# N885FD: 2011 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: 41064
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: October 28, 2011
- Certificate issued: October 28, 2011
- Expires: October 31, 2027
- Mode S code: AC30E9
- 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=885FD
- Page: https://openairdocs.org/aircraft/N885FD

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 N885FD.

## FAA accident and incident reports

None matched to N885FD.

## Service difficulty reports (17)

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 FDEA202605300655](https://openairdocs.org/sdr/FDEA202605300655), May 30, 2026: WIRE. DETACHED. ARMING WIRE ON EMERGENCY LIGHTS SWITCH ON OVERHEAD PANEL IS STRETCHED OUT AND NOT ARMING EMERGENCY LIGHTS NORMALLY WHEN THE WIRE FALLS OFF SWITCH. AMM: 33-51-00
- [SDR FDEA202501280143](https://openairdocs.org/sdr/FDEA202501280143), Jan 28, 2025: WEDGE. DENTED. FOUND RHW T/E O/B FLAP LOWER SURFACE WEDGE 1EA DENT AT THE CROSS OTEF76.96 AND FROM T/E TO FWD 22 INCHS LONG . REPAIRED RH WING T/E O/B FLAP LOWER SURFACE WEDGE
- [SDR FDEA202501270138](https://openairdocs.org/sdr/FDEA202501270138), Jan 27, 2025: SKIN. CRACKED. NUMBER 7 SLAT EXTERNAL UPR SKIN FROM IB TO OB 10 INCH CROSS TE TO LE 15 INCH FOUND CRACK. NO.7 SLAT EXTERNAL UPR SKIN FROM IB TO OB 10 INCH CROSS TE TO LE 15 IN
- [SDR FDEA202206031364](https://openairdocs.org/sdr/FDEA202206031364), Jun 3, 2022: DOUBLER. NONE. DURING PERFORMING EA TG-5710-T0367832 P2 STEP 11.C.(5), FOUND 01EA ZLJ-8 (BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINED S
- [SDR FDEA202206031363](https://openairdocs.org/sdr/FDEA202206031363), Jun 3, 2022: DOUBLER. MISREPAIRED. DURING PERFORMING EA TG-5710-T0367832 P1 STEP 11.C.(5), FOUND 01EA ZLJ-8 (BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 LHS TOO CLOSE TO EDGE OF MACHINED S
- [SDR FDEA202205311342](https://openairdocs.org/sdr/FDEA202205311342), May 31, 2022: SKIN. DENTED. R/H AFT FUSELAGE SKIN BETWEEN STA 1895 AND STA 1916 , S-43R TO S-46R FOUND DENT AND BULGE. R/H AFT FUSELAGE SKIN BETWEEN STA 1895 AND STA 1916, S-43R TO S-46R D
- [SDR FDEA202205191257](https://openairdocs.org/sdr/FDEA202205191257), May 19, 2022: TIRE. FAILED. DURING CRUISE TIRE PRESS ON EICAS AND STATUS PAGE. COMPLIED WITH CHECKLIST. #2 TIRE PSI WAS 91 PSI. ***EMERGENCY DECLARED*** REF: AMM 32-45-04-6-0 AND 32-45-01-
- [SDR FDEA202204080894](https://openairdocs.org/sdr/FDEA202204080894), Apr 8, 2022: NONE. LEAKING. TIRE PRESS INDICATION ON EICAS, GEAR SYNOPTIC PAGE INDICATED TIRE #6 173PSI. TIRE PRESSURE CONTINUED TO DECAY AT AN APPROXIMATE RATE OF 6PSI/HR. RAN NNC AND DEC
- [SDR FDEA201708252355](https://openairdocs.org/sdr/FDEA201708252355), Aug 25, 2017: SIGN. INOPERATIVE. ON PREFLIGHT FOUND LT FWD EMER EXIT SIGN LED HALF OUT. REMOVED AND REPLACED LT FWD EMER EXIT SIGN PN 702409-101 IAW AMM 323-51-01-2, OPS CHECK GOOD. A/C OK FOR 
- [SDR FDEA201606262147](https://openairdocs.org/sdr/FDEA201606262147), Jun 26, 2016: LIGHT. INOPERATIVE. 2 OVERHEAD EMERGENCY LIGHTS INOPERATIVE. OVERHEAD EMERGENCY LIGHTS RELAMPED IAW MM 33-50-00-02.
- [SDR FDEA201508052483](https://openairdocs.org/sdr/FDEA201508052483), Aug 5, 2015: SWITCH. FAULTY. REPEAT WRITE UP, AFTER SHUTDOWN ECC INDICATED EMER LIGHTS STILL ARMED WHEN SWITCH MOVED TO OFF. REPLACED WINDOW HEAT & EMER LIGHT SWITCH MODULE IAW AMM 30-41-02
- [SDR FDEA201508022448](https://openairdocs.org/sdr/FDEA201508022448), Aug 2, 2015: LIGHT. DEFECTIVE. AFTER SHUTDOWN ECL INDICATED EMERGENCY LIGHTS STILL ARMED, WHEN SWITCH MOVED TO OFF. R & R BULB ON CAPTAINS SIDE. OPERATIONS CHECKED NORMAL IAW AMM 33-50-00-008
- [SDR FDEA201503140928](https://openairdocs.org/sdr/FDEA201503140928), Mar 14, 2015: SPRING. OUT OF ADJUST. EMERGENCY LIGHTS WON'T TURN OFF ON SHUTDOWN CHECKLIST. FOUND INTERNAL WIRE SPRING INSIDE OVERHEAD EMER LIGHT SWITCH COVER SLIPPED OVER THE SWITCH & DIDN'T ALLOW
- [SDR FDEA201412264189](https://openairdocs.org/sdr/FDEA201412264189), Dec 26, 2014: TIRE. FAILED. NUMBER 11 MAIN TIRE MISSING TREAD AFTER BOCK IN. R & R NR 11 MLG TIRE & WHEEL ASSEMBLY IAW AMM 32-45-01-4.
- [SDR FDEA201406271569](https://openairdocs.org/sdr/FDEA201406271569), Jun 27, 2014: VALVE. INOPERATIVE. RIGHT ON DESCENT HAD A FAINT HOT ELEC SMELL. ON LANDING WE WERE UNABLE TO CONTROL THE COCKPIT TEMPERATURE IN AUTO OR MANUAL MODE. R & R 3 WAY VLV & TESTED IAW A
- [SDR FDEA201302170356](https://openairdocs.org/sdr/FDEA201302170356), Feb 17, 2013: SWITCH. FAILED. EMERGENCY LIGHT SWITCH DID NOT SENSE THE OFF POSITION ON SHUTDOWN. EMERGENCY LIGHT SHOWN OFF ON SHUTDOWN CHECK LIST WITHOUT MARK. CYCLED SW AND WENT OUT OF CHEC
- [SDR FDEA201206292423](https://openairdocs.org/sdr/FDEA201206292423), Jun 29, 2012: THROTTLE. MALFUNCTIONED. AFTER PUSHBACK AND DURING CONFIGURATION BEFORE TAXI, THROTTLE WENT FULL FORWARD TO TAKEOFF POWER WHILE BRAKES WERE SET, HANDS WERE NOT ON THROTTLES, HAD TO FORC

## 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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