# N895FD: 2013 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: 41749
- Year built: 2013
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 14, 2013
- Certificate issued: November 15, 2013
- Expires: November 30, 2029
- Mode S code: AC5868
- 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=895FD
- Page: https://openairdocs.org/aircraft/N895FD

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 N895FD.

## FAA accident and incident reports

None matched to N895FD.

## Service difficulty reports (33)

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 FDEA202603020314](https://openairdocs.org/sdr/FDEA202603020314), Mar 2, 2026: SLIDE. FAULTED. UPON CLOSING THE AIRCRAFT ENTRY DOOR AND ARMING THE EVACUATION SLIDES, F/O NOTICED AN FSS FAULT ON POSITIONS 13L AND 13R. F/O OPENED THE DOOR TO SEE IF THE FAUL
- [SDR FDEA202603020304](https://openairdocs.org/sdr/FDEA202603020304), Mar 2, 2026: SLIDE. UNWANTED DEPLOY. UPON CLOSING THE ACFT ENTRY DOOR AND ARMING THE EVACUATION SLIDES, F/O NOTICED AN FSS FAULT ON POSITIONS 13L & 13R. F/O OPENED THE DOOR TO SEE IF THE FAULTS WOU
- [SDR FDEA202511232199](https://openairdocs.org/sdr/FDEA202511232199), Nov 23, 2025: MODULATING VALVE. FAILED. DURING DESCENT, FLIGHT DECK TEMP EXCESSIVELY COLD. RAN ECL CABIN TEMP COLD CHECKLIST WITHOUT IMPROVEMENT. DESCENDED FOR MANUAL VENTILATION. FLIGHT DECK TEMP REA
- [SDR FDEA202506010826](https://openairdocs.org/sdr/FDEA202506010826), Jun 1, 2025: SWITCH. INOPERATIVE. EMERGENCY EXIT LIGHTS REMAIN ON AFTER CLOSING AND ARMING 1L AND 1R. SLAVED IN NEW L1 DOOR OPEN SWITCH (S52125) AND DOOR ARMING/EMERGENCY LIGHTS OPERATED NORMAL.
- [SDR FDEA202404110454](https://openairdocs.org/sdr/FDEA202404110454), Apr 11, 2024: SKIN. DAMAGED. RH WING OB FLAP LWR SURFACE 2 IN AWAY TO AFT EDGE,4 IN AWAY TO OB FOUND A REPAIR IN POOR CONDITION. RE-REPAIRED RH WING OB FLAP LWR SURFACE AT OTEF STA514 EXIST
- [SDR FDEA202404070446](https://openairdocs.org/sdr/FDEA202404070446), Apr 7, 2024: SKIN. CRACKED. RH WING NO.8 SLAT EXTERNAL UPP SURFACE FOUND CRACKED AT ISS184. CRACK LENGTH:0.3 INCH, NUMBER OF CRACK: 01EA. RH WING NO.8 SLAT EXTERNAL UPR SURFACE CRACKED ARE
- [SDR FDEA202305220916](https://openairdocs.org/sdr/FDEA202305220916), May 22, 2023: UNKNOWN. UNKNOWN. ON CLIMB OUT OF ICN TIRE PRESS EICAS. RAN CHECKLIST AND GEAR SYNOPSIS SHOWED RIGHT NOSE GEAR TIRE PRESSURE AT 54 PSI. IT EVENTUALLY WENT TO 0. LANDED AT CAN AND
- [SDR DALA2022120607829](https://openairdocs.org/sdr/DALA2022120607829), May 22, 2023: UNKNOWN. UNKNOWN. ON CLIMB OUT OF ICN TIRE PRESS EICAS. RAN CHECKLIST AND GEAR SYNOPSIS SHOWED RIGHT NOSE GEAR TIRE PRESSURE AT 54 PSI. IT EVENTUALLY WENT TO 0. LANDED AT CAN AND
- [SDR FDEA202109302434](https://openairdocs.org/sdr/FDEA202109302434), Sep 30, 2021: NONE. DAMAGED. CLIMBING THROUGH 9000 ON DEPARTURE EICAS DOOR AFT CARGO WITH MASTER CAUTION - ACCOMPLISHED CHECKLIST , JETTISONED 11000 POUNDS OF FUEL AND RETURNED TO PANC COMP
