# N854FD: 2010 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: 37725
- Year built: 2010
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 2, 2010
- Certificate issued: September 3, 2010
- Expires: May 31, 2028
- Mode S code: ABB6B5
- 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=854FD
- Page: https://openairdocs.org/aircraft/N854FD

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 N854FD.

## FAA accident and incident reports

None matched to N854FD.

## Service difficulty reports (30)

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 FDEA202608221218](https://openairdocs.org/sdr/FDEA202608221218), Aug 22, 2026: POWER SUPPLY. INOPERATIVE. DURING SERVICE CHECK, FOUND EXTERIOR RT EMERGENCY LIGHT NOT WORKING. RT EMERGENCY LIGHT POWER SUPPLY REPLACED IAW AMM 33-51-06-2. TESTED OK.
- [SDR FDEA202603200359](https://openairdocs.org/sdr/FDEA202603200359), Mar 20, 2026: SKIN. DENTED. RIGHT WING OTBD FLAP LOWER SURFACE FROM OB TO IB 272 INCHES CROSS TE TO LE 12 INCHES FOUND ONE DENT. REPAIRED RH WING OB FLAP LOWER SURFACE DENT AT OTEF STA 250
- [SDR FDEA202603170356](https://openairdocs.org/sdr/FDEA202603170356), Mar 17, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285G P12 STEP 3.B.(1) & STEP 5.A.(2) THEN FOUND 02EA CRACK ON UPPER WING SKIN FASTENER NR 5. RH WING UPPER SKIN #5 HOLE CR
- [SDR FDEA202603160354](https://openairdocs.org/sdr/FDEA202603160354), Mar 16, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285G P11 STEP 3.B.(1)& STEP 5.A.(2) THEN FOUND 01EA CRACK ON UPPER WING SKIN FASTENER #5. LT WING UPPER SKIN #5 HOLE CRACK
- [SDR FDEA202603050315](https://openairdocs.org/sdr/FDEA202603050315), Mar 5, 2026: LAMP. INOPERATIVE. DURING POSTFLIGHT, FOUND R1 DOOR SLIDE EMERGENCY LIGHT INOP. REPLACED THE LAMPS, R1 DOOR SLIDE EMERGENCY EXTERIOR LIGHT 777 AMM. OPS CHECKED GOOD. ACFT OK FOR S
- [SDR FDEA202402240211](https://openairdocs.org/sdr/FDEA202402240211), Feb 24, 2024: LAMP. FAILED. PRE-FLT MX INSP, GALLEY OVRHD (1EA) EMERGENCY LT INOP. AMM: 33-50-00-2 RELAMPED, REF B777 AMM: 33-50-00-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA202112083049](https://openairdocs.org/sdr/FDEA202112083049), Dec 8, 2021: NONE. UNKNOWN. PDIS 854 28-41 2132 08DEC21 ANC APPROX 2.5 HRS INTO FLT HAD FUEL IMBALANCE ON EICAS. AS WE RAN ECL WE NOTICED DISCREPANCIES IN TOTALIZER FUEL AND CALCULATED FUE
- [SDR FDEA202110022447](https://openairdocs.org/sdr/FDEA202110022447), Oct 2, 2021: NONE. NONE. MDIS 854 05-50 1962 02OCT21 KIX REPORTED FOR CAPTAIN EE# 216581 REF WRI 05-50-1960 KIX RWY 06L WIND 060 AT 5 KT MANUAL LANDING FROM RIGHT SEAT, HIGH SINK RATE L
- [SDR FDEA202102180393](https://openairdocs.org/sdr/FDEA202102180393), Feb 18, 2021: SKIN. DAMAGED. WHILE ACCOMPLISHING RIGHT HAND E.O. #G-5310-E0332629 I P6 FOUND NEW FUSELAGE SKIN DOUBLER (P/N: 143W2314Y406) EXISTING HOLE AT STATION 998 STRINGER S-35 RIGHT N
- [SDR FDEA202102180392](https://openairdocs.org/sdr/FDEA202102180392), Feb 18, 2021: SKIN. DAMAGED. WHILE ACCOMPLISHING LEFT HAND E.O. #G-5310-E0332629 I P5 FOUND NEW FUSELAGE SKIN DOUBLER (P/N: 143W2314Y405) EXISTING HOLE AT STATION 998 STRINGER S-35 LEFT NEA
- [SDR FDEA202102180397](https://openairdocs.org/sdr/FDEA202102180397), Feb 18, 2021: SPAR. DAMAGED. WHILE PERFORMING LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR REPAIR (SNRM NO. N00486) FOUND 01 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD THROU
- [SDR FDEA202102180396](https://openairdocs.org/sdr/FDEA202102180396), Feb 18, 2021: SPAR. DAMAGED. WHILE PERFORMING LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR REPAIR (SNRM NO. N00486) FOUND 01 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD STATI
- [SDR FDEA202102180395](https://openairdocs.org/sdr/FDEA202102180395), Feb 18, 2021: SPAR. DAMAGED. WHILE PERFORMING RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (SNRM NO. N00487) FOUND 01 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD THROUGH WEB
- [SDR FDEA202102180394](https://openairdocs.org/sdr/FDEA202102180394), Feb 18, 2021: SPAR. DAMAGED. WHILE PERFORMING RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (SNRM NO. N00487) FOUND 01 EACH EXISTING OVERSIZED HOLE AT LOWER CHORD STATION 103
