# N869FD: 2015 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: 40675
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 18, 2015
- Certificate issued: September 22, 2015
- Expires: September 30, 2028
- Mode S code: ABF0C7
- 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=869FD
- Page: https://openairdocs.org/aircraft/N869FD

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 N869FD.

## FAA accident and incident reports

None matched to N869FD.

## Service difficulty reports (13)

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 FDEA202606050674](https://openairdocs.org/sdr/FDEA202606050674), Jun 5, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP 5.A.(2) THEN FOUND 02EA CRACKS ON RH UPPER WING SKIN COMMON TO FASTENER #5 AS MARKED.
- [SDR FDEA202602080223](https://openairdocs.org/sdr/FDEA202602080223), Feb 8, 2026: SAFETY WIRE. WRONG PART. REMOVE RH DOOR SLIDE FOR FEA INSPECTION OF PROPER CAD PLATED COPPER SAFETY WIRE MS20995CY16. REMOVED R1 DOOR SLIDE IN REF TO 777 AMM. SLIDE WAS REMOVED DUE TO T
- [SDR FDEA202511202194](https://openairdocs.org/sdr/FDEA202511202194), Nov 20, 2025: SWITCH. MALFUNCTIONED. WHEN EMERGENCY LIGHTS SWITCH COVER IS CLOSED, THE EMERGENCY LIGHTS ARE NOT AUTOMATICALLY ARMED BY THE SWITCH COVER AND STAY IN THE OFF POSITION. MUST MANUALLY A
- [SDR FDEA202507011144](https://openairdocs.org/sdr/FDEA202507011144), Jul 1, 2025: WARNING LIGHT. FALSE ACTIVATION. AFTER BLOCK OUT, EMER LIGHTS ICAS ALERT ILLUMINATED. WORKED WITH MANT. TURNED EMER LIGHT ARMING SWITCH TO OFF. CYCLE FLIGHT ATTENDANT EMER LIGHT SWITCH AND REAR
- [SDR FDEA202503250492](https://openairdocs.org/sdr/FDEA202503250492), Mar 25, 2025: TIRE. FAILED. TIRE PRESS EICAS. NOSE TIRE #13 WAS 196PSI AT 2000Z. BY 0400Z, PRESSURE HAD DECREASED TO 173PSI. EMERGENCY DECLARED BY ATC FOR GEAR ISSUE. LANDED UNEVENTFULLY, 
- [SDR FDEA202309091568](https://openairdocs.org/sdr/FDEA202309091568), Sep 9, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8352-29 FOUND CRACKED AT STA1014 LBL86. EVALUATED AND MEASURED MAIN DECK CARGO FLOOR PANEL P/N:152W8352-29 CRACKED AT STA 10
- [SDR FDEA201907111534](https://openairdocs.org/sdr/FDEA201907111534), Jul 11, 2019: WHEEL. LEAKING. 5HRS INTO FLIGHT AT FL370 .82M GOT TIRE PRESS EICAS ALERT. GEAR SYNOPTIC SHOWS #9 TIRE AT 181 PSI AND AMBER. TIRE PRESS ON STATUS PAGE ALSO. REMOVED AND REPLACE
- [SDR FDEA201710273084](https://openairdocs.org/sdr/FDEA201710273084), Oct 27, 2017: SLIDE. MALFUNCTIONED. L1 DOOR WILL NOT ARM. INSTALLED A NEW L1 DOOR ESCAPE SLIDE AND INSTALLATION CHECKED GOOD IAW AMM 25-66-01-4.
- [SDR FDEA201710213024](https://openairdocs.org/sdr/FDEA201710213024), Oct 21, 2017: SLIDE. UNWANTED DEPLOY. L1 DOOR SLIDE DEPLOYED DURING DOOR OPENING. BOTH DOORS DISARMED, GREEN DOORS MANUAL & M M DISPLAYED ON STATUS PAGE. REMOVED AND REPLACED THE L1 DOOR SLIDE ASSY 
- [SDR FDEA201710152963](https://openairdocs.org/sdr/FDEA201710152963), Oct 15, 2017: WARNING MESSAGE. FALSE ACTIVATION. FLAP OVERSPEED AT FLAPS 1, DURING DESCENT. NO ORAL WARNING, SPEED ABOUT 270-275. MAT IS GIVING THE FAULT CODE 31-71011. AIRPLANE HAS EXCEEDED VFE OVERSPEED BY 1
- [SDR FDEA201706101610](https://openairdocs.org/sdr/FDEA201706101610), Jun 10, 2017: LENS. LOOSE. EMERGENCY LIGHT LENS CAME LOOSE. LT SIDE OF THE L1 DOOR. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY IAW AMM 33-50-00-2. EMERGENCY LIGHTS TESTED GOOD, OK FOR 
- [SDR FDEA201607092345](https://openairdocs.org/sdr/FDEA201607092345), Jul 9, 2016: FLAP. DAMAGED. FOUND LT INB'D AFT FLAP HAS DAMAGE. INSTALLED LT I/B AFT FLAP AND OPS CHECK OK PER AMM27-51-12-4. A/C OK FOR SERVICE.
- [SDR FDEA201606021792](https://openairdocs.org/sdr/FDEA201606021792), Jun 2, 2016: HANDLE. OUT OF ADJUST. L1 DOOR FAILS TO ARM. FOUND THE LT PAX ENTRY DOOR OUTSIDE TEE HANDLE NOT SEATED PROPERLY. COMPLIED WITH PAX ENTRY DOOR ADJUSTMENT TEST IAW MM 52-11-00-5. OPERAT

## 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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