# N372FE: 1972 Mcdonnell Douglas MD-10-10F, registration cancelled 2024-02-01

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: February 1, 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: 46610
- Year built: 1972
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 24, 2002
- Certificate issued: October 8, 1998
- Last registry action: June 3, 2023
- Mode S code: A43BBB
- 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/N372FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=372FE
- Page: https://openairdocs.org/deregistered/N372FE-2024-02-01

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 (224, newest 50)

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

- [SDR FDEA201804261124](https://openairdocs.org/sdr/FDEA201804261124), Apr 26, 2018: SEAL. DIRTY. L1 DOOR SEAL NOISY DURING CLIMB. CLEANED L1 DOOR SEAL AND DOOR THREASHOLD OF DIRTY AND DEBRIS.
- [SDR FDEA201803200740](https://openairdocs.org/sdr/FDEA201803200740), Mar 20, 2018: ENGINE. FAILED. ENG FAILURE NR 1 ENG CLIMBING THRU 5K. YAW, LOUD BANG RAPIDLY RISING EGT. ENG EXCEEDANCE 942 DEG. THROTTLE TRIMMED POSITIONED TO IDLE. ENG SHUT DOWN. FIRE BOTTL
- [SDR FDEA201708232299](https://openairdocs.org/sdr/FDEA201708232299), Aug 23, 2017: CLAMP. LEAKING. AIR MANIFOLD NR 2 FAILED. AFTER TAKEOFF. AIR TURN BACK. REMOVED & REPLACED CLAMP ON DUCT ASSY IN LEFT WHEEL WELL IAW MM 36-14-02-4. NO LEAKS NOTED. PERFORMED DE
- [SDR FDEA201708222297](https://openairdocs.org/sdr/FDEA201708222297), Aug 22, 2017: CLAMP. FAILED. AIR MANF NR 2 FAIL. AFTER TAKEOFF. AIR TURN BACK. R&R CLAMP ASSY PER MM 36-14-02-4 IN LEFT WHEEL WELL JUST FWD OF BULKHEAD.
- [SDR FDEA201708162286](https://openairdocs.org/sdr/FDEA201708162286), Aug 16, 2017: SKIN. GOUGED. FOUND GOUGED ON LOWER BELLY NEAR BS 1721, LONGERON 47L. REPAIRED THE SKIN IAW SRM 53-20-00, FIG 6.
- [SDR FDEA201708162285](https://openairdocs.org/sdr/FDEA201708162285), Aug 16, 2017: SKIN. CRACKED. FOUND CRACK ON FUSELAGE JUST AFT OF CTR CARGO DOOR AROUND BS 1801 AND STRINGER 45L. REPAIRED THE SKIN IAW SRM 53-20-00, FIG 6.
- [SDR FDEA201704261270](https://openairdocs.org/sdr/FDEA201704261270), Apr 26, 2017: FIRE LOOP. FAILED. DURING CLIMBOUT RECEIVED A LEVEL 2 ALERT FOR THE NR 1 ENGINE FIRE LOOP B AND TOOK THE APROPRIATE QRH ACTIONS (NO FIRE). TROUBLESHOT THE FIRE LOOP AND FOUND HIGH
- [SDR FDEA201606282172](https://openairdocs.org/sdr/FDEA201606282172), Jun 28, 2016: STIFFENER. CRACKED. LEFT GEAR WELL OTBD SIDE TO FLAP WELL BULKHEAD, LOWER GUSSET REPAIR IS CRACKED AND RIVETS SHEARED. REMOVED EXISTING REPAIR AND TRIMMED OUT CRACKED AREA. FABRICA
- [SDR FDEA201606272157](https://openairdocs.org/sdr/FDEA201606272157), Jun 27, 2016: SKIN. CRACKED. LEFT WING OTBD FLAP UPPER SURFACE CRACKED SKIN AT APPROXIMATELY XOFH 548, DEFECTIVE. INSTALLED DOUBLER AND FILLER IAW SRM 57-00-01, FIG 4, VOL 1. CLEANED AND PA
- [SDR FDEA201606242146](https://openairdocs.org/sdr/FDEA201606242146), Jun 24, 2016: ACCESS PANEL. DELAMINATED. RIGHT T/E ACCESS PANEL 641NB IS DELAMINATED IN MANY SPOTS. MARKED IN RED CIRCLES, REPAIRED RT T/E PANEL 641NB IAW SRM 51-71-00, VOL II.