- [SDR FDEA202108122003](https://openairdocs.org/sdr/FDEA202108122003), Aug 12, 2021: SKIN. CRACKED. FOUND AFT LARGE CARGO DOOR INNER UPPER SKIN CRACK AT STA 1718. AFT LARGE CARGO DOOR AT STA 1718 INNER UPPER CRACKED SKIN REPAIRED AS PER EA G-5232-T0363395 P1 .
- [SDR FDEA202108061966](https://openairdocs.org/sdr/FDEA202108061966), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-19 FOUND CRACK AT STA 1355 LBL18. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-19 STA 1355 LBL 18 REPAIRED AS PER B777 SRM5
- [SDR FDEA202108061965](https://openairdocs.org/sdr/FDEA202108061965), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8652-5 FOUND CRACK AT STA 1434 LBL10. MAIN DECK CARGO FLOOR PANEL P/N:152W8652-5 STA 1434 LBL 10 REPAIRED AS PER B777 SRM53-
- [SDR FDEA202108061964](https://openairdocs.org/sdr/FDEA202108061964), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-13 FOUND CRACK AT STA 1267 LBL22. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-13 STA 1267 LBL 22 REPAIRED AS PER B777 SRM5
- [SDR FDEA202108061963](https://openairdocs.org/sdr/FDEA202108061963), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-21 FOUND CRACK AT STA 1348 LBL48 MAIN DECK CARGO FLOOR PANEL P/N:152W8452-21 STA 1348 LBL 48 REPAIRED AS PER B777 SRM53
- [SDR FDEA202108061962](https://openairdocs.org/sdr/FDEA202108061962), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-11 FOUND CRACK AT STA 1153 LBL91. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-11 STA 1153 LBL 91 REPAIRED AS PER B777 SRM5
- [SDR FDEA202108061961](https://openairdocs.org/sdr/FDEA202108061961), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-7 FOUND CRACK AT STA 1150 LBL22. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-7 STA 1150 LBL 22 REPAIRED AS PER B777 SRM 53
- [SDR FDEA202108061960](https://openairdocs.org/sdr/FDEA202108061960), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-22 FOUND CRACK AT STA 1351 RBL55. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-22 STA 1351 RBL 55 REPAIRED AS PER B777 SRM5
- [SDR FDEA202108061959](https://openairdocs.org/sdr/FDEA202108061959), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8652-4 FOUND CRACK AT STA 1455 RBL76. MAIN DECK CARGO FLOOR PANEL P/N:152W8652-4 STA 1455 RBL 76 REPAIRED AS PER B777 SRM53-
- [SDR FDEA202108061958](https://openairdocs.org/sdr/FDEA202108061958), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8652-2 FOUND CRACK AT STA 1434 RBL108 MAIN DECK CARGO FLOOR PANEL P/N:152W8652-2 STA 1434 RBL 108 REPAIRED AS PER B777 SRM 5
- [SDR FDEA202108061957](https://openairdocs.org/sdr/FDEA202108061957), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-14 FOUND CRACK AT STA 1247 RBL38. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-14 STA 1247 RBL 38 REPAIRED AS PER B777 SRM5
- [SDR FDEA202108061956](https://openairdocs.org/sdr/FDEA202108061956), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-20 FOUND CRACK AT STA 1398 RBL35. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-20 STA 1398 RBL 35 REPAIRED AS PER B777 SRM5
