# N856FD: 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: 37727
- Year built: 2010
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 2, 2010
- Certificate issued: August 4, 2010
- Expires: February 29, 2028
- Mode S code: ABBE23
- 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=856FD
- Page: https://openairdocs.org/aircraft/N856FD

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 N856FD.

## FAA accident and incident reports

None matched to N856FD.

## Service difficulty reports (36)

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 FDEA202602090152](https://openairdocs.org/sdr/FDEA202602090152), Feb 9, 2026: SKIN. CRACKED. DURING WORK CARD: EG-5710-E0376285F P12 STEP3.B(1) & 5.A.(2), FOUND TWO CRACKS ON RT UPPER WING SKIN FASTENER NR 5. RIGHT WING UPPER SKIN NR 5 FASTENER HOLE REP
- [SDR FDEA202602090151](https://openairdocs.org/sdr/FDEA202602090151), Feb 9, 2026: SKIN. CRACKED. DURING WORK CARD: EG-5710-E0376285F P12 STEP4.B(2).(B), THEN FOUND ONE CRACK ON RT UPPER WING SKIN FASTENER #6 AS MARKED. RIGHT WING UPPER SKIN NR 6 FASTENER HO
- [SDR FDEA202602090150](https://openairdocs.org/sdr/FDEA202602090150), Feb 9, 2026: SKIN. CRACKED. DURING WORK CARD: EG-5710-E0376285F P11 STEP4.B(2).(B), THEN FOUND ONE CRACK ON LT UPPER WING SKIN FASTENER NR 6. THE LEFT WING UPPER SKIN #6 FASTENER HOLE CRAC
- [SDR FDEA202602090149](https://openairdocs.org/sdr/FDEA202602090149), Feb 9, 2026: SKIN. CRACKED. DURING WORK CARD: EG-5710-E0376285F P11 STEP3.B.(1) & 5.A.(2) THE FOUND TWO CRACKS ON LT UPPER WING SKIN FASTENER NR 5. THE LEFT WING UPPER SKIN NR 5 FASTENER H
- [SDR FDEA202401150077](https://openairdocs.org/sdr/FDEA202401150077), Jan 15, 2024: UNKNOWN. UNKNOWN. AIRBORNE RETURN DUE TO AIR CONTAMINATION OF AN UNKNOWN SUBSTANCE. NOTED SOOT ON BOTH SIDES OF FLIGHTR COMPARTMENT CAPTAIN AND FO SEATS ON FLAT AREAS NEAR TILLER
- [SDR FDEA202311231886](https://openairdocs.org/sdr/FDEA202311231886), Nov 23, 2023: LAMP. FAILED. RIGHT SLIDE/OVERWING LIGHT IS BURNED OUT AMM: 33_51_04_2 IPC: 33-51-11-01 ITEM 30 REMOVED AND REPLACED RIGHT SLIDE/OVERWING LIGHT REF AMM AMD IPC ABOVE WITH PN 
- [SDR FDEA202306091011](https://openairdocs.org/sdr/FDEA202306091011), Jun 9, 2023: FLOOR PANEL. DAMAGED. MAIN DECK CARGO FLOOR PANEL P/N:152W8402-7 FOUND PUNCTURED AT STA1224 LBL29. EVALUATED MAIN DECK CARGO FLOOR PANEL P/N:152W8402-7 PUNCTURED AT STA1224 LBL29 DAM
- [SDR FDEA202306070999](https://openairdocs.org/sdr/FDEA202306070999), Jun 7, 2023: FLAP. DENTED. LH OB FLAP LWR SURFACE FROM IB TO OB 110INCH CROSS TE TO LE 6.2INCH FOUND ONE DENT. EVALUATED LH OB FLAP LWR SURFACE FROM IB TO OB 110INCH CROSS TE TO LE 6.2INC
- [SDR FDEA202211232829](https://openairdocs.org/sdr/FDEA202211232829), Nov 23, 2022: LAMP. INOPERATIVE. PRE-FLT MX INSP, GALLEY CTR OVRHD (1) EMERGENCY LT INOP. RE-LAMPED, REF B777 AMM: 33-51-04-2. LT TESTS SATIS, ITEM OK FOR SVC.
- [SDR FDEA202102160383](https://openairdocs.org/sdr/FDEA202102160383), Feb 16, 2021: AILERON SYS. MALFUNCTIONED. WITH AUTOPILOT OFF @ 500' ON FINAL, AIELRON CONTROL WAS LIMITED, CHECKED THAT AUTOPILOT WAS OFF AND CONFIRMED AIELRON CONTROL WAS VERY LIMITED, PITCH CONTROL WA
- [SDR FDEA202102160377](https://openairdocs.org/sdr/FDEA202102160377), Feb 16, 2021: AUTOPILOT SYS. MALFUNCTIONED. PDIS 856 27-02 1015 16FEB21 MEM LOGPAGES:2781587 WITH AUTOPILOT OFF @ 500' ON FINAL, AIELRON CONTROL WAS LIMITED, CHECKED THAT AUTOPILOT WAS OFF AND CONFIRMED A