- [SDR FDEA201606232131](https://openairdocs.org/sdr/FDEA201606232131), Jun 23, 2016: SEAT TRACK. DAMAGED. MAIN CABIN SEAT TRACK IS DAMAGED AT STA 630, RBL 8. REMOVED DAMAGED SECTION OF SEAT TRACK FROM STA 605-645, RBL 8. INSTALLED SEAT TRACK SPLICE REPAIR REF SRM 53
- [SDR FDEA201606222112](https://openairdocs.org/sdr/FDEA201606222112), Jun 22, 2016: ACCESS DOOR. DELAMINATED. RIGHT WING LOWER ACCESS DOOR, PN ARC0286-2, 641AB DELAMINATION. REPAIRED RT WING LOWER ACCESS DOOR ARC0286-2 IAW SRM 51-71-00, VOL NR 2.
- [SDR FDEA201606172034](https://openairdocs.org/sdr/FDEA201606172034), Jun 17, 2016: FITTING. CRACKED. STA 1159, RT SIDE CORNER. HAIRPIN FITTING CRACKED FROM UPPER INBD AFT FASTENER TO EDGE, 2016-06-17. REPAIRED FITTING AT BS 1159, RT SIDE IN REF TO SRM 53-30-00,
- [SDR FDEA201606152017](https://openairdocs.org/sdr/FDEA201606152017), Jun 15, 2016: SUPPORT ANGLE. CRACKED. R-1 DOOR SUPPORT ANGLE CRACKED ON UPPER FWD CORNER OF DOOR, ABOVE NR 8 BEAM, MARKED DOT 1, 2016-06-15. REMOVED SUPPORT ANGLE FROM R-1 DOOR, INSTALLED THE NEW PA
- [SDR FDEA201606142044](https://openairdocs.org/sdr/FDEA201606142044), Jun 14, 2016: PANEL. DELAMINATED. NR 2 ENGINE PICKLE BARREL PANEL 364JR HAS DELAMINATED AT UPPER CENTER TOP SURFACE PANEL 364JR. REPAIRED DELAMINATION IAW SRM 51-71-00, VOL NR 2.
- [SDR FDEA201606142043](https://openairdocs.org/sdr/FDEA201606142043), Jun 14, 2016: SKIN PANEL. DAMAGED. RIGHT NR 2 ENGINE INLET DUCT PANEL 364JR, EXTERNAL SKIN HAS 1 LIGHTNING STRIKE REPAIRED AREA ON PANEL 364JR IAW SRM 51-71-00, VOL NR 2.
- [SDR FDEA201606111949](https://openairdocs.org/sdr/FDEA201606111949), Jun 11, 2016: STIFFENER. CRACKED. RIGHT ACM COMPARTMENT, STA 595 BULKHEAD, HORIZONTAL STIFFENER, 3RD FROM BOTTOM, OTBD EDGE IS CRACKED. FABRICATED NEW STIFFENER NCA6044-58 IN REF TO DWG NCA6044.
- [SDR FDEA201606101941](https://openairdocs.org/sdr/FDEA201606101941), Jun 10, 2016: SKIN. DAMAGED. NR 2 ENGINE RT FAN COWL LANDING HAS DAMAGE ON THE SKIN AT THE FWD END AT APPROXIMATELY 5:30 POSITION. REMOVED AND REPLACED DAMAGED SKIN IN REF TO SRMN 54-10-00 
- [SDR FDEA201606091910](https://openairdocs.org/sdr/FDEA201606091910), Jun 9, 2016: DOUBLER. CRACKED. LEFT LOWER VERTICAL AT FUSELAGE DRAG ANGLE REPAIR DOUBLER CRACKED. MARKED AT NR 2 BANJO FITTING 2016-06-09. REMOVED CRACKED ANGLE. INSTALLED NEW ANGLE IN REF TO
- [SDR FDEA201606081895](https://openairdocs.org/sdr/FDEA201606081895), Jun 8, 2016: FRAME. CRACKED. RIGHT NR 3 ACM COMPARTMENT, BS 555, APPROXIMATELY LONGERON 38, CRACKED FRAME. INSTALLED FABRICATED DOUBLER IN NR 3 ACM COMPARTMENT, STA 555 AT APPROXIMATELY LON
- [SDR FDEA201606081893](https://openairdocs.org/sdr/FDEA201606081893), Jun 8, 2016: CAP. CRACKED. RIGHT BS 595 BULKHEAD TEE CAP VERTICAL LEG UPPER FASTENER HOLE AT LONGERON 39R HAS A CRACK INDICATION.
