# N868FD: 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: 40674 - Year built: 2015 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: July 22, 2015 - Certificate issued: July 27, 2015 - Expires: July 31, 2028 - Mode S code: ABED10 - 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=868FD - Page: https://openairdocs.org/aircraft/N868FD 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 N868FD. ## FAA accident and incident reports None matched to N868FD. ## Service difficulty reports (8) 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 FDEA202602280291](https://openairdocs.org/sdr/FDEA202602280291), Feb 28, 2026: SAFETY WIRE. WRONG PART. LEFT SLIDE PACKBOARD RELEASE CABLE MECHANISM REQUIRES CAD COPPER SAFETY WIRE. REF FEA G-2560-F0386282 C P1. SAFETIED LT SLIDE PACKBOARD RELEASE CABLE MECHANISH - [SDR FDEA202410141512](https://openairdocs.org/sdr/FDEA202410141512), Oct 14, 2024: POWER SUPPLY. FAILED. DURING F/O INSPECTION, EMERGENCY LIGHT CHECK FAILED. ALL 3 LIGHTS AROUND ENTRY 1L AND THE THREE CLOSEST CEILING LIGHTS TO ENTRY 1L ARE NOT ILLUMINATING. REMOVED - [SDR FDEA202307051151](https://openairdocs.org/sdr/FDEA202307051151), Jul 5, 2023: SKIN. WORN. FOUND FUSELAGE SKIN A ABRASION (DEPTH:0.016 IN) AT STA 1014, S36R-S37R, WHICH EXCEEDS 0.005 IN DEPTH. COMPLETED AS PER EA G-5710-T0375107 P2 STEP 1. REPAIR CLAS - [SDR FDEA202306281117](https://openairdocs.org/sdr/FDEA202306281117), Jun 28, 2023: FLOOR PANEL. DAMAGED. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-17 FOUND PUNCTURED AT STA 1288 LBL92. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8452-17 PUNCTURED AT STA 1288 LBL92 - [SDR FDEA202306281116](https://openairdocs.org/sdr/FDEA202306281116), Jun 28, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8652-1 FOUND CRACKED AT STA 1434 LBL109. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8652-1 CRACKED AT STA 1434 LBL109, TH - [SDR FDEA202306281115](https://openairdocs.org/sdr/FDEA202306281115), Jun 28, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8452-21 FOUND CRACKED AT STA 1359 LBL45. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N: 152W8452-21 CRACKED AT STA 1359 LBL45. - [SDR FDEA202303140421](https://openairdocs.org/sdr/FDEA202303140421), Mar 14, 2023: WHEEL. FAILED. FOUND #3 WHEEL WITH SKIDDING DAMAGE THAT CAUSED TIRE TO BURST. ACCOMPLISHED AMM 05-51-16-2 TIRE BURST INPECTION. NO FINDINGS. REMOVED AND REPLACED #3 MAIN WHEEL - [SDR FDEA202011242951](https://openairdocs.org/sdr/FDEA202011242951), Nov 24, 2020: FLOOR SUPPORT. CRACKED. LOWER BULK CARGO COMPARTMENT FLOOR STRINGER FOUND CRACK AT STATION 1937 RIGHT BUTT LINE 41.5. LOWER BULK CARGO COMPARTMENT FLOOR STRINGER AT STATION 1937 RIGHT ## 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.