- [SDR FDEA202011252965](https://openairdocs.org/sdr/FDEA202011252965), Nov 25, 2020: LAMP. INOPERATIVE. POST-FLT INSPECTION, R-1 DOOR EXTERIOR EMERGENCY LIGHT INOPERABLE. RE-LAMPED, REF B777 AMM 33-51-04-2. LIGHT TESTS SATISFACTORY, ITEM OK FOR SERVICE.
- [SDR FDEA202010222596](https://openairdocs.org/sdr/FDEA202010222596), Oct 22, 2020: STRUCTURE. DAMAGED. WHILE PERFORMING RIGHT HAND WING CENTER FRONT SPAR LOWER CHORD REPAIR (SPECIAL/NONROUTINE MAINTENANCE FORM NR N00613) FOUND 01 EACH EXISTING OVERSIZED HOLE AT L
- [SDR FDEA202010222593](https://openairdocs.org/sdr/FDEA202010222593), Oct 22, 2020: SPAR. DAMAGED. WHILE PERFORMING RIGHT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (SPECIAL/NONROUTINE MAINTENANCE FORM NR N00613 ) FOUND 01 EACH EXISTING OVERSIZED 
- [SDR FDEA202010222598](https://openairdocs.org/sdr/FDEA202010222598), Oct 22, 2020: SPAR. DAMAGED. WHILE PERFORMING LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (SPECIAL/NONROUTINE MAINTENANCE FORM N00612) FOUND 01 EACH EXISTING OVERSIZED HOLE 
- [SDR FDEA202010222597](https://openairdocs.org/sdr/FDEA202010222597), Oct 22, 2020: WEB. DAMAGED. WHILE PERFORMING LEFT HAND WING CENTER SECTION FRONT SPAR LOWER CHORD REPAIR (SPECIAL/NONROUTINE MAINTENANCE FORM N00612) FOUND 01 EACH EXISTING OVERSIZED HOLE 
- [SDR FDEA202010112460](https://openairdocs.org/sdr/FDEA202010112460), Oct 11, 2020: DOUBLER. DAMAGED. WHILE ACCOMPLISHING RIGHT HAND EO G-5310-E0332629 H P6 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35R NEAR MILLED EDGE. COMPLIED WI
- [SDR FDEA202010042405](https://openairdocs.org/sdr/FDEA202010042405), Oct 4, 2020: DOUBLER. OUT OF ALIGNMENT. WHILE ACCOMPLISHING EO G-5310-E0332629 H P6 FOUND 03 EACH PILOT HOLES AT NEW FUSELAGE SKIN DOUBLER MISALIGNED WITH THE LONGERON FITTING, BETWEEN BODY STATION 99
- [SDR FDEA202010032402](https://openairdocs.org/sdr/FDEA202010032402), Oct 3, 2020: DOUBLER. OUT OF ALIGNMENT. WHILE ACCOMPLISHING EO G-5310-E0332629 H P6 FOUND NEW FUSELAGE SKIN DOUBLER PART NUMBER 143W2314Y406 PILOT HOLES MISALIGN WITH EXISTING FUSELAGE SKIN HOLES, BET
- [SDR FDEA202010032401](https://openairdocs.org/sdr/FDEA202010032401), Oct 3, 2020: DOUBLER. OUT OF ALIGNMENT. WHILE ACCOMPLISHING E.O. #G-5310-E0332629 H P6 FOUND NEW FUSELAGE SKIN DOUBLER PART NUMBER 143W2314Y406 PILOT HOLES MISALIGN WITH EXISTING FUSELAGE SKIN HOLES B
- [SDR FDEA202010012368](https://openairdocs.org/sdr/FDEA202010012368), Oct 1, 2020: DOUBLER. DAMAGED. WHILE ACCOMPLISHING LEFT HAND EO NR G-5310-E0332629 H P5 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35L NEAR MILLED EDGE. COMPLIED 
- [SDR FDEA202009302358](https://openairdocs.org/sdr/FDEA202009302358), Sep 30, 2020: SKIN. CRACKED. HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON THE EXTERNAL SURFACE OF THE FUSELAGE SKIN WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHT HAND SID
- [SDR FDEA202009292351](https://openairdocs.org/sdr/FDEA202009292351), Sep 29, 2020: FLANGE. CRACKED. DURING ULTRASONIC INSPECTION AND HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES ON RIGHT HAND SIDE VERTICAL FLANGE OF TH