- [SDR FDEA202108061955](https://openairdocs.org/sdr/FDEA202108061955), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8652-6 FOUND CRACK AT STA 1490 RBL 33. MAIN DECK CARGO FLOOR PANEL P/N:152W8652-6 STA 1490 RBL 33 REPAIRED AS PER B777 SRM 5
- [SDR FDEA202108061954](https://openairdocs.org/sdr/FDEA202108061954), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-26 FOUND CRACK AT STA 1398 LBL10. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-26 STA 1398 LBL 10 REPAIRED AS PER B777 SRM5
- [SDR FDEA202108061953](https://openairdocs.org/sdr/FDEA202108061953), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-25 FOUND CRACK AT STA 1300 RBL 8. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-25 STA 1300 RBL 8 REPAIRED AS PER B777 SRM 5
- [SDR FDEA202108061952](https://openairdocs.org/sdr/FDEA202108061952), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N :152W8452-28 FOUND CRACK AT STA 1120 RBL 38. MAIN DECK CARGO FLOOR PANEL P/N:152W8452-28 STA 1120 RBL 38 REPAIRED AS PER B777 SR
- [SDR FDEA202108061951](https://openairdocs.org/sdr/FDEA202108061951), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8452-2 FOUND CRACK AT STA 1100 RBL22 MAIN DECK CARGO FLOOR PANEL P/N:152W8452-2 STA 1100 RBL 22 REPAIRED AS PER B777 SRM 53
- [SDR FDEA202108061950](https://openairdocs.org/sdr/FDEA202108061950), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8452-12 FOUND CRACK AT STA 1245 RBL 90 MAIN DECK CARGO FLOOR PANEL P/N:152W8452-12 STA 1245 RBL 90 REPAIRED AS PER B777 SRM
- [SDR FDEA202108061949](https://openairdocs.org/sdr/FDEA202108061949), Aug 6, 2021: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N :152W8450-1 FOUND CRACK AT STA 1043 LBL8 MAIN DECK CARGO FLOOR PANEL P/N:152W8450-1 STA 1043 LBL 8 REPAIRED AS PER B777 SRM 53-0
- [SDR FDEA201901180164](https://openairdocs.org/sdr/FDEA201901180164), Jan 18, 2019: FLOOR SUPPORT. CRACKED. BULK CARGO COMPARTMENT STATION 1937, RIGHT BUTTOCK LINE 41 FLOOR PANEL STRINGER FOUND WITH CRACK. BULK CARGO COMPARTMENT STATION 1937 RIGHT BUTTOCK LINE 41 FLOO
- [SDR FDEA201410213317](https://openairdocs.org/sdr/FDEA201410213317), Oct 21, 2014: FIRE BOTTLE. FAULTY. MULTI-FUNCTION DISPLAY STATUS PAGE SHOWED MSG CGO BOTTLE 2A, 2B & 2C. DURING ACFT POWER UP WIRING CONTINUITY CHECK CARRIED OUT ON CGO FIRE EXTINGUISHING BOTTLE 
- [SDR FDEA201409232713](https://openairdocs.org/sdr/FDEA201409232713), Sep 23, 2014: FIRE BOTTLE. DISCHARGED. AFTER ACFT POWER UP, FOUND STATUS MSG BOTTLE 2A CARGO, BOTTLE 2B CARGO & BOTTLE 2C CARGO ON MFD. 2A,2B,2C FIRE EXTINGUISHER BOTTLE DISCHARGED. R&R LOWER CARGO F
- [SDR FDEA201312122972](https://openairdocs.org/sdr/FDEA201312122972), Dec 12, 2013: UNKNOWN. MALFUNCTIONED. AFTER LANDING THE STEERING TILLER WAS FROZEN & WOULD NOT TURN THE ACFT. CAPTAIN & FIRST OFFICER APPLYING PRESS, THE TILLER BROKE LOOSE & ACFT STEERING RETURNED 
- [SDR FDEA201311222853](https://openairdocs.org/sdr/FDEA201311222853), Nov 22, 2013: SOCKET. DEFECTIVE. L1 DOOR EMERGENCY EXTERIOR SLIDE LIGHT INTERMITTENT. REPLACED LIGHT SOCKET IAW AMM 33-51-04-2.

## 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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