# N861FD: 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: 37732
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 4, 2011
- Certificate issued: November 8, 2011
- Expires: November 30, 2027
- Mode S code: ABD30F
- 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=861FD
- Page: https://openairdocs.org/aircraft/N861FD

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 N861FD.

## FAA accident and incident reports

None matched to N861FD.

## Service difficulty reports (26)

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 FDEA202605110586](https://openairdocs.org/sdr/FDEA202605110586), May 11, 2026: SWITCH. OUT OF ADJUST. EMERGENCY LIGHTS ADVISORY MESSAGE STILL APPEARS. AMM: 33-51-00-5 ADJUSTED SWITCH GAURD, OPS CHECK GOOD.
- [SDR FDEA202605110585](https://openairdocs.org/sdr/FDEA202605110585), May 11, 2026: WARNING MESSAGE. FALSE ACTIVATION. EMERGENCY LIGHTS ADVISORY APPEARED ON PREFLIGHT. AMM: 33-51-00-5 EMERGENCY LIGHTS OPS CHECKS OK PER ABOVE REF, OK FOR SERVICE
- [SDR FDEA202503190458](https://openairdocs.org/sdr/FDEA202503190458), Mar 19, 2025: WIRE. DAMAGED. EMERGENCY LIGHT SWITCH ON OVERHEAD PANEL RED COVER SWITCH WIRE LOOP NOT ADJUSTED PROPERLY TO ACTUATE THE THREE POSITION SWITCH AS DESIGNED. THE WIRE LOOP IS STR
- [SDR FDEA202412271845](https://openairdocs.org/sdr/FDEA202412271845), Dec 27, 2024: POWER SUPPLY. INOPERATIVE. DURING PILOT PRE-FLT, LH SUPRMRY EMER EXIT LIGHTS INOP. POWER SUPPLY IN STOCK BAD FROM STOCK. CANNED POWER SUPPLY FROM A/C N866FD. REMOVED/REPLACED POWER SUPPLY
- [SDR FDEA202410281590](https://openairdocs.org/sdr/FDEA202410281590), Oct 28, 2024: SKIN. DAMAGED. FOUND A LIGHTNING STRIKE AT RUDDER TRAILING EDGE ABOUT RUD STA 525.
- [SDR FDEA202410221570](https://openairdocs.org/sdr/FDEA202410221570), Oct 22, 2024: SKIN. DENTED. RH WING OB FLAP LWR SURFACE FOUND DENT AT 170.5 INCHES TO IB AND 7.3 INCHES TO AFT EDGE. REPAIRED RH WING OB FLAP LWR SURFACE DENT AT OTEF STA 205 AS PER B777 S
- [SDR FDEA202307261296](https://openairdocs.org/sdr/FDEA202307261296), Jul 26, 2023: DOOR. DAMAGED. ON PRE FLIGHT FOUND FUEL LEAKING FROM L/H WING PANEL 541CB CONTAINING MEASURING STICK #5 AMM: 28-44-01-4 TRANSFERRED FUEL MEASURING STICK AND BASE PLATE FROM RE
- [SDR FDEA202203180577](https://openairdocs.org/sdr/FDEA202203180577), Mar 18, 2022: NONE. NONE. DURING PERFORMING EA: T G-5710-T0366591 P1, STEP10.D.(4), AT STA1035 LBL70, QTY 01 HOLE REQUEST TO INSTALL BACB30WR5K()LX IN HOLE DIA.0.3232"-0.3252", AND NOW O
- [SDR FDEA202203180576](https://openairdocs.org/sdr/FDEA202203180576), Mar 18, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 241HF FOUND BROKEN. MAIN DECK CARGO FLOOR PANEL 241HF REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1, REV 40.0. REPAIR CLASSIFIED AS 
- [SDR FDEA202203180575](https://openairdocs.org/sdr/FDEA202203180575), Mar 18, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242DF FOUND BROKEN. MAIN DECK CARGO FLOOR PANEL 242DF REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1, REV 40.0. REPAIR CLASSIFIED AS 
- [SDR FDEA202203180574](https://openairdocs.org/sdr/FDEA202203180574), Mar 18, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242GF FOUND BROKEN. MAIN DECK CARGO FLOOR PANEL 242GF REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1, REV 40.0. REPAIR CLASSIFIED AS 
- [SDR FDEA202203180573](https://openairdocs.org/sdr/FDEA202203180573), Mar 18, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242KF FOUND BROKEN. MAIN DECK CARGO FLOOR PANEL 242KF REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1, REV 40.0. REPAIR CLASSIFIED AS 
