# N855FD: 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: 37726
- Year built: 2010
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: September 8, 2010
- Certificate issued: September 9, 2010
- Expires: May 31, 2028
- Mode S code: ABBA6C
- 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=855FD
- Page: https://openairdocs.org/aircraft/N855FD

From the FAA registry file of October 20, 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 N855FD.

## FAA accident and incident reports

None matched to N855FD.

## Service difficulty reports (32)

As reported by operators and repair stations.

- [SDR FDEA202605140595](https://openairdocs.org/sdr/FDEA202605140595), May 14, 2026: SKIN. DEBONDED. LEFT OTBD FLAP LWR SURFACE FROM OTBD TO INBD 268 INCHES CROSS TE TO LE 10 INCHES FOUND DEBONDED. REPAIRED LH OB FLAP LWR SURFACE DISBOND AT OTEF STA 260 AS PER 
- [SDR FDEA202605110581](https://openairdocs.org/sdr/FDEA202605110581), May 11, 2026: SKIN. BULGED. FOUND RT WING LE NR 11 SLAT EXTERNAL SURFACE A BULGE AT STA 873. BULGE REPAIRED AS PER B777 SRM57- 43-01-2R REPAIR 9 FIGURE 202 REV:51.0 AND EA G-5750-T0387321 
- [SDR FDEA202605110580](https://openairdocs.org/sdr/FDEA202605110580), May 11, 2026: SKIN. BULGED. FOUND RT WING LE NR 9 SLAT EXTERNAL SURFACE A BULGE AT STA 564. BULGE REPAIRED AS PER B777 SRM57-43- 01-2R REPAIR 16 FIGURE 202 REV:53.0. AND EA G-5750-T0387322
- [SDR FDEA202605100579](https://openairdocs.org/sdr/FDEA202605100579), May 10, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285 G P12 STEP3.B & STEP5.A.(2) THEN FOUND 01EA CRACK ON THE RH UPPER WING SKIN FASTENER #5. RH UPPER WING SKIN RIB BAY 10
- [SDR FDEA202605100578](https://openairdocs.org/sdr/FDEA202605100578), May 10, 2026: SKIN. CRACKED. DURING PERFORM WORK CARD:EG-5710-E0376285 G P11 STEP3.B & STEP5.A.(2) FOUND TWO CRACKS ON THE LT UPPER WING SKIN FASTENER #5. H WING UPPER SKIN IN RIB BAY 10 TR
- [SDR FDEA202508181496](https://openairdocs.org/sdr/FDEA202508181496), Aug 18, 2025: POWER SUPPLY. NO TEST. 2 EMERGENCY LIGHTS IN COURIER AREA ABOVE R1 ARE INOP. ONE INOPERATIVE LIGHT LOCATED ABOVE GALLEY AREA, SECOND INOPERATIVE LIGHT LOCATED NEAR R1 DOOR. AMM: 33-51
- [SDR FDEA202410091453](https://openairdocs.org/sdr/FDEA202410091453), Oct 9, 2024: THROTTLE CONTROL. MALFUNCTIONED. DURING LEFT ENGINE START, WITH THE RIGHT ENGINE SHUTDOWN, BOTH THROTTLES ADVANCED UNCOMMANDED TOWARDS MAX POWER. CREW PULLED BOTH THROTTLES TO FLIGHT IDLE AND A
- [SDR FDEA202308151433](https://openairdocs.org/sdr/FDEA202308151433), Aug 15, 2023: FLAP. DENTED. LH OB FLAP LWR SURFACE FROM IB TO OB 330 INCH CROSS LE TO TE 43 INCH FOUND ONE DENT. EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 330 INCH CROSS LE TO TE 43 I
- [SDR FDEA202308101393](https://openairdocs.org/sdr/FDEA202308101393), Aug 10, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8402-17) AT STA1290/LBL105.5-107.5 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 241MF(P/N:152W8402-17)
- [SDR FDEA202308101392](https://openairdocs.org/sdr/FDEA202308101392), Aug 10, 2023: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8402-18) AT STA1269.5/RBL81-83.25 FOUND CRACK(OFF WING). EVALUATED MAIN DECK CARGO FLOOR PANEL 242KF(P/N:152W8402-18) 
