# N887FD: 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: 41066
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 3, 2012
- Certificate issued: October 4, 2012
- Expires: October 31, 2028
- Mode S code: AC3857
- 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=887FD
- Page: https://openairdocs.org/aircraft/N887FD

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 N887FD.

## FAA accident and incident reports

None matched to N887FD.

## Service difficulty reports (19)

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 FDEA202602160215](https://openairdocs.org/sdr/FDEA202602160215), Feb 16, 2026: SAFETY WIRE. WRONG PART. RH SLIDE - REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOARD RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER
- [SDR FDEA202602160214](https://openairdocs.org/sdr/FDEA202602160214), Feb 16, 2026: SAFETY WIRE. WRONG PART. LH SLIDE - REPLACE THE BREAKAWAY WIRE SECURING THE RELEASE CABLE TO THE PACKBOAR RELEASE MECHANISM ON THE PACKBOARD WITH MS20995CY16 CAD-PLATED COPPER WIRE PER 
- [SDR FDEA202510101945](https://openairdocs.org/sdr/FDEA202510101945), Oct 10, 2025: SKIN. WORN. NUMBER 7 SLAT OUTER SKIN FASTENER HOLE FOUND WORN OUT AT ISS 184. NR 7 SLAT OUTER SKIN FASTENER HOLE AT ISS 184 REPAIRED IAW SRM 57-43-01-2R, REPAIR 6, FIGURE 2
- [SDR FDEA202510081920](https://openairdocs.org/sdr/FDEA202510081920), Oct 8, 2025: SKIN. CRACKED. DURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF LT WING UPPER SKIN COMMON TO FASTENERS 0-5, FOUND ONE CRACK AT 6 O'CLOCK ON HOLE NR 5. NR 5 HOLE AT LT WING UPP
- [SDR FDEA202510081918](https://openairdocs.org/sdr/FDEA202510081918), Oct 8, 2025: SKIN. CRACKED. DURING PERFORMANCE OF UT &OPEN HOLE HFEC INSPECTION OF RT WING UPPER SKIN COMMON TO FASTENERS 0-5 & FOUND TWO CRACKS AT 6 O'CLOCK & 12 O'CLOCK ON HOLE NR 5. NR 
- [SDR FDEA202412121812](https://openairdocs.org/sdr/FDEA202412121812), Dec 12, 2024: LIFE RAFT. DAMAGED. AFTER ARRIVAL IN MEMPHIS L1 DOOR VERY DIFFICULT TO OPEN. DURING T/S AS PER FIM 52-11-00-810-814 FOUND FLUF AND OTHER DEBRIE HINDERING THE PROPER OPERATION AND I
- [SDR FDEA202304190676](https://openairdocs.org/sdr/FDEA202304190676), Apr 19, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLLOR PANEL 241UF(P/N:152W8652-3) AT STA1446/LBL73.5-76 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241UF(P/N:152W8652-3) AT STA1446/LBL73.5-76 CRA
- [SDR FDEA202304180666](https://openairdocs.org/sdr/FDEA202304180666), Apr 18, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8652-19) AT STA1393/LBL20-21.5 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241PF(P/N:152W8452-19) AT STA1393/LBL20-21.5 C
- [SDR FDEA202304180665](https://openairdocs.org/sdr/FDEA202304180665), Apr 18, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8652-21) AT STA1363/LBL43.75-44.75 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241QF(P/N:152W8452-21) AT STA1363/LBL43.75
- [SDR FDEA202304180664](https://openairdocs.org/sdr/FDEA202304180664), Apr 18, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1435.75/RBL76.25-77.25 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 242QF(P/N:152W8652-4) AT STA1435.75/RBL7
- [SDR FDEA202304180663](https://openairdocs.org/sdr/FDEA202304180663), Apr 18, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8452-17) AT STA1292/LBL110-111 FOUND CRACK. MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8452-17) AT STA1292/LBL110-111 C
- [SDR FDEA202304180662](https://openairdocs.org/sdr/FDEA202304180662), Apr 18, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-18) AT SVTA1272/RBL110-113 FOUND CRACK. CRACK SIZE L =3.0" IN LOWER SKIN WITHIN LIMIT. EVALUATED AS PER B777 SRM 
- [SDR FDEA202108031924](https://openairdocs.org/sdr/FDEA202108031924), Aug 3, 2021: CONTROL UNIT. MALFUNCTIONED. 03AUG21 MEM OVER NORTH ATLANTIC, ELEC GEN OFF R, STARTED THE APU WITH APU GEN OFF, RESET GEN PER ECL. . APPROX 2.5 LATER, GOT ELEC AC BUS R. RESE THE R BUS TIE 
- [SDR FDEA2019120433163](https://openairdocs.org/sdr/FDEA2019120433163), Dec 3, 2019: TIRE. LEAKING. PDIS 887 32-42 6858 03DEC19 MEM OPEN U LOGPAGES:3182122 TIRE PRESS EICAS ON DEPARTURE FROM ZSPD, TIRE #12 PRESSURE IS LOW AND DECREASING. REMOVED AND REPLACED #
- [SDR FDEA201911223047](https://openairdocs.org/sdr/FDEA201911223047), Nov 22, 2019: PCU. LEAKING. ON CLIMBOUT RECEIVED "HYD QTY LOW R" EICAS, FOLLOWED BY "HYD PRESS PRI R" EICAS AND THEN "HYD PRESS SYS R" EICAS, COMPLIED WITH ALL NON-NORMAL CHECKLISTS. CHECK
- [SDR FDEA201707091886](https://openairdocs.org/sdr/FDEA201707091886), Jul 9, 2017: AUTOTHROTTLE SYS. MALFUNCTIONED. AFTER BOTH ENGINES WERE STARTED. WHILE AWAITING THE GROUND CREW TO CLEAR THE WING. THE AUTO THROTTLE SERVO ENGAGED AND ATTEMPTED TO ADVANCE THE POWER. CAPTAIN R
- [SDR FDEA201609293403](https://openairdocs.org/sdr/FDEA201609293403), Sep 29, 2016: FLOOR PANEL. CRACKED. FOUND FLOOR SURFACE PLATE HAS CRACK 12 INCH, TWO LOCATION ON SAME PANEL AT POSITION 7R ON MDC. TEMPORARY REPAIR TO FLOOR PANEL AT POSITION 6R,7R, AND 8R. ROLLER
- [SDR FDEA201301230164](https://openairdocs.org/sdr/FDEA201301230164), Jan 23, 2013: COVER. FAULTY. EMERGENCY LIGHTS SWITCH RETURN SPRING FAULTY. DOES NOT RETURN SWITCH TO ARM WITH COVER CLOSED. R & R LIGHT SWITCH GUARD COVER IAW SMP OPS CHECKED NORMAL, ACFT O
- [SDR FDEA201212204340](https://openairdocs.org/sdr/FDEA201212204340), Dec 20, 2012: SMOKE DETECTOR. MALFUNCTIONED. AFTER BLOCK IN AND SHUTTING DOWN BOTH ENGINES, THE CREW SLEEP ROOM HAD AN AURAL SMOKE ALARM. THE ASSOCIATED ALARM LIGHT, NO APPARENT SMOKE WAS SEEN OR DETECTED.

## 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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