# N889FD: 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: 41067
- Year built: 2012
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 8, 2012
- Certificate issued: November 9, 2012
- Expires: November 30, 2028
- Mode S code: AC3FC5
- 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=889FD
- Page: https://openairdocs.org/aircraft/N889FD

From the FAA registry file of October 22, 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 N889FD.

## FAA accident and incident reports

None matched to N889FD.

## Service difficulty reports (16)

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 FDEA202602200247](https://openairdocs.org/sdr/FDEA202602200247), Feb 20, 2026: SKIN. DENTED. LH WING OB FLAP LOWER SURFACE FROM OB TO IB 97 INCHES CROSS TE TO LE 8 INCHES FOUND ONE DENT. REPAIRED LT WING OB FLAP LOWER SURFACE DENT AT OTEF STA 431 AS PER
- [SDR FDEA202412281848](https://openairdocs.org/sdr/FDEA202412281848), Dec 28, 2024: AMU. BURNED. INTERPHONE SERVICE BREAKER N P11 C23631 FOUND POPPED AFTER POWER SURGE/DROPPED OFFLINE. FOUND BOTH P11 C23631 INTERPHONE SERVICE BREAKER B24 POPPED AND P320 PAN
- [SDR FDEA202412271846](https://openairdocs.org/sdr/FDEA202412271846), Dec 27, 2024: ELECTRICAL SYS. MALFUNCTIONED. DURING COCKPIT SETUP. ACFT POWER SURGED & POPPED OFF. ALL SCREENS WENT BLACK. POWER CAME BACK ON A FEW SECS LATER. POWER THEN DROPPED OFF AGAIN & CAME BACK. THE
- [SDR FDEA202306151039](https://openairdocs.org/sdr/FDEA202306151039), Jun 15, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-18) AT STA1268.75/RBL112.75-115 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8452-1
- [SDR FDEA202306151038](https://openairdocs.org/sdr/FDEA202306151038), Jun 15, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8452-17) AT STA1240-1241.5/LBL109 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8452-17) 
- [SDR FDEA202304200719](https://openairdocs.org/sdr/FDEA202304200719), Apr 20, 2023: PANEL. TORN. CABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL #242HF FOUND TORN AT STATION 1285 REPAIRED MAIN DECK CARGO COMPARTMENT STATION 1285 FLOOR PANEL # 242 HF. AS PER B
- [SDR FDEA202304200718](https://openairdocs.org/sdr/FDEA202304200718), Apr 20, 2023: PANEL. TORN. CABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL #242JF FOUND TORN AT STATION 1285 REPAIRED MAIN DECK CARGO COMPARTMENT STATION 1285 FLOOR PANEL # 242 JF.AS PER B7
- [SDR FDEA202304200717](https://openairdocs.org/sdr/FDEA202304200717), Apr 20, 2023: PANEL. TORN. CABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL #214LF FOUND TORN AT STATION 1285 REPAIRED MAIN DECK CARGO COMPARTMENT STATION 1285 FLOOR PANEL # 241 LF.AS PER B7
- [SDR FDEA202304200716](https://openairdocs.org/sdr/FDEA202304200716), Apr 20, 2023: PANEL. TORN. CABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL #242EF FOUND TORN AT STATION 1235 REPAIRED MAIN DECK CARGO COMPARTMENT STATION 1235 FLOOR PANEL # 242 EF. AS PER B
- [SDR FDEA202304200715](https://openairdocs.org/sdr/FDEA202304200715), Apr 20, 2023: PANEL. TORN. CABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL#242FF FOUND TORN AT STATION 1140 REPAIRED MAIN DECK CARGO COMPART MENT STATION 1140 FLOOR PANEL # 242FF. AS PER B7
- [SDR FDEA202304200713](https://openairdocs.org/sdr/FDEA202304200713), Apr 20, 2023: PANEL. TORN. CABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL #241GF FOUND TORN AT STATION 1140 REPAIRED MAIN DECK CARGO COMPARTMENT STATION 1140 FLOOR PANEL # 241 GF.AS PER B7
- [SDR FDEA202304200711](https://openairdocs.org/sdr/FDEA202304200711), Apr 20, 2023: PANEL. TORN. CABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL #241JF FOUND TORN AT STATION 1300. REPAIRED MAIN DECK CARGO COMPARTMENT STATION 1300. FLOOR PANEL # 241 JF. AS PER
- [SDR FDEA202304190701](https://openairdocs.org/sdr/FDEA202304190701), Apr 19, 2023: PANEL. TORN. CABIN-MAIN DECK CARGO COMPARTMENT FLOOR PANEL#241KF FOUND TORN AT STATION 1285. REPAIRED MAIN DECK CARGO COMPARTMENT STATION 1285 FLOOR PANEL # 241 KF. AS PER B
- [SDR FDEA202301200148](https://openairdocs.org/sdr/FDEA202301200148), Jan 20, 2023: ACTUATOR. FAILED. L/H ENGINE I/B FAN COWL OPEN ACTUATOR UPPER ROD END BROKEN. REMOVED L/H ENGINE INBOARD FAN COWL ACTUATOR REF AMM 71-12-01-4 R/I. INSTALLED NEW FAN COWL OPENING 
- [SDR FDEA201708032104](https://openairdocs.org/sdr/FDEA201708032104), Aug 3, 2017: LENS. CRACKED. RIGHT DOOR EMERGENCY EXIT LIGHT COVER BROKEN FOUND DURING POST FLIGHT. REPLACED THET SIGN IAW AMM 33-51-01-2. OPS CHECKED GOOD. ACFT OK FOR SERVICE.
- [SDR FDEA201304210824](https://openairdocs.org/sdr/FDEA201304210824), Apr 21, 2013: SMOKE DETECTOR. MALFUNCTIONED. FOUND FLASHING RED LED ON SMOKE DETECTOR FOR CREW REST UPPER BUNK. R & R SMOKE DETECTOR M26035 AND TESTED OK IAW AMM 26-14-11-4.

## 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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