- [SDR FDEA202308081373](https://openairdocs.org/sdr/FDEA202308081373), Aug 8, 2023: SKIN. CORRODED. FOUND THE LOWER FUSELAGE SKIN CORROSION INSIDE BODY FAIRING 192JR AT BS 930 TO BS 940 AND S-49L TO S-49R. THE LOWER FUSELGE SKIN CORRODED AREA AT BS 930 TO BS 9
- [SDR FDEA202101280212](https://openairdocs.org/sdr/FDEA202101280212), Jan 28, 2021: SKIN. CRACKED. DURING ACCOMPLISHMENT OF HFEC INSPECTION ON RH FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATIONS AROUND 01 EA FASTENER HOLE AT STA 1033 STR 37
- [SDR FDEA202101150117](https://openairdocs.org/sdr/FDEA202101150117), Jan 15, 2021: DOUBLER. MISINSTALLED. WHILE ACCOMPLISHING LH E.O.#G-5310-E0332629 I P5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STA 998 STR. S-35L NEAR MILLED EDGE COMPLIED WITH E.A.#:G-5310
- [SDR FDEA202101150116](https://openairdocs.org/sdr/FDEA202101150116), Jan 15, 2021: DOUBLER. MISINSTALLED. WHILE ACCOMPLISHING RH E.O.#G-5310-E0332629 I P6 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STA 998 STR. S-35R NEAR MILLED EDGE. COMPLIED WITH E.A.#:G-531
- [SDR FDEA202101150115](https://openairdocs.org/sdr/FDEA202101150115), Jan 15, 2021: SKIN. CRACKED. DURING ACCOMPLISHMENT OF HFEC INSPECTION ON RH FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATIONS AROUND 01 EA FASTENER HOLE STA 1028 STR 37R, 
- [SDR FDEA202101150109](https://openairdocs.org/sdr/FDEA202101150109), Jan 15, 2021: SPAR. CRACKED. DURING HFEC OPEN HOLE INSPECTION CARRIED OUT AS PER EO NO:E G-5310-E0332629 I P6 ON OVERSIZED FASTENER HOLES AND FOUND (01 EA) CRACK INDICATION ON RHS VERTICAL 
- [SDR FDEA202101150114](https://openairdocs.org/sdr/FDEA202101150114), Jan 15, 2021: SKIN. CRACKED. DURING ACCOMPLISHMENT OF HFEC INSPECTION ON LH FUSELAGE SKIN COMMON TO UNDERWING LONGERON, FOUND CRACK INDICATION AROUND FASTENER HOLE AT STA 1033 STR 37L, APPR
- [SDR FDEA202101110038](https://openairdocs.org/sdr/FDEA202101110038), Jan 11, 2021: FLOOR SUPPORT. CRACKED. LOWER BULK CARGO COMPARTMENT STATION 1937, RIGHT BUTT LINE 41 FLOOR STRINGER FOUND WITH CRACK AS MARK. LOWER BULK CARGO COMPARTMENT STATION 1937 RIGHT BUTT LINE
- [SDR FDEA202101100032](https://openairdocs.org/sdr/FDEA202101100032), Jan 10, 2021: FLOOR SUPPORT. CRACKED. LOWER BULK CARGO COMPARTMENT STATION 1980, RIGHT BUTT LINE 33 FLOOR STRINGER FOUND WITH CRACK AS MARK. LOWER BULK CARGO COMPARTMENT STATION 1980 RIGHT BUTT LINE
- [SDR FDEA202101100031](https://openairdocs.org/sdr/FDEA202101100031), Jan 10, 2021: FLOOR SUPPORT. CRACKED. LOWER BULK CARGO COMPARTMENT STATION 1980, RIGHT BUTT LINE 41 FLOOR STRINGER FOUND WITH CRACK AS MARK. LOWER BULK CARGO COMPARTMENT STATION 1980 RIGHT BUTT LINE
- [SDR FDEA201710152964](https://openairdocs.org/sdr/FDEA201710152964), Oct 15, 2017: FRAME. CRACKED. NR 2 ENGINE PYLON HAS AN INTERNAL FRAME CRACKED. CRACK LOCATED INBOARD SIDE NAC STA 325.3, JUST ABOVE AFT ACCESS DOOR FOR AFT ENGINE MOUNT BOLTS. CRACK CONFIRME
