# N858FD: 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: 37729
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 1, 2011
- Certificate issued: June 30, 2011
- Expires: June 30, 2027
- Mode S code: ABC591
- 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=858FD
- Page: https://openairdocs.org/aircraft/N858FD

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 N858FD.

## FAA accident and incident reports

None matched to N858FD.

## 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 FDEA202602160217](https://openairdocs.org/sdr/FDEA202602160217), Feb 16, 2026: SAFETY WIRE. WRONG PART. LEFT SLIDE ASSY. SN 3359, FOUND BREAK AWAY WIRE SECURES THE RELEASE MECHANISM NOT TO BE CLAD-PLATED COPPER WIRE. RELEASED FOR SERVICE PER MEL : 52-11-01-02 CATE
- [SDR FDEA202602120183](https://openairdocs.org/sdr/FDEA202602120183), Feb 12, 2026: WIRE. WRONG PART. FOUND BREAKAWAY WIRE THAT SECURES THE RELEASE MECHANISM NOT TO BE CLAD-PLATED COPPER WIRE. REMOVED LT DOOR SLIDE IAW MM 25-66-01-4. REMOVED STAINLESS SAFETY WIR
- [SDR FDEA202403210329](https://openairdocs.org/sdr/FDEA202403210329), Mar 21, 2024: SKIN. CRACKED. LH WING NO.7 SLAT OUTER SKIN FOUND CRACK AT ISS193. CRACK LENGTH 1.44 INCHES, NUMBER OF CRACK: 01 EA. LH WING NO.7 SLAT OUTER SKIN CRACKED AREA REPAIRED AS PER 
- [SDR FDEA202403140284](https://openairdocs.org/sdr/FDEA202403140284), Mar 14, 2024: SKIN. DENTED. RH WING OB FLAP LWR SURFACE FOUND DENT AT 261 IN AWAY FROM OB EDGE AND 6 IN AWAY FROM AFT EDGE. EVALUATED RH WING OB FLAP LWR SURFACE DENT AT 261 IN AWAY FROM O
- [SDR FDEA202403140283](https://openairdocs.org/sdr/FDEA202403140283), Mar 14, 2024: SKIN. DENTED. RH WING OB FLAP LWR SURFACE FOUND DENT AT 257 IN AWAY FROM OB EDGE AND 14.5 IN AWAY FROM AFT EDGE. EVALUATED RH WING OB FLAP LWR SURFACE DENT AT 257 IN AWAY FRO
- [SDR FDEA202107281886](https://openairdocs.org/sdr/FDEA202107281886), Jul 28, 2021: UNKNOWN. ODOR. AFTER BLOCK-IN AND SHUTDOWN ENTIRE CREW SMELLED AN ELECTRICAL TYPE BURNING SMELL IN THE GALLEY. THIS WAS SLIGHTLY NOTICEABLE DURING THE FLIGHT AND THE RFO WHO W
- [SDR FDEA202106231585](https://openairdocs.org/sdr/FDEA202106231585), Jun 23, 2021: FLOOR PANEL. CRACKED. MAIN DECK FLOOR PNL P/N:152W8652-16 FOUND CRACKED AT STA 1622 RBL75. THE CARACKED MAIN DECK FLOOR PNL P/N:152W8652-16 AT STA 1622 RBL 75 REPAIRED AS PER B777 SR
- [SDR FDEA202106231584](https://openairdocs.org/sdr/FDEA202106231584), Jun 23, 2021: FLOOR PANEL. CRACKED. MAIN DECK FLOOR PNL P/N: 152W8652-4 FOUND CRACKED AT STA 1455 RBL 60. THE CARACKED MAIN DECK FLOOR PNL P/N:152W8652-4 AT STA 1455 RBL 60 REPAIRED AS PER B777 SR
- [SDR FDEA202106231583](https://openairdocs.org/sdr/FDEA202106231583), Jun 23, 2021: FLOOR PANEL. CRACKED. MAIN DECK FLOOR PNL P/N: 152W8652-6 FOUND CRACKED AT STA 1470 RBL 33. THE CARACKED MAIN DECK FLOOR PNL P/N:152W8652-6 AT STA 1470 RBL 33 REPAIRED AS PER B777 SR
- [SDR FDEA202106231582](https://openairdocs.org/sdr/FDEA202106231582), Jun 23, 2021: FLOOR PANEL. CRACKED. MAIN DECK FLOOR PNL P/N: 152W8652-3 FOUND CRACKED AT STA 1488 LBL53. THE CARACKED MAIN DECK FLOOR PNL P/N:152W8652-3 AT STA 1488 LBL 53 REPAIRED AS PER B777 SRM
- [SDR FDEA202106231581](https://openairdocs.org/sdr/FDEA202106231581), Jun 23, 2021: FLOOR PANEL. CRACKED. MAIN DECK FLOOR PNL P/N:152W8452-21 FOUND CRACKED AT STA 1325 LBL 43. THE CRACKED MAIN DECK FLOOR PNL P/N:152W8452-21 AT STA 1325 LBL 43 REPAIRED AS PER B777 SR
- [SDR FDEA202106231580](https://openairdocs.org/sdr/FDEA202106231580), Jun 23, 2021: FLOOR PANEL. CRACKED. MAIN DECK FLOOR PNL P/N: 152W8452-19 FOUND CRACKED AT STA 1355 LBL 25. THE CRACKED MAIN DECK FLOOR PNL P/N:152W8452-19 AT STA 1355 LBL 25 REPAIRED AS PER B777 S
- [SDR FDEA201909202294](https://openairdocs.org/sdr/FDEA201909202294), Sep 20, 2019: TIRE. LOW PRESSURE. 20 MINUTES INTO FLIGHT, REC'D TIRE PRESS EICAS. #12 TIRE SHOWED 199 PSI AT 1 HOUR 30 MINUTES SHOWS 173PSI ALL OTHER TIRES PRESSURE APPROX 235 PSI. PRESSURE ON L
- [SDR FDEA201712283459](https://openairdocs.org/sdr/FDEA201712283459), Dec 28, 2017: LAMP. BURNED OUT. EMERGENCY LIGHTS REMAINED ON DURING PREFLIGHT. RED LIGHT ILLUMINATED IN THE GUARDED SWITCH. PERFORMED AN EMERGENCY LIGHT TEST IAW MM 33-51-00-05, AND FOUND ONE 
- [SDR FDEA201711183271](https://openairdocs.org/sdr/FDEA201711183271), Nov 18, 2017: DOOR. BINDING. THERE WAS A LOT OF RESISTANANCE WHEN ATTEMPTED TO OPEN L1 DOOR. LEFT DOOR CLOSED. USED R1 DOOR. VERIFIED ARM & DIARM FUNCTION WAS OK AND L1 DOOR POSSIBLE TO OPE
- [SDR FDEA201607242610](https://openairdocs.org/sdr/FDEA201607242610), Jul 24, 2016: FLOOR SUPPORT. CRACKED. BULK CARGO FLOOR SUPPORT AT BS 1980.5 APPROXIMATELY AT RBL 34 FOUND CRACKED.
- [SDR FDEA201412124117](https://openairdocs.org/sdr/FDEA201412124117), Dec 12, 2014: LIGHT. INOPERATIVE. EMERGENCY CEILING LIGHT IN CABIN AREA NEAR L1 DOOR WOULD NOT ILLUMINATE DURING TEST. R & R THE LIGHT IAW AMM 33-51-03-2. ACFT OK FOR SERVICE.

## 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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