- [SDR FDEA202203180572](https://openairdocs.org/sdr/FDEA202203180572), Mar 18, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242QF FOUND BROKEN. MAIN DECK CARGO FLOOR PANEL 242QF REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1, REV 40.0. REPAIR CLASSIFIED AS 
- [SDR FDEA202203180571](https://openairdocs.org/sdr/FDEA202203180571), Mar 18, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 241QF FOUND BROKEN. MAIN DECK CARGO FLOOR PANEL 241QF REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1, REV 40.0. REPAIR CLASSIFIED AS 
- [SDR FDEA202203180570](https://openairdocs.org/sdr/FDEA202203180570), Mar 18, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 241PF FOUND BROKEN. MAIN DECK CARGO FLOOR PANEL 241PF REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1, REV 40.0. REPAIR CLASSIFIED AS 
- [SDR FDEA202203180569](https://openairdocs.org/sdr/FDEA202203180569), Mar 18, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242PF FOUND BROKEN. MAIN DECK CARGO FLOOR PANEL 242PF REPAIRED AS PER B777 SRM 53-00-50-2R REPAIR 1,REV 40.0. REPAIR CLASSIFIED AS M
- [SDR FDEA202203180579](https://openairdocs.org/sdr/FDEA202203180579), Mar 18, 2022: DOUBLER. DAMAGED. DURING PERFORMING EA T G-5710-T0366591 P2 STEP 11.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINED S
- [SDR FDEA202203180578](https://openairdocs.org/sdr/FDEA202203180578), Mar 18, 2022: DOUBLER. DAMAGED. DURING PERFORMING EA T G-5710-T0366591 P1 STEP 11.C.(5), FOUND 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 LHS TOO CLOSE TO EDGE OF MACHINED S
- [SDR FDEA2019121313221](https://openairdocs.org/sdr/FDEA2019121313221), Dec 11, 2019: SWITCH. OUT OF POSITION. PDIS 861 25-60 8026 11DEC19 CGN FACT U EMERG LIGHTS SWITCH COVER TURNS OFF SWITCH WHEN CLOSED. CGN U FOUND PULLING MECHANISM OF SWITCH GUARD MOVED OF THE SWITCH
- [SDR FDEA201804221092](https://openairdocs.org/sdr/FDEA201804221092), Apr 22, 2018: CONTROLLER. FAILED. AFTER LEVEL OFF, HAD NO FWD CABIN TEMP CONTROL. RECEIVED A CABIN TEMP ICAS. TROUBLESHOT IAW MOCC. RETURNED TO DEPARTURE. SYSTEM CONFIGURATION OF CH 21 CTC SHOWE
- [SDR FDEA201804060874](https://openairdocs.org/sdr/FDEA201804060874), Apr 6, 2018: LIGHT. INOPERATIVE. DURING A POST FLIGHT INSPECTION, THE L1 DOOR FWD EMERGENCY LIGHT ASSY LESS THAN 10% ILLUMINATED DURING A LIGHT TEST. REMOVED AND REPLACED THE LIGHT ASSY IAW AMM
- [SDR FDEA201712053334](https://openairdocs.org/sdr/FDEA201712053334), Dec 5, 2017: LIGHT. INOPERATIVE. LT DOOR CEILING EMERGENCY LIGHT OUT. AMM: 33-51-03-2, RELAMPED EMERGENCY LIGHT ABOVE L1 DOOR. OPERATIONAL CHECKS GOOD. OK FOR SERVICE.
- [SDR FDEA201605281783](https://openairdocs.org/sdr/FDEA201605281783), May 28, 2016: SLIDE. FAILED. PORT SIDE DOOR SLIDE DEPLOYED BUT DID NOT INFLATE. COCKPIT INDICATIONS INDICATED BOTH DOORS MANUAL. INSTALLED L1 SLIDERAFT ASSY, REF 25-66-01-4.
- [SDR FDEA201512093957](https://openairdocs.org/sdr/FDEA201512093957), Dec 9, 2015: SLIDE. MALFUNCTIONED. WITH DOOR 1L CLOSED & LEVER IN LOCKED POSITION, THE DOOR ARM & DISARM LEVER WILL NOT MOVE TO THE ARMED POSITION. WHILE PERFORMING L1 DOOR SLIDE INSPECTION IAW A
- [SDR FDEA201407021604](https://openairdocs.org/sdr/FDEA201407021604), Jul 2, 2014: STRINGER. DAMAGED. DURING REMOVAL OF FLOOR PANEL RT BULK CARGO COMPARTMENT STATION 1937, BULK CARGO DOORWAY FOUND FLOOR PANEL STRINGER BROKEN. REPAIR CARRIED OUT AS PER B777 SRM 5
- [SDR FDEA201112035133](https://openairdocs.org/sdr/FDEA201112035133), Dec 3, 2011: DISPLAY. FAILED. 20 MINUTES INTO FLIGHT, CAPTAIN`S NAVAGATION DISPLAY BLANKED OUT AFTER ABOUT 5 MINUTES, THE LOWER CENTER DISPLAY BLANKED ALSO A FEW MINUTES LATER BOTH DISPLAYS 

## 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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.