# N851FD: 2009 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: 37722
- Year built: 2009
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 10, 2009
- Certificate issued: December 11, 2009
- Expires: February 28, 2029
- Mode S code: ABAB90
- 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=851FD
- Page: https://openairdocs.org/aircraft/N851FD

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 N851FD.

## FAA accident and incident reports

None matched to N851FD.

## Service difficulty reports (37)

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 FDEA202606040671](https://openairdocs.org/sdr/FDEA202606040671), Jun 4, 2026: LAMP. INOPERATIVE. POST-FLT INSP, L1 OVERHEAD EMERGENCY LT INOP. AMM: 33-51-04-2 RE-LAMPED, REF B777 AMM: 33-51-04-2. LT TESTS SATIS, ITEM OK FOR SVC.
- [SDR FDEA202512042219](https://openairdocs.org/sdr/FDEA202512042219), Dec 4, 2025: LAMP. INOPERATIVE. EMERGENCY LIGHT OVERHEAD DOOR 1L INOPERATIVE. REPLACED THE LAMP OF EMERGENCY AREA LIGHT OVERHEAD DOOR 1L REF AMM 33-51-03-2 , TEST NORMAL. A/C OK TO CONTINUE.
- [SDR FDEA202507121185](https://openairdocs.org/sdr/FDEA202507121185), Jul 12, 2025: FLOOR PANEL. CRACKED. REWORK: MAIN DECK CARGO FLOOR PANEL P/N:152W8302-33 FOUND CRACKED AT STA1010 LBL85. MAIN DECK CARGO FLOOR PANEL P/N:152W8302-33 CRACKED AT STA1010 LBL85 DAMAGE 
- [SDR FDEA202507111177](https://openairdocs.org/sdr/FDEA202507111177), Jul 11, 2025: FLOOR SUPPORT. CORRODED. MAIN DECK CARGO FLOOR FITTING FOUND CORROSION AT STA1434 RBL40. MAIN DECK CARGO FLOOR FITTING CORROSION AT STA1434 RBL40 REMOVED AND EVALUATED: THE REWORKED ARE
- [SDR FDEA202507101167](https://openairdocs.org/sdr/FDEA202507101167), Jul 10, 2025: FITTING. CORRODED. MAIN DECK CARGO FLOOR FITTING FOUND CORROSION AT STA 1393 LBL6.5 MAIN DECK CARGO FLOOR FITTING CORROSION AT STA 1393 LBL6.5 REMOVED AND EVALUATED : THE REWORKED
- [SDR FDEA202507101166](https://openairdocs.org/sdr/FDEA202507101166), Jul 10, 2025: FITTING. CORRODED. MAIN DECK CARGO FLOOR FITING FOUND CORROSION AT STA1393 RBL6.5. MAIN DECK CARGO FLOOR FITTING CORROSION AT STA 1393 RBL6.5 REMOVED AND EVALUATED : THE REWORKED 
- [SDR FDEA202507061125](https://openairdocs.org/sdr/FDEA202507061125), Jul 6, 2025: SKIN. DELAMINATED. LH WING OB FLAP LWR SURFACE FROM IB TO OB 20 INCH CROSS TE TO LE 5 INCH FOUND DELAMINATION.
- [SDR FDEA202507041114](https://openairdocs.org/sdr/FDEA202507041114), Jul 4, 2025: SKIN. CRACKED. MFEC INSPECTION OF THE OUTBOARD SLAT NO.10 OUTER SKIN DETECTED 1EA FASTENER WITH TWO CRACKS, APPROXIMATELY 4MM AND 6MM IN LENGTH RESPECTIVELY. RH WING NO.10 SLA
- [SDR FDEA202507041113](https://openairdocs.org/sdr/FDEA202507041113), Jul 4, 2025: SKIN. BULGED. RH WING NO.11 SLAT OUTER SKIN FOUND BULGE AT 28-33 INCH TO OB EDGE. RH WING NO.11 SLAT OUTER SKIN BULGE AREA REPAIRED AS PER B777 SRM 57-43-01-2R REPAIR 9 FIG 2
- [SDR FDEA202507031101](https://openairdocs.org/sdr/FDEA202507031101), Jul 3, 2025: SKIN. CRACKED. DURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF THE LEFT UPPER WING SKIN COMMON TO FASTENERS 0-5 AND FOUND 02EA CRCAK AT HOLE #5. LEFT WING UPPER SