# N864FD: 2012 Boeing 777-FS2

- Status: Valid registration
- Airframe: [Boeing 777-FS2](https://openairdocs.org/model/boeing-777-fs2) (registry code 138527H, 13 seats)
- Engine: [GE GE90-110B1](https://openairdocs.org/engine/ge-ge90-110b1) (registry code 30046)
- Data sheets: [TCDS E00049EN](https://openairdocs.org/tcds/E00049EN) (General Electric Company GE Aviation) (OpenAirDocs)
- Serial number: 37735
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: May 14, 2012
- Certificate issued: May 15, 2012
- Expires: May 31, 2028
- Mode S code: ABDE34
- Registered owner: [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 is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=864FD
- Page: https://openairdocs.org/aircraft/N864FD

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 21 in force

### Matched by airframe (Boeing 777-FS2)

None in force.

### Matched by engine (GE GE90-110B1)

- [AD 2025-25-07](https://openairdocs.org/ad/2025-25-07): Turbine Section · General Electric Company GE GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Feb 6, 2026
- [AD 2025-07-10](https://openairdocs.org/ad/2025-07-10): Fuel Controlling System · General Electric Company GE GE90-110B1 and GE90-115B. Effective May 21, 2025
- [AD 2024-06-15](https://openairdocs.org/ad/2024-06-15): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective May 14, 2024
- [AD 2023-26-07](https://openairdocs.org/ad/2023-26-07): Turbine Section · General Electric GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Feb 27, 2024
- [AD 2023-04-19](https://openairdocs.org/ad/2023-04-19): Turbine Engine Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Mar 27, 2023
- [AD 2022-23-09](https://openairdocs.org/ad/2022-23-09): Turbine Engine Compressor Section, Turbine Section · General Electric GE90-90B, GE90-94B, GE90-110B1 and 1 more. Effective Jan 17, 2023
- [AD 2022-18-06](https://openairdocs.org/ad/2022-18-06): Turbine Engine Compressor Section, Turbine Section · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective Oct 26, 2022
- [AD 2021-26-06](https://openairdocs.org/ad/2021-26-06): Turbine Engine Accessory Drive · General Electric GE90-76B, GE90-85B, GE90-90B and 3 more. Effective Feb 15, 2022
- [AD 2020-21-13](https://openairdocs.org/ad/2020-21-13): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Nov 17, 2020
- [AD 2020-18-14](https://openairdocs.org/ad/2020-18-14): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Oct 21, 2020
- [AD 2020-10-04](https://openairdocs.org/ad/2020-10-04): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective May 27, 2020
- [AD 2020-01-55](https://openairdocs.org/ad/2020-01-55): Turbine Section · General Electric GE90-110B1 and GE90-115B. Effective Mar 2, 2020
- [AD 2018-20-23](https://openairdocs.org/ad/2018-20-23): Turbine Engine Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Nov 30, 2018
- [AD 2018-20-22](https://openairdocs.org/ad/2018-20-22): Turbine Section · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Nov 13, 2018
- [AD 2017-08-06](https://openairdocs.org/ad/2017-08-06): Engine Oil Cooler · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective May 22, 2017
- [AD 2013-23-18](https://openairdocs.org/ad/2013-23-18): Variable bypass valve (VBV) actuator fuel supply tube · General Electric GE90-110B1 and GE90-115B. Effective Jan 7, 2014
- [AD 2013-17-07](https://openairdocs.org/ad/2013-17-07): Stage 1 high-pressure turbine (HPT) stator shrouds · General Electric GE90-110B1, GE90-115B, GE90-76B and 3 more. Effective Oct 18, 2013
- [AD 2013-15-20](https://openairdocs.org/ad/2013-15-20): Transfer gearbox assembly (TGB) radial gearshafts · General Electric GE90-110B1, GE90-113B, GE90-115B and 5 more. Effective Aug 21, 2013
- [AD 2011-26-11](https://openairdocs.org/ad/2011-26-11): HPC stages 1-2 seal teeth · General Electric GE90-110B1 and GE90-115B. Effective Feb 3, 2012
- [AD 2009-25-14](https://openairdocs.org/ad/2009-25-14): Blade · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Jan 19, 2010
- [AD 2007-10-05](https://openairdocs.org/ad/2007-10-05): Turbine Center Frames (TCFs) · General Electric GE90-110B1, GE90-113B and GE90-115B. Effective Jun 14, 2007

### Historical (superseded or no longer in force)

- [AD 2021-15-05](https://openairdocs.org/ad/2021-15-05) (historical): Engine Controls · General Electric GE90-110B1 and GE90-115B. Effective Sep 13, 2021
- [AD 2020-20-17](https://openairdocs.org/ad/2020-20-17) (historical): Engine Controls · General Electric GE90-110B1 and GE90-115B. Effective Oct 23, 2020
- [AD 2017-07-04](https://openairdocs.org/ad/2017-07-04) (historical): Compressor Section · General Electric GE90-110B1 and GE90-115B. Effective Apr 21, 2017
- [AD 2013-24-17](https://openairdocs.org/ad/2013-24-17) (historical): High pressure compressor (HPC) rotor stage 2-5 spools · General Electric GE90-110B1 and GE90-115B. Effective Dec 31, 2013
- [AD 2013-14-51](https://openairdocs.org/ad/2013-14-51) (historical): Failure of a transfer gearbox assembly radial gearshaft · General Electric GE90-110B1 and GE90-115B
- [AD 2013-10-52](https://openairdocs.org/ad/2013-10-52) (historical): Transfer gearbox assemblies (TGBs) · General Electric GE90-110B1 and GE90-115B. Effective Jun 26, 2013

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N864FD.

## FAA accident and incident reports

None matched to N864FD.

## Service difficulty reports (23)

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

- [SDR FDEA202602140194](https://openairdocs.org/sdr/FDEA202602140194), Feb 14, 2026: SAFETY WIRE. WRONG PART. SAFETY WIRE FOUND ON SLIDE WAS NOT THE CORRECT TYPE ACCORDING TO F.E.A.#:G-2560-F0386282 C PART: 1 (P1) REPLACED BREAKAWAY WIRE WITH CORRECT WIRE SPEC (MS20995C
- [SDR FDEA202602130192](https://openairdocs.org/sdr/FDEA202602130192), Feb 13, 2026: SLIDE. MISWIRED. R1 DOOR SLIDE HAS INCORRECT SAFETY WIRE ON PACKBOARD RELEASE CABLE. INSTALLED PROPER SAFETY WIRE ON R1 SLIDE PACKBOARD RELEASE CABLE IAW B777MM 25-66-01-4. A/C 
- [SDR FDEA202503130389](https://openairdocs.org/sdr/FDEA202503130389), Mar 13, 2025: SKIN. DENTED. FOUND RHW T/E I/B AFT FLAP LOWER SURFACE DENT AT THE CROSS ITEF 250 AND T/E 2 INCHES. REPAIRED RHW T/E I/B AFT FLAP LOWER SURFACE DENT AT THE CROSS ITEF 250 AND
- [SDR FDEA202209302403](https://openairdocs.org/sdr/FDEA202209302403), Sep 30, 2022: DOUBLER. DAMAGED. DURING PERFORMING EO G-5710-E0365655 A P7 STEP 8.C.(6),FOUND 01EA HOLE OVERSIZED AT STA1030,STGR38-1",LHS. COMPLETED AS PER EA G-5310-T0370456 A P1 STEP 8. TITL
- [SDR FDEA202209302402](https://openairdocs.org/sdr/FDEA202209302402), Sep 30, 2022: DOUBLER. DAMAGED. DURING PERFORMING EO G-5710-E0365655 A P8 STEP8.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINED STE
- [SDR FDEA202209302401](https://openairdocs.org/sdr/FDEA202209302401), Sep 30, 2022: DOUBLER. DAMAGED. DURING PERFORMING EO G-5710-E0365655 A P7 STEP8.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 LHS TOO CLOSE TO EDGE OF MACHINED STE
- [SDR FDEA202209212352](https://openairdocs.org/sdr/FDEA202209212352), Sep 21, 2022: SKIN. DELAMINATED. NO.8 SPOILER LWR SURFACE OB AFT CORNER FOUND DELAMINATION. NO.8 SPOILER LWR SURFACE OB AFT CORNER REPAIRED AS PER B777 SRM 57-70-01-2R REPAIR 1 AND SRM 51-70-04
- [SDR FDEA202209212351](https://openairdocs.org/sdr/FDEA202209212351), Sep 21, 2022: SKIN. DENTED. LH WING OB FLAP LWR SURFACE FOUND DENT AT OTEF 407. LH WING OB FLAP LWR SURFACE AT OTEF 407 REPAIRED AS PER B777 SRM 57-53-01-2R REPAIR 2 AND SRM 51-70-04-2R RE
- [SDR FDEA202209152328](https://openairdocs.org/sdr/FDEA202209152328), Sep 15, 2022: DOUBLER. DAMAGED. DURING PERFORMING EO G-5710-E0365655 A P7 STEP 8.C.(6), FOUND 01EA HOLE OVERSIZED AT STA1030, STGR38 -1", LHS. COMPLETED AS PER EA G-5310-T0370456 A P1 STEP 8. 
- [SDR FDEA202209152327](https://openairdocs.org/sdr/FDEA202209152327), Sep 15, 2022: DOUBLER. DAMAGED. DURING PERFORMING EO G-5710-E0365655 A P8 STEP8.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINED STE
- [SDR FDEA202209152326](https://openairdocs.org/sdr/FDEA202209152326), Sep 15, 2022: DOUBLER. DAMAGED. DURING PERFORMING EO G-5710-E0365655 A P7 STEP8.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 LHS TOO CLOSE TO EDGE OF MACHINED STE
- [SDR FDEA202208262076](https://openairdocs.org/sdr/FDEA202208262076), Aug 26, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 FOUND CRACKED AT STA1706 BL0. REPAIRED MAIN DECK CARGO FLOOR PANEL P/N:152W8650-4 CRACKED AT STA1706 BL0 AS PER B777 
- [SDR FDEA202208262075](https://openairdocs.org/sdr/FDEA202208262075), Aug 26, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 FOUND CRACKED AT STA 1660 BL 0. REPAIRED MAIN DECK CRGO FLOOR PANEL P/N:152W8650-3 CRACKED AT STA1660 BL0 AS PER B777
- [SDR FDEA202004130738](https://openairdocs.org/sdr/FDEA202004130738), Apr 13, 2020: FLOOR SUPPORT. WORN. LOWER BULK CARGO COMPARTMENT STATION 1926 RIGHT BUTT LINE 41 STRINGER FOUND SEVERAL HOLES AS MARKED. LOWER BULK CARGO COMPARTMENT STATION 1926 RIGHT BUTT LINE 4
- [SDR FDEA202002210365](https://openairdocs.org/sdr/FDEA202002210365), Feb 21, 2020: SWITCH. MALFUNCTIONED. DURING PREFLIGHT EMER LIGHTS EICAS REMAINED ILLUMINATED AFTER SWITCH TO GUARDED POSITION. CYCLED EMERGENCY LIGHTS SWITCH PER B777 FIM ATA 33-51-00-2. OK FOR SER
- [SDR FDEA2019100752443](https://openairdocs.org/sdr/FDEA2019100752443), Oct 5, 2019: SPRING. LOOSE. RETENSION WIRE ON THE EMERGENCY LIGHTS SWITCH IS MISSHAPENED AND DOES NOT PULL THE SWITCH TO ARMED WHEN CLOSED FOUND RETENSION SPRING LOOSE. RESECURED PER STAND
- [SDR FDEA201809202635](https://openairdocs.org/sdr/FDEA201809202635), Sep 20, 2018: PUMP. DAMAGED. AFTER LEVEL OFF AT FL 350 RECEIVED "HYD QTY LOW L" ALERT QTY DECREASED TO 0. FOLLOWED BY "HYD QTY PRESS LOW". QRH ACCOMPLISHED AFTER T/S FOUND LT EDP HOUSING CR
- [SDR FDEA201802040302](https://openairdocs.org/sdr/FDEA201802040302), Feb 4, 2018: LIGHT. INOPERATIVE. ON POST FLT FOUND L1 DOORWAY FWD EMERGENCY EXIT LIGHT HALF LED'S BURNED OUT. REMOVED AND REPLACED L1 DOORWAY FWD EMERGENCY EXIT LIGHT IAW AMM 33-51-01-2 AND OPS
- [SDR FDEA201710293098](https://openairdocs.org/sdr/FDEA201710293098), Oct 29, 2017: BATTERY PACK. DISCHARGED. L1 DOOR EPAS BATTERY LIGHT DOES NOT FLASH GREEN, FOUND DURING POST FLIGHT INSPECTION. REMOVED AND REPLACED BATTERIES IN L1 DOOR EPAS BATTERY PACK IAW AMM 52-11-
- [SDR FDEA201707111915](https://openairdocs.org/sdr/FDEA201707111915), Jul 11, 2017: STRUCTURE. DAMAGED. LEFT ELEVATOR T/E DAMAGED. AREA REPAIRED IAW SRM 55-20-01-2R, FIG 202, REPAIR 1. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201701180225](https://openairdocs.org/sdr/FDEA201701180225), Jan 18, 2017: BRAKE SYS. MALFUNCTIONED. DURING POST-FLIGHT CHECK FOUND BRAKE UNIT NR 7 WITH TEMP 0 ON GEAR PAGE, BRAKE COLD AT TOUCH. FURTHER TROUBLESHOOTING IAW 32-46-00-810-807, INSPECTED THE NR 7 B
- [SDR FDEA201404270865](https://openairdocs.org/sdr/FDEA201404270865), Apr 27, 2014: SEAT. DEFECTIVE. FIRST OFFICER`S SEAT SHORTED OUT, SPARKED WITH SOME SMOKE, MOVED ON PREFLIGHT. VISUAL INSPECTED & FOUND FIRST OFFICER`S SEAT ELEC CABLE EVIDENCE OF SPARK NEAR R
- [SDR FDEA201306251395](https://openairdocs.org/sdr/FDEA201306251395), Jun 25, 2013: LAMP. INOPERATIVE. RT EXTERIOR EMERGENCY LIGHT INOPERATIVE, REPLACED LAMPS. CHECKED NORMAL.

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Boeing 777-FS2 aircraft: https://openairdocs.org/model/boeing-777-fs2/aircraft.md
- The GE GE90-110B1 engine: https://openairdocs.org/engine/ge-ge90-110b1.md

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