# N360FE: 1980 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 CF6-6 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: 46636
- Year built: 1980
- Type of aircraft: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 30, 2002
- Certificate issued: October 9, 2001
- Last registry action: June 3, 2023
- Mode S code: A40CCE
- 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/N360FE
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=360FE
- Page: https://openairdocs.org/deregistered/N360FE-2024-03-02

From the FAA registry file of October 31, 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 (149, newest 50)

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

- [SDR FDEA202007161537](https://openairdocs.org/sdr/FDEA202007161537), Jul 16, 2020: SENSOR. MALFUNCTIONED. AFTER TAKEOFF, LEVEL TWO BRAKE OVER TEMP. FOLLOWED QRH, MAX TEMP 996. CLEANED CONNECTOR TEMP READING GOOD. CONNECTED TO ORIGINAL SENSOR TEMP, READING GOOD. AFTE
- [SDR FDEA2020071761537](https://openairdocs.org/sdr/FDEA2020071761537), Jul 16, 2020: SENSOR. FALSE INDICATION. AFTER TAKEOFF, LEVEL TWO BRAKE OVER TEMP. FOLLOWED QRH. MAX TEMP 996. DEBRIEFED CREW UPON ARRIVAL INTO IND. AFTER TAKEOFF, TEMP CLIMBED TO 999 THEN "X'ED" OUT. 
- [SDR FDEA202002040265](https://openairdocs.org/sdr/FDEA202002040265), Feb 4, 2020: ACCESS DOOR. MISSING. FOUND ACCESS DOOR (152RT) ON CENTER CARGO DOOR FAIRING FOR VENT DOOR HANDLE MISSING AT BLOCK-IN. INSTALLED SERVICEABLE DOOR OPS CHECK NORMAL REF MM CHAP 52-32-0
- [SDR FDEA201910292779](https://openairdocs.org/sdr/FDEA201910292779), Oct 29, 2019: FLOOR SUPPORT. CORRODED. MAIN DECK STA 1900 RBL52 FLOOR SUPPORT WSP0711-552 UNDER NUTPLATE IS CORRODED REF PREVIOUS SDR #: 18-3003 REPAIRED FLOOR SUPPORT WSP0711-552 PER EA 8-5310-T0343
- [SDR FDEA2019122089831](https://openairdocs.org/sdr/FDEA2019122089831), Aug 9, 2019: ENGINE. OVERTEMP. PDIS 360 77-20 6391 09AUG19 MEM OPEN U LOGPAGES:2977480 APPROXIMATELY 500 FEET AFTER TAKEOFF. WE RECEIVED A LEVEL 1 ENG 1 EXEEDANCE. TEMP SHOWED 1010?, THROTTLE
- [SDR FDEA2019081291831](https://openairdocs.org/sdr/FDEA2019081291831), Aug 9, 2019: ENGINE. FAILED. APPROXIMATELY 500 FEET AFTER TAKEOFF. WE RECEIVED A LEVEL 1 ENG 1 EXEEDANCE. TEMP SHOWED 1010, THROTTLE 1 WAS PULLED BACK AND TEMP DECREASED INTO A NORMAL RANGE
- [SDR FDEA201812213588](https://openairdocs.org/sdr/FDEA201812213588), Dec 21, 2018: SLAT SYSTEM. MALFUNCTIONED. PDIS 360 27-80 5760 21DEC18 SAN FACT U LOGPAGES:3057986 ON APPROACH WITH FLAPS 50, FULLY COFIGURED AT 2000' A/C SLOWING ON SPEED TO 148KNTS, GOT STICK SHACKER W
- [SDR FDEA2018102953019](https://openairdocs.org/sdr/FDEA2018102953019), Oct 25, 2018: DOUBLER. CRACKED. LT WING AT APPROX XORS 568, INTERNAL. WING BEADED DOUBLER HAS A 1" CRACK. REPAIRED REF SRM 57-10-00 VOL 1 FIG 71 PG 222. MAJOR REPAIR.
- [SDR FDEA2018110243073](https://openairdocs.org/sdr/FDEA2018110243073), Oct 24, 2018: ROLLER TRAY. CRACKED. FWD CARGO BS 919, RT OTBD OMNI ROLLER TRAY HAD A 5 INCH CRACK. FABRICATED AND INSTALLED A NEW ROLLER TRAY IAW DWG ADJ7005, AND SRM 51-31-01, VOL 2.