- [SDR FDEA202102160363](https://openairdocs.org/sdr/FDEA202102160363), Feb 16, 2021: SKIN. CRACKED. DURING ACCOMPLISMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND AROU
- [SDR FDEA202102160364](https://openairdocs.org/sdr/FDEA202102160364), Feb 16, 2021: SKIN. CRACKED. DURING ACCOMPLISMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON LEFT HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER H
- [SDR FDEA202102160362](https://openairdocs.org/sdr/FDEA202102160362), Feb 16, 2021: SKIN. CRACKED. DURING ACCOMPLISMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND HAND FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND AROU
- [SDR FDEA202102160361](https://openairdocs.org/sdr/FDEA202102160361), Feb 16, 2021: STRUCTURE. CRACKED. DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT AS PER EO EO NO: E G-5310-E0332629 I P6 ON REMOVED FASTENER HOLES AND FOUND (01 EA) CRACK IN
- [SDR FDEA202102160360](https://openairdocs.org/sdr/FDEA202102160360), Feb 16, 2021: STRUCTURE. CRACKED. DURING HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT AS PER EO NO: E G-5310-E0332629 I P5 ON REMOVED FASTENER HOLES AND FOUND (01 EA) CRACK INDIC
- [SDR FDEA202010292692](https://openairdocs.org/sdr/FDEA202010292692), Oct 29, 2020: VALVE. FAILED. PDIS 854 28-30 0702 29OCT20 ANC OPEN U. AFTER DUMPING FUEL. FUEL JET NOZZLE RIGHT ILLUMINATED AND THE RIGHT JET VALVE CONTINUED TO DUMP WHEN DUMP WAS TERMINATED
- [SDR FDEA2020070671373](https://openairdocs.org/sdr/FDEA2020070671373), Jun 27, 2020: RELAY. FAILED. AT 6000' ON DESCENT WITH AUTOPILOT ENGAGED GOT SEVERAL EICAS INDICATIONS ON NOTICEABLE "THUMP" EICAS AND STATUS MSG INCLUDED : ALT CALLOUTS, TERR POSS, SATCOM, 
- [SDR FDEA2020063071373](https://openairdocs.org/sdr/FDEA2020063071373), Jun 27, 2020: UNKNOWN. MALFUNCTIONED. AT 6000' ON DESCENT WITH AUTOPILOT ENGAGED GOT SEVERAL EICAS INDICATIONS ON NOTICEABLE "THUMP" EICAS AND STATUS MSG INCLUDED: ALT CALLOUTS, TERR POSS, SATCOM, N
- [SDR FDEA201810303050](https://openairdocs.org/sdr/FDEA201810303050), Oct 30, 2018: SWITCH. DEFECTIVE. DURING PREFLIGHT OBSERVER SEAT OXYGEN MASK "PRESS TO TEST" SWITCH GETS STUCK IN DOWN POSITION. REMOVED AND REPLACED 1ST OBSERVER OXY STORAGE BOX, OPS CK'S NORMA
- [SDR FDEA201511183682](https://openairdocs.org/sdr/FDEA201511183682), Nov 18, 2015: INTERCOSTAL. DAMAGED. WHILE ACCOMPLISHING EA G-5310-T0312163 PART 2. FLOOR INTERCOSTAL DRILL HOLE DAMAGED. REPAIR CLASSIFIED AS MAJOR REPAIR IAW GMM 6-2-100.
- [SDR FDEA201402020237](https://openairdocs.org/sdr/FDEA201402020237), Feb 2, 2014: SPRING. LOOSE. WHEN GUARD TO EMERGENCY LIGHTS SWITCH IS CLOSED, EMERGENCY LIGHTS REMAIN IN THE OFF POSITION. FOUND SPRING OF GUARD LOOSE. SPRING REINSTALLED IN GOOD POSITION. 
- [SDR FDEA201208243147](https://openairdocs.org/sdr/FDEA201208243147), Aug 24, 2012: BULB. INOPERATIVE. ONE EMERGENCY EXIT LIGHT INOPERATIVE. DURING EMERGENCY EXIT LIGHT TEST. R & R BULB IAW SMP. OPS TEST OK IAW MM 33-51-00-5. ACFT OK FOR SERVICE.
- [SDR FDEA201203160994](https://openairdocs.org/sdr/FDEA201203160994), Mar 16, 2012: TIRE. LEAKING. 40 MINUTES AFTER REACHING CRUISE, RECEIVED TIRE PRESSURE EICAS ALERT. PRESSURE WAS LOW ON TIRE NR 10. PRESSURE WENT FROM 204 -114 OVER AN HOUR, DIVERTED. INSPEC
- [SDR FDEA201103040842](https://openairdocs.org/sdr/FDEA201103040842), Mar 4, 2011: LAMP. INOPERATIVE. LT ENTRY DOOR EMERGENCY LIGHT INOP. RELAMPED, REF:B777, AMM 33-51-04-2, OPERATIONAL CHECKS GOOD. FINAL CLOSED.
- [SDR FDEA201011024206](https://openairdocs.org/sdr/FDEA201011024206), Nov 2, 2010: BULB. FAILED. 2EA OVERHEAD EMER LIGHTS DID NOT ILLUMINATE DURING TEST IN CABIN AREA. REPLACED EMER LTS LAMP 2EA (MPN 1317)OPS CHECKED NML IAW AMM 33-51-03-20.
- [SDR FDEA201009253709](https://openairdocs.org/sdr/FDEA201009253709), Sep 25, 2010: BATTERY PACK. INOPERATIVE. R1 DOOR EPAS BATTERY PACK TEST LIGHT IS NOT BLINKING GREEN AS REQUIRED. REMOVED R1 EPAS BATTERY PACK AND REPLACED INTERNAL BACKUP BATTERIES IAW AMM 52-11-20-4.

## 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

---
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.