PERFORMED DECAY CHECK ON THE NR 3 MANIFOLD IAW MM 36-00-01-5, SYSTEM PASSED. CHEC - [SDR 05FDEA00106](https://openairdocs.org/sdr/05FDEA00106), Jan 17, 2005: VALVE. MALFUNCTIONED. ENG 3 A-ICE DISAGREEMENT, LEVEL ONE ALERT ILLUMINATED STEADY WITH SWITCH IN EITHER POSITION. ENG NR 3 ANTI-ICE VALVE - INOP, FOUND OLD VALVE WAS BINDING SEVERLY - [SDR 05FDEA00043](https://openairdocs.org/sdr/05FDEA00043), Aug 14, 2004: SKIN. DAMAGED. NOT APPROVED FUSELAGE SKIN REPAIR AT LT AND RT LONG 44-47, STA 1526. SUBJECT REPAIRS WERE INSPECTED FOR COMPLIANCE WITH 14CFR 121.368, THE REPAIRS WERE EVALUATE - [SDR 05FDEA00044](https://openairdocs.org/sdr/05FDEA00044), Jun 10, 2004: RAIL. CORRODED. BULK CARGO DOOR JAMB RAIL P/N AFA3249-1 CORRODED APPROX AT STA 1755-1764. FILLER, CAP AND REPAIR ANGLE INSTALLED AFTER CORROSION REMOVAL IAW FEDEX EA 8-5310- 79 - [SDR 04FDEA00226](https://openairdocs.org/sdr/04FDEA00226), Jan 26, 2004: PROXIMITY SWITCH. FAULTY. WHEN WE LOWERED THE GEAR FOR LANDING WE FELT THE GEAR COME DOWN BUT RED LIGHTS STAYED ON. WE MOVED THE HANDLE A FEW TIMES BUT NO HELP. RECYCLED GEAR AND THE RED - [SDR 03FDEA01681](https://openairdocs.org/sdr/03FDEA01681), Oct 2, 2003: SWITCH. INOPERATIVE. AIR CONDITIONING DOORS LIGHT ON S/O PANEL BEGAN FLICKERING INFLIGHT. FUEL WAS DUMPED AND LANDING ACCOMPLISHED AT SLC IAW RED TABS. ACN RELEASED FOR SERVICE IAW - [SDR 2000ZZZX654](https://openairdocs.org/sdr/2000ZZZX654), Feb 11, 2000: WEB. CRACKED. DURING MAINTENANCE, THREE 10 INCH CRACKS WERE FOUND ON RIGHT/CENTER WHEELWELL (Y=1386, Z=52) COMMON TO KEEL WEB, WEB DOUBLER, AND UPER WEB SPLICE, P/N'S, AEA016 - [SDR 99FDEA00269](https://openairdocs.org/sdr/99FDEA00269), May 3, 1999: WEB. CRACKED. DUR A/C P-F CONV AT AERONAVALI, 3 10' CRACKS WERE FOUND AT Y=1386 COMMON TO KEEL WEB, WEB DOUBLER & AEA0501 KEEL WEB UPPER SPLICE. REPAIRED KEEL WEB AND WEB DOU - [SDR 99FDEA00270](https://openairdocs.org/sdr/99FDEA00270), Nov 27, 1998: SKIN. CRACKED. DUR A/C P-F CONV FOUND DAMAGE AT XIFH=288.14 ON THE UPPER SURFACE OF LT I/B FLAP SKIN. REMOVED AND REPLACED O/B UPPER SKIN SECTION DAMAGE ARC2369. SRM 57-10-00 - [SDR 99FDEA00271](https://openairdocs.org/sdr/99FDEA00271), Oct 26, 1998: BOLT. CORRODED. DUR A/C P-F CONV CORROSION WAS FOUND IN ALL FOUR HOLE BORES COMMON TO ABA7003-2 & ABA7172 FITTINGS. THREE BOLTS FAILED IN TENSION. REMOVED AND REPLACED BOLTS FR - [SDR 99FDEA00272](https://openairdocs.org/sdr/99FDEA00272), Oct 2, 1998: SKIN. CORRODED. DUR A/C P-F CONV ON EXT LWR FUSELAGE FROM BS 1099 TO BS 1541 CORROSION. REMOVED AND REPLACED FUSELAGE BELLY SKIN FROM Y=1119 TO Y-1308, BETWEEN L48L-L48R. REPAI --- 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.