- [SDR FDEA201810202963](https://openairdocs.org/sdr/FDEA201810202963), Oct 20, 2018: SKIN. DELAMINATED. LT WING NR 5 SPOILER, UPPER SKIN, PREVIOUS I/B REPAIR, HAS SMALL AREA DELAMINATION. REPAIRED NR 5 SPOILER PER SRM 57-10-00 VOL I AND SRM 51-71-00 VOL II.
- [SDR FDEA201810172936](https://openairdocs.org/sdr/FDEA201810172936), Oct 17, 2018: BRACKET. CRACKED. APU INLET DOOR, LT BRACKET AT SHAFT CRACKED. WELDED DAMAGED AREA AS PER AMM 20-90-00-8 AND DPS 10.225 SECTIONS 4.5 TO 4.5.6 AND GENERAL WELD PROCEDURES 5.3 TO 5
- [SDR FDEA2018102662991](https://openairdocs.org/sdr/FDEA2018102662991), Oct 16, 2018: FLOOR SUPPORT. CORRODED. CENTER CARGO STA 1841 FLOOR BOARD SUPPORT HAS CORROSION. INSTALLED NEW SUPPORT AGA7170-5 PER SRM 51-31-01 VOL. 2 AND DAC DWG AGA7170.
- [SDR FDEA2018102623014](https://openairdocs.org/sdr/FDEA2018102623014), Oct 12, 2018: FLOOR SUPPORT. CORRODED. MAIN DECK STA 1990 RBL 27 UNDER FLOOR HAS CORROSION AROUND NUT PLATE. MARKED NR 13 (ABOVE FLOOR) REMOVED DAMAGED FLOOR BOARD SUPPORT P/N WSP0711-554, FABRICATED
- [SDR FDEA2018102623001](https://openairdocs.org/sdr/FDEA2018102623001), Oct 12, 2018: FLOOR SUPPORT. WORN. MAIN DECK; STA. 440 26RBL FLOOR SUPPORT HAS UNDOCUMENTED MODIFICATION. DOT 47 REMOVED AND REPLACED AS REQUIRED FLOOR SUPPORT AT MAIN DECK; STA 440, RBL 19-26. R
- [SDR FDEA201810122859](https://openairdocs.org/sdr/FDEA201810122859), Oct 12, 2018: SKIN. DELAMINATED. RT WING NR 3 SPOILER UPPER SURFACE HAS SUSPECTED DELAMINATION AREA MARKED. REPAIRED DELAM AREA ON RT NR 3 SPOILER IAW SRM 51-71-00 VOL NR 2.
- [SDR FDEA2018102693000](https://openairdocs.org/sdr/FDEA2018102693000), Oct 9, 2018: SEAT TRACK. CRACKED. MAIN DECK - STA. 635 RBL 8. SEAT TRACK CRACKED LOWER FLANGE. NOTE: SEAT TRACK UNDER BALL MAT AREA. REPLACED DAMAGED SEAT TRACK FROM STA 635 TO STATION 615 REF S
- [SDR FDEA2018102692997](https://openairdocs.org/sdr/FDEA2018102692997), Oct 9, 2018: SEAT TRACK. CRACKED. MAIN DECK; STA. 485 - 490 15RBL SEAT TRACK DAMAGED 4" SECTION MISSING ON IB LEG. DOT 43 NEW SEAT TRACK INSTALLED AT LOCATION NOTED WORKED ON NR 501 REF SRM 51-3
- [SDR FDEA201810092978](https://openairdocs.org/sdr/FDEA201810092978), Oct 9, 2018: SUPPORT. CRACKED. FWD CARGO COMPT STA 795 FLOOR SUPPORT IS CRACKED. REMOVED AND REPLACED CRACKED FLOOR SUPPORT AS REQUIRED REF SRM51-35-01 VOL 2 AND DAC DWG ADA0235, NEW FLOOR SU
- [SDR FDEA2018102682995](https://openairdocs.org/sdr/FDEA2018102682995), Oct 8, 2018: SEAT TRACK. CRACKED. MAIN DECK; STA. 485 75LBL SEAT TRACK DAMAGED - 4" OF MISSING MISSING OB LEG. DOT 42 NOTE: RCB AREA INSTALLED NEW SEAT TRACK @ NOTED LOCATION REF SRM 51-31-01 VO
- [SDR FDEA201810073003](https://openairdocs.org/sdr/FDEA201810073003), Oct 7, 2018: FLOOR SUPPORT. CORRODED. MAIN DECK STA 1900 RBL52 FLOOR SUPPORT WSP0711-552 UNDER NUTPLATE IS CORRODED. REF SDR #: 19-2779 REPAIRED FLOOR SUPPORT WSP0711-552 PER EA 8-5310-T0343200 P1 F
- [SDR FDEA201810263003](https://openairdocs.org/sdr/FDEA201810263003), Oct 7, 2018: FLOOR SUPPORT. CORRODED. MAIN DECK, BS 1900, RBL 52 FLOOR SUPPORT WAS CORRODED. REPAIRED THE FLOOR SUPPORT IAW EA 8-5310-T0343200 P1. MAJOR REPAIR.