- [SDR FDEA201703270995](https://openairdocs.org/sdr/FDEA201703270995), Mar 27, 2017: DUCT. RUPTURED. CARGO FIRE WARNING DURING TAXI, BOTTLES DISCHARGED, STATUS MESSAGE FOR BOTTLE 1B AND BOTTLE 1A. REPLACED A RUPTURED DUCT.
- [SDR FDEA201610063476](https://openairdocs.org/sdr/FDEA201610063476), Oct 6, 2016: SWITCH. OUT OF POSITION. EICAS MESSAGE FOR EMERGENCY LIGHTS. ACFT RETURNED TO BLOCKS. FOUND EMERGENCY SWITCH GUIDE RING OUT OF RANK. REPOSITION AND PERFORMED RTS PASSED IAW MM 33-50-00.
- [SDR FDEA201507112197](https://openairdocs.org/sdr/FDEA201507112197), Jul 11, 2015: LINK. BROKEN. ON ARRIVAL, FOUND LT MAIN GEAR DOOR & MLG DRAG STRUT DOOR DAMAGED DUE TO LINK BROKEN ON MLG DRAG STRUT DOOR. REINSTALLED LT MAIN LANDING GEAR SHOCK STRUT DOOR I
- [SDR FDEA201504171254](https://openairdocs.org/sdr/FDEA201504171254), Apr 17, 2015: EEC. INOPERATIVE. DURING CRUISE THE LT ENGINE FLAMED OUT, WOULD NOT RESTART. LEFT FUEL CONTROL VALVE ILUMINATED SHUTTING DOWN LEFT ENGINE. INFLIGHT START CHECKLIST ACCOMPLISHED L
- [SDR FDEA201406081361](https://openairdocs.org/sdr/FDEA201406081361), Jun 8, 2014: TIRE. LEAKING. ABOUT 90 MINUTES INTO THE FLIGHT, RECEIVED AN EICAS, TIRE PRESSURE NR 10. TIRE SHOWED AMBER AT 184 PSI. NR 10 TIRE PRESSURE CONTINUED TO SLOWLY DECREASE DURING 
- [SDR FDEA201307101519](https://openairdocs.org/sdr/FDEA201307101519), Jul 10, 2013: LAMP. INOPERATIVE. EXTERNAL EMERGENCY LIGHT INOPERATIVE. REPLACED LAMP. OPS CHECK GOOD IAW MM 33-51-00-5.
- [SDR FDEA201303300690](https://openairdocs.org/sdr/FDEA201303300690), Mar 30, 2013: SKIN. DAMAGED. RIGHT NOSE SKIN BEHIND F/O WINDOW FOUND 2 LIGHTNING STRIKES DAMAGED AT BS 246 AND 228. REPAIRED IAW EA G 5330-161299A PART 3.
- [SDR FDEA201205151811](https://openairdocs.org/sdr/FDEA201205151811), May 15, 2012: HANDLE. OUT OF ADJUST. L1 DOOR WAS HARD TO MOVE SLIDE HANDLE FROM DISARM TO ARMED POSITION ON BLOCKOUT. PERFORMED ADJUSTMENT AND TEST IAW MM 52-11-00-5. OPS CHECKED NORMAL. OK FOR SER
- [SDR FDEA201203070865](https://openairdocs.org/sdr/FDEA201203070865), Mar 7, 2012: SKIN. DELAMINATED. LEFT WING FLAP DELAMINATED T/E BETWEEN NR 1 AND NR 2 CANOE APPROX 10" X 10" AREA . REMOVED LT OTBD T/E FLAP REF MM 27-51-21-4. T/E FLAP SYS MAINT PRACTICES COMP
- [SDR FDEA201202150580](https://openairdocs.org/sdr/FDEA201202150580), Feb 15, 2012: BRACKET. LOOSE. L1 DOOR SLIDE CONTAINER LOWER BRACKET LOOSE. AFFIXED COMESTIC TRIM PIECE TO L1 DOOR BUSTLE IAW MM 25-66-06 AND SMP CH 20.
- [SDR FDEA201107082614](https://openairdocs.org/sdr/FDEA201107082614), Jul 8, 2011: AUTOTHROTTLE SYS. MALFUNCTIONED. ON TAXI OUT, HAD AN UNCOMMANDED AUTO THROTTLE ENGAGEMENT TO TAKEOFF POWER. THROTTLES HAS JUST BEEN MOVED TO IDLE FROM ABOUT 30 PERCENT, AT WHICH TIME THE ATS EN

## Related

- Other Boeing 777-FS2 aircraft: https://openairdocs.org/model/boeing-777-fs2/aircraft.md
- STCs for the Boeing 777-FS2: https://openairdocs.org/model/boeing-777-fs2/stcs.md
- The GE GE90-110B1 engine: https://openairdocs.org/engine/ge-ge90-110b1.md

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From OpenAirDocs.org, an independent open copy of FAA and NTSB data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.