- [SDR FDEA201606081892](https://openairdocs.org/sdr/FDEA201606081892), Jun 8, 2016: BULKHEAD. CRACKED. RIGHT BS 595 BULKHEAD WEB LOWER FASTENER HOLE COMMON TO THE TEE CAP HAS A CRACK INDICATION.
- [SDR FDEA201606081875](https://openairdocs.org/sdr/FDEA201606081875), Jun 8, 2016: FLOORBEAM. CORRODED. FORWARD CARGO COMPARTMENT BILGE SPACE, THERE ARE 2 AREAS OF CORROSION ALONG A LATERAL FLOORBEAM UPPER ANGLE UNDER 2 DIFFRENT ROLLER TRAYS AT AFT SIDE OF THE BS 
- [SDR FDEA201606071869](https://openairdocs.org/sdr/FDEA201606071869), Jun 7, 2016: FITTING. CRACKED. CAC STA 1159, RT SIDE CORNER, HAIRPIN FITTING CRACKED FROM UPPER INBD AFT FASTENER TO EDGE. REPAIRED FITTING AT BS 1159 IAW SRM 53-30-00, VOL 1, FIG 7, SHEET 1,
- [SDR FDEA201606051852](https://openairdocs.org/sdr/FDEA201606051852), Jun 5, 2016: TEE FITTING. CRACKED. LEFT HORIZONTAL LE, CTR INBD SECTION APPEARS TO BE CRACKED AT UPPER T. REMOVED & INSTALLED NEW T CAP. PN ALC7052-19, IAW DWG ALC7052 & SRM 51-31-00 VOL 2.
- [SDR FDEA201606041813](https://openairdocs.org/sdr/FDEA201606041813), Jun 4, 2016: FLOORBEAM. CRACKED. MAIN CABIN CTR WING AREA, FLOORBEAM CRACKED AT STATION 1259, RBL 107, BELOW OTBD SEAT TRACK AREA. INSTALLED SR10530081 -15,-17,-19,-21, &-23 IAW DWG SR10530081.
- [SDR FDEA201606041811](https://openairdocs.org/sdr/FDEA201606041811), Jun 4, 2016: FLOORBEAM. CRACKED. MAIN CABIN CTR WING AREA, FLOORBEAM CRACKED AT STATION 1293, RBL 107, BELOW OTBD SEAT TRACK. REMOVED DAMAGED SECTION OF FLOORBEAM AND REPLACED WITH KIT SB105301
- [SDR FDEA201606041810](https://openairdocs.org/sdr/FDEA201606041810), Jun 4, 2016: FLOORBEAM. CRACKED. MAIN CABIN CTR WING AREA, FLOORBEAM CRACKED AT STATION 1259, LBL 107, AT OVERWING DOOR FWD FRAME AREA. REMOVED SECTION OF CRACKED FLOORBEAM AND REPLACED SECTION
- [SDR FDEA201606031807](https://openairdocs.org/sdr/FDEA201606031807), Jun 3, 2016: BULKHEAD. CRACKED. RIGHT STATION 595 BULKHEAD, LONGERON 38R, T CAP AFT LEG HAS CRACK INDICATION FROM RADIUS TO END OF LEG SECTION. CRACK LOCATED 1.75" BELOW LONGERON 38R. R & R SE
- [SDR FDEA201606011782](https://openairdocs.org/sdr/FDEA201606011782), Jun 1, 2016: INTERCOSTAL. CRACKED. AIR CYCLE MACHINE COMPARTMENT NR 3, AT STATION 548, HAS A CRACKED INTERCOSTAL. STOP DRILLED CRACK, NDT VERIFIED NO CRACK BEYOND STOP DRILL AND INSTALLED REPAIR 
- [SDR FDEA201606011781](https://openairdocs.org/sdr/FDEA201606011781), Jun 1, 2016: FITTING. CRACKED. BS 1159 RT SIDE CORNER, HAIR PIN FITTING CRACKED, FROM UPPER INBD AFT FASTENER TO EDGE.