- [SDR FDEA2018102673002](https://openairdocs.org/sdr/FDEA2018102673002), Oct 7, 2018: FLOOR SUPPORT. CRACKED. MAIN DECK STA 427 LBL 79 LEFT SIDE LATERAL FLOOR SUPPORT ABA7339-1 DAMAGED AT CLIP NUT LOCATION. REMOVED DAMAGED FLOOR SUPPORT AND FAB NEW PER DRAWING ABA7339 A
- [SDR FDEA201810063086](https://openairdocs.org/sdr/FDEA201810063086), Oct 6, 2018: INTERCOSTAL. CORRODED. FORWARD AVIONICS COMPARTMENT STA 449 4 INCHES LEFT OF CENTERLINE CLIP HAS CORROSION. REMOVED AND REPLACED INTERCOSTAL AS REQUIRED IN REF DWG ABA7882 AND SRM-51-
- [SDR FDEA201810063012](https://openairdocs.org/sdr/FDEA201810063012), Oct 6, 2018: FRAME. CORRODED. AFT CARGO COMPT, STA 1901 FRAME UNDERSIDE CORROSION BY NUTPLATE. ACCOMPLISH CORROSION REPAIR PER SRM 53-00-01 FIG 9 VOL 1.
- [SDR FDEA2018102662996](https://openairdocs.org/sdr/FDEA2018102662996), Oct 6, 2018: SEAT TRACK. CRACKED. STA 488 RBL 17 SEAT TRACK WSP0826-513, TRACK DAMAGED AT FASTENER HOLE REMOVED AND REPLACED NOTED SEAT TRACK RF SRM 51-31-01 VOL II, DAC DWG WSP0826 MAJOR REPAIR
- [SDR FDEA2018102662994](https://openairdocs.org/sdr/FDEA2018102662994), Oct 6, 2018: SEAT TRACK. CRACKED. STA 488 LBL 82 SEAT TRACK WSP0826-509, FLANGE DAMAGED AT SCREW HOLE. INSTALLED NEW SEAT TRACK @ NOTED LOCATION REF SRN 51-31-01 VOL II DWG WSP0826.
- [SDR FDEA2018102652990](https://openairdocs.org/sdr/FDEA2018102652990), Oct 5, 2018: BULKHEAD. DAMAGED. CENTER CARGO COMPT STA1841 BULKHEAD SKIN DAMAGED (MARKED) REPLACED WEB AGA7170-3 AND AGA7170-4 PER SRM 51-31-01 VOL. 2. AND DAC DWG AGA7170.
- [SDR FDEA201810052972](https://openairdocs.org/sdr/FDEA201810052972), Oct 5, 2018: BRACKET. LOOSE. RT WING TRAILING EDGE OUTBD FLAP, INBD HINGE, BULLET FAIRING (635EL) INTERNAL BRACKET HAS LOOSE FASTENERS. REMOVED AND REPLACED INTERNAL BRACKET ON FAIRING 635E
- [SDR FDEA201810052971](https://openairdocs.org/sdr/FDEA201810052971), Oct 5, 2018: BRACKET. CRACKED. RT WING TRAILING EDGE OUTBD FLAP, INBD HINGE, BULLET FAIRING (635EL ) INTERNAL BRACKET HAS LOOSE FASTENERS. FABRICATED NEW BRACKET AS REQ PER DWG ARC0504.
- [SDR FDEA2018102643013](https://openairdocs.org/sdr/FDEA2018102643013), Oct 4, 2018: SKIN. WORN. TAIL CONE FOREWARD UPPER LEFT SKIN EDGE HAS WEAR MARKS MARKED NR 5 REPAIRED THE DAMAGE AREA AS REQUIRED REF SRM 53-00-01 FIG. 4 SHEET. 2 VOL. 1.