- [SDR FDEA202009292350](https://openairdocs.org/sdr/FDEA202009292350), Sep 29, 2020: FLANGE. CRACKED. DURING ULTRASONIC INSPECTION AND HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES ON LEFT HAND SIDE VERTICAL FLANGE OF THE
- [SDR FDEA202009282344](https://openairdocs.org/sdr/FDEA202009282344), Sep 28, 2020: FLOOR SUPPORT. CRACKED. LOWER BULK CARGO COMPARTMENT STATION 1980.5 RIGHT BUTT LINE 33.2 FLOOR PANEL STRINGER FOUND CRACKED, AS MARKED. LOWER BULK CARGO COMPARTMENT STATION 1980.5 RIGH
- [SDR FDEA202009282343](https://openairdocs.org/sdr/FDEA202009282343), Sep 28, 2020: FLOOR SUPPORT. CRACKED. LOWER BULK CARGO COMPARTMENT STATION 1962.5 LEFT BUTT LINE 24.9 FLOOR PANEL STRINGER FOUND CRACKED. LOWER BULK CARGO COMPARTMENT STATION 1962.5 LEFT BUTT LINE 2
- [SDR FDEA202009242311](https://openairdocs.org/sdr/FDEA202009242311), Sep 24, 2020: FLOOR SUPPORT. CRACKED. LOWER BULK CARGO COMPARTMENT STATION 1937 RIGHT BUTT LINE 41.5 FLOOR PANEL STRINGER FOUND CRACK, AS MARKED. LOWER BULK CARGO COMPARTMENT STATION 1937 RIGHT BUTT
- [SDR FDEA2019121753248](https://openairdocs.org/sdr/FDEA2019121753248), Dec 15, 2019: LINE. LEAKING. PDIS 856 29-02 9464 15DEC19 LGG FACT U LOGPAGES:3029639 HYD QTY LOW C EICAS MESSAGE FOLLOWED BY RESERVE BRAKES / STRG MESSAGE. ISLN VALVES CLOSED AT .40 LEAK ST
- [SDR FDEA201910312793](https://openairdocs.org/sdr/FDEA201910312793), Oct 31, 2019: SLIDE RAFT. JAMMED. PDIS 856 52-10 9353 31OCT19 LAX OPEN U LOGPAGES:2986641 F/O STATES L1 DOOR IS VERY DIFFICULT TO ARM. HAD TO SELECT IT TO ARM MORE THAN ONCE FOR THE DEPARTURE. R
- [SDR FDEA201903030531](https://openairdocs.org/sdr/FDEA201903030531), Mar 3, 2019: WARNING SYSTEM. ACTIVATED. PDIS 856 36-11 8701 03MAR19 CDG FACT U LOGPAGES:3019358 BLEED OFF ENG R ILLUMINATED AFTER TAKE OFF. FACT 03MAR19 03:04 CDG U PLEASE REF. WRI# 36-11/8702, BLEED 
- [SDR FDEA20180829405](https://openairdocs.org/sdr/FDEA20180829405), Feb 15, 2018: CYLINDER. EMPTY. ON ARRIVAL, FOUND THE L1 DOOR EMERGENCY POWER ASSIST SYSTEM RESERVOIR EMPTY.
- [SDR FDEA201710092885](https://openairdocs.org/sdr/FDEA201710092885), Oct 9, 2017: LINE. CHAFED. HYD QTY LOW C IN FLIGHT. TROUBLESHOT AND FOUND HYD FLUID LEAKING FROM RT MLG STEERING PCU PRESSURE HOSE. FOUND A HOLE ON IT DUE TO CHAFING WITH ITS GUIDE. R & R
- [SDR FDEA201707111914](https://openairdocs.org/sdr/FDEA201707111914), Jul 11, 2017: LIGHT. NO TEST. DURING A POST FLIGHT CHECK, THE R1 DOOR AFT EMERGENCY EXIT LIGHT HAS OVER 50% NOT ILLUMINATED DURING TEST. REMOVED AND REPLACED THE EMERGENCY LIGHT ASSY, IAW AM
- [SDR FDEA201502270610](https://openairdocs.org/sdr/FDEA201502270610), Feb 27, 2015: MECHANISM. LACK OF LUBE. DOOR 1L ARMING HANDLE HANDLING UP WHEN ARMING. TAKES MULTIPLE ATTEMPTS TO MOVE HANDLE. LUBRICATED 1L DOOR MECHANISM & OPERATED IAW AMM 52-11-00-021. DOOR HANDLE
- [SDR FDEA201109083774](https://openairdocs.org/sdr/FDEA201109083774), Sep 8, 2011: BATTERY PACK. INOPERATIVE. FOUND L1 DOOR EPAS GREEN TEST LIGHT WOULD NOT COME ON. R & R L1 DOOR EPAS POWER PACK 9V BACKUP BATTERIES IAW MM 52-11-20-4-2 AND CKS OK IAW MM 52-11-20-5-2. OK 
- [SDR FDEA201008183033](https://openairdocs.org/sdr/FDEA201008183033), Aug 18, 2010: BULB. FAILED. EMERGENCY LIGHT AT THE R1 DOOR INOP. R & R R1 EMERGENCY DOOR LIGHT IAW 33-51-04-2. OPS CHECK GOOD, 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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