- [SDR FDEA201605311794](https://openairdocs.org/sdr/FDEA201605311794), May 31, 2016: SKIN. PUNCTURED. SMALL PUNCTURE IN THE CTR OF MLG DOOR. REPAIRED IAW SRM 51-71-00 VOL 2.
- [SDR FDEA201605282178](https://openairdocs.org/sdr/FDEA201605282178), May 28, 2016: ANGLE. CORRODED. FORWARD CARGO COMPARTMENT, BILGE AT STA 879, ANGLE ON AFT SIDE OF FRAME CORRODED LBL4-LBL40. REPAIRED ANGLE IAW DWG RAM 1429.
- [SDR FDEA201605271747](https://openairdocs.org/sdr/FDEA201605271747), May 27, 2016: SEAT TRACK. DAMAGED. MAIN CABIN SEAT TRACK AT STATION 1381, LBL 75 IS DAMAGED & GOUGED. SEAT TRACK DAMAGED BEYOND LIMITS. R & R SECTION FROM STATION 1371 - 1391 IAW SRM 53-70-00 FIG
- [SDR FDEA201605201689](https://openairdocs.org/sdr/FDEA201605201689), May 20, 2016: FLOORBEAM. CORRODED. FORWARD CARGO COMPARTMENT BILGE SPACE, THERE IS A LATERAL FLOORBEAM SUPPORT THAT IS CORRODED AT STATION 1059, NEAR BL 0. REMOVED AND REPLACED FLOOR SUPPORT BEAM
- [SDR FDEA201605201704](https://openairdocs.org/sdr/FDEA201605201704), May 20, 2016: LONGERON. CRACKED. AFT EMPENNAGE UPPER AFT FUSELAGE COMPARTMENT, STATION 2030 - 2038 LT 7TH LONGERON HAS 8 CRACKS UPPER & LOWER AREAS, TRANSITIONING THRU 2033 BULKHEAD DOT 6 ZONE 
- [SDR FDEA201605201703](https://openairdocs.org/sdr/FDEA201605201703), May 20, 2016: LONGERON. CRACKED. AFT EMPENNAGE UPPER AFT FUSELAGE COMPARTMENT, STATION 2027 - 2037 RT 8TH LONGERON HAS 10 CRACKS UPPER & LOWER AREAS, TRANSITIONING THRU 2033 BULKHEAD DOT 5 ZONE
- [SDR FDEA201605201702](https://openairdocs.org/sdr/FDEA201605201702), May 20, 2016: LONGERON. CRACKED. AFT EMPENNAGE UPPER AFT FUSELAGE COMPARTMENT, STATION 2031 - 2035 RT 6TH LONGERON HAS 4 CRACKS UPPER & LOWER AREAS, TRANSITIONING THRU 2033 BULKHEAD DOT NR 4 ZO
- [SDR FDEA201605201701](https://openairdocs.org/sdr/FDEA201605201701), May 20, 2016: FLOORBEAM. CORRODED. FORWARD CARGO COMPARTMENT, STATION 735, BETWEEN BL 0 - LBL 30, HAS A LATERAL FRAME FLOOR SUPPORT BEAM ANGLE THAT IS CORRODED 2016 05 20. REMOVED MINOR CORROSION
- [SDR FDEA201605201700](https://openairdocs.org/sdr/FDEA201605201700), May 20, 2016: LONGERON. CRACKED. AFT EMPENNAGE UPPER AFT FUSELAGE COMPARTMENT, STATION 2031- 2035 RT 5TH LONGERON HAS 4 CRACKS UPPER & LOWER AREAS, TRANSITIONING THRU 2033 BULKHEAD DOT NR 3 ZON
- [SDR FDEA201605201699](https://openairdocs.org/sdr/FDEA201605201699), May 20, 2016: FLOOR SUPPORT. CORRODED. FORWARD CARGO COMPARTMENT AT STATION 791, BETWEEN BL 0 - LBL 30, A LATERAL BEAM FLOOR SUPPORT ANGLE HAS CORROSION 2016 05 20. R & R FLOOR SUPPORT ANGLE AT STA 7