- [SDR FDEA201810042987](https://openairdocs.org/sdr/FDEA201810042987), Oct 4, 2018: LONGERON. CORRODED. A/C COMPT, PACK BAY NR 1. APPROX STA 565 TO 588, JUST O/B OF EXHAUST DOOR. RUSTED /CORRODED FASTENERS AND FRAME AND SKIN STRUCTURE. REMOVED AND REPLACED WITH LO
- [SDR FDEA201810033059](https://openairdocs.org/sdr/FDEA201810033059), Oct 3, 2018: SKIN. CORRODED. RT WING UPPER SURFACE AT APPROX XORS 387 STRINGER 5 CORROSION AROUND TWO (2) FASTENERS. REMOVED CORROSION REF SRM 57-10-00 FIG 60 SHEET 1 VOL 1. MATERIAL REMOVE
- [SDR FDEA201810033058](https://openairdocs.org/sdr/FDEA201810033058), Oct 3, 2018: SKIN. CORRODED. RT WING UPPER SURFACE AT APPROX XORS 264 STRINGER 13 CORROSION AROUND TWO (2) FASTENERS. REMOVED CORROSION REF SRM 57-10-00 FIG 60 SHEET 1 VOL 1. MATERIAL REMOV
- [SDR FDEA201810033057](https://openairdocs.org/sdr/FDEA201810033057), Oct 3, 2018: SKIN. CORRODED. LT WING UPPER SURFACE AT APPROX XORS 264 STRINGER 12 CORROSION AROUND ONE (1) FASTENER. REMOVED CORROSION REF SRM 57-10-00 FIG 60 SHEET 1 VOL 1. MATERIAL REMOVE
- [SDR FDEA201810033056](https://openairdocs.org/sdr/FDEA201810033056), Oct 3, 2018: SKIN. CORRODED. RT WING UPPER SURFACE AT APPROX XORS 264 BETWEEN STRINGERS 9 AND 10, CORROSION AROUND ONE (1) FASTENER. REMOVED CORROSION REF SRM 57-10-00 FIG 60 SHEET 1 VOL 1.
- [SDR FDEA2018102632999](https://openairdocs.org/sdr/FDEA2018102632999), Oct 3, 2018: SEAT TRACK. WORN. MAIN DECK : SEAT TRACK RBL X= 8.50 NEAR STA 755 WORN MARKED INSTALLED NEW SEAT TRACK SPLICE REF SRM 53-70-00 FIG 1 VOL I MAJOR REPAIR.
- [SDR FDEA2018102632998](https://openairdocs.org/sdr/FDEA2018102632998), Oct 3, 2018: SEAT TRACK. WORN. MAIN DECK : SEAT TRACK RBL X= 107.25 NEAR STA 695 WORN MARKED REMOVED DAMAGE AND PLUGGED SEAT TRACK REF SRM 53-70-00 FIG 2 VOL. I MAJOR REPAIR.
- [SDR FDEA201810032854](https://openairdocs.org/sdr/FDEA201810032854), Oct 3, 2018: SEAT TRACK. DAMAGED. MAIN DECK SEAT TRACK LBL X= 47.50 NEAR STA 755 WORN. REPLACED DAMAGED SEAT TRACK REF SRM 53-70-00, FIG 1, VOL 1 & SRM 51-31-01, VOL 2. MAJOR REPAIR.
- [SDR FDEA201807301850](https://openairdocs.org/sdr/FDEA201807301850), Jul 30, 2018: CONNECTOR. DEFECTIVE. UPON EXTENDING GEAR ON FINAL WE RECEIVED A LEVEL 2 ANTISKID L FAIL ALERT. REMOVED NR 1 MLG WHEEL TRANSDUCER ASSY, REF AMM 32-45-03-2. FOUND FULLY PUSHED PIN ON 
- [SDR FDEA2018073091840](https://openairdocs.org/sdr/FDEA2018073091840), Jul 29, 2018: CONTROL UNIT. FAILED. UPON PUTTING LANDING GEAR DOWN, GOT LEVEL 2 ANTI-SKID L FAIL ALERT. ON LAST LEG FAULTS FOUND ASCU INTERNAL FAULT CODE 324141. RTS FAILED. REMOVED AND REPLACED A
- [SDR FDEA201802140395](https://openairdocs.org/sdr/FDEA201802140395), Feb 14, 2018: PUMP. FAILED. HYD 3 FAIL WHEN SELECTING GEAR DOWN. REMOVED AND REPLACED NR 3 ENGINE DRIVEN HYDRAULIC PUMPS LEFT AND RIGHT REF AMM 29-11-01-2. OPS AND LEAK CHECKS REQUIRED. RE
- [SDR FDEA201801030004](https://openairdocs.org/sdr/FDEA201801030004), Jan 3, 2018: LIGHT. MALFUNCTIONED. EMERGENCY TEST FAILED, ALERT DISPLAYED IAW AMM 24-00-00-5-0, DOWN POWERED ACFT, REPOWERED. RESET THE LT EMERGENCY BUSS SENSE BREAKER. SYSTEM OPS CHECKED GOOD IA
- [SDR FDEA201712143383](https://openairdocs.org/sdr/FDEA201712143383), Dec 14, 2017: WIRE. BROKEN. PDIS 360 26-10 4655 13DEC17 MEM FACT U LOGPAGES:2734383 ENG #3 FIRE INDICATION ON CLIMB OUT. COMPLIED WITH QRH PROCEDURES, INCLUDING DISCHARGE OF AGT 2. FIRE IN
- [SDR FDEA201707131934](https://openairdocs.org/sdr/FDEA201707131934), Jul 13, 2017: DUCT. LEAKING. TWO HOURS INTO FLIGHT, HAD A QUICK FLASH ALERT LEVEL 2 FOR THE NR 2 ENGINE FIRE LOOP A, LASTED ONE SECOND AND WENT AWAY. 15 MINUTES LATER HAD STEADY LEVEL 2 ALE
- [SDR FDEA201703210964](https://openairdocs.org/sdr/FDEA201703210964), Mar 21, 2017: ACTUATOR. INOPERATIVE. 1L DOOR INOP. ELECTRIC DOOR ACTUATOR INOP. FOR EMERGENCY EGRESS, USE PNEUMATIC SYSTEM TO OPERATE DOOR. REPLACED L1 DOOR ACTUATOR ELECTRIC REF AMM 52-11-01-2. AD
- [SDR FDEA201610313757](https://openairdocs.org/sdr/FDEA201610313757), Oct 31, 2016: SLIDE. INOPERATIVE. L1 DOOR SLIDE PRESSURE LIGHT ILLUMINATED. TROUBLE SHOT IAW FIM 25-61-00-2, TASK 25-61-00-810-802, PTT INDICATOR LIGHT DOESN`T GO OFF. CHECKED PLUG OUT OF JACK W
- [SDR FDEA201610213667](https://openairdocs.org/sdr/FDEA201610213667), Oct 21, 2016: SKIN. CORRODED. LOWER FUSELAGE SKIN FOUND SURFACE CORROSION AT FWD DRAIN MAST LOCATION STA 665 APPROX. TRIMMED OUT SKIN DAMAGED, FABRICATED FILLER, DOUBLERS AND INSTALLED REF S
- [SDR FDEA201610133608](https://openairdocs.org/sdr/FDEA201610133608), Oct 13, 2016: TEE FITTING. CRACKED. LT STA 595 BULKHEAD TEE CAP VERTICAL LEG HAS A .5 INCH CRACK THROUGH THE LOWER FASTENER AT LONGERON 39L. REMOVED AND REPLACED SECTION OF TEE CHORD BETWEEN LONGE
- [SDR FDEA201610133604](https://openairdocs.org/sdr/FDEA201610133604), Oct 13, 2016: TEE FITTING. CRACKED. STA 595 BULKHEAD T CAP, LT FORWARD SIDE, HORIZONTAL LEG BETWEEN STR 38L AND STR 40L. 8 EA FASTENER HOLES SHOW CRACK INDICATION. REMOVED AND REPLACED SECTION OF 
- [SDR FDEA201610133594](https://openairdocs.org/sdr/FDEA201610133594), Oct 13, 2016: SKIN. DAMAGED. LT WING FUEL TANK LANDING 536CB HAS 1 BLOWN HOLE. REPAIRED PER EA 8-5710-T0328817, LT WING LOWER SURFACE-TANK ACCESS PANELS.

All 149: https://openairdocs.org/deregistered/N360FE-2024-03-02/reports.md

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