- [SDR FDEA201605201698](https://openairdocs.org/sdr/FDEA201605201698), May 20, 2016: LONGERON. CRACKED. AFT EMPENNAGE UPPER AFT FUSELAGE COMPARTMENT, STATION 2030 - 2039 RT 4TH LONGERON HAS 9 CRACKS UPPER & LOWER AREAS, TRANSITIONING THRU 2033 BULKHEAD DOT NR 2 ZO
- [SDR FDEA201605201697](https://openairdocs.org/sdr/FDEA201605201697), May 20, 2016: LONGERON. CRACKED. AFT EMPENNAGE UPPER AFT FUSELAGE COMPARTMENT, STATION 2030 - 2036 RT 3RD LONGERON HAS 6 CRACKS UPPER & LOWER AREAS, TRANSITIONING THRU 2033 BULKHEAD DOT 1 ZONE 
- [SDR FDEA201605201696](https://openairdocs.org/sdr/FDEA201605201696), May 20, 2016: ROLLER TRAY. CORRODED. FORWARD CARGO COMPARTMENT, ROLLER TRAY HAS CORROSION ON A LT FLOOR SUPPORT TANG, BETWEEN STATION 755 - 808 AT BL 0. REMOVED CORRODED ROLLER TRAY AND REPLACED WI
- [SDR FDEA201605201695](https://openairdocs.org/sdr/FDEA201605201695), May 20, 2016: FLOOR SUPPORT. CORRODED. FORWARD CARGO COMPARTMENT, BILGE AT STATION 879 FRAME FLOOR SUPPORT ANGLE, BETWEEN LONGERON 52 & LBL 24 IS CORRODED. R & R FLOOR SUPPORT IN REF TO SRM 51-31-01,
- [SDR FDEA201605201691](https://openairdocs.org/sdr/FDEA201605201691), May 20, 2016: FRAME. CORRODED. FORWARD CARGO COMPARTMENT, BILGE AT STATION 879, AFT SIDE OF FRAME AT RBL 36, HAS CORROSION UNDER ROLLER TRAY. REMOVED CORROSION FROM ANGLE, TREATED AND PRIMED 
- [SDR FDEA201605121540](https://openairdocs.org/sdr/FDEA201605121540), May 12, 2016: TEE FITTING. CRACKED. RIGHT STATION 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 43R, HAS A 2 INCH CRACK. REPAIRED THE 595 BULKHEAD AT LONGERON 43R BY SPLICING IN A NEW SECTION OF T
- [SDR FDEA201605121539](https://openairdocs.org/sdr/FDEA201605121539), May 12, 2016: TEE FITTING. CRACKED. LEFT STATION 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 39L HAS A 2 INCH CRACK. R & R SECTION OF TEE CAP FROM LONGERON 36L TO 40L AT STA 595 WITH PN ACA7016-
- [SDR FDEA201605121538](https://openairdocs.org/sdr/FDEA201605121538), May 12, 2016: TEE FITTING. CRACKED. LEFT STATION 595 BULKHEAD TEE CAP VERTICAL LEG AT LONGERON 36L, HAS A 2 INCH CRACK. R & R SECTION OF TEE CAP FROM LONGERON 36L TO 40L AT STA 595 WITH PN ACA7016
- [SDR FDEA201512043907](https://openairdocs.org/sdr/FDEA201512043907), Dec 4, 2015: TRIM PANEL. OUT OF POSITION. ON LANDING ROLL OUT, HAD THE CABIN DOOR 1L APPEAR. AFTER COMING TO A STOP ON THE TAXIWAY, INSPECTED DOOR & ALL WAS NORMAL, EXCEPT FOR ARMED TAB FOR GIRT BAR WEN

All 224: https://openairdocs.org/deregistered/N372FE-2024-02-01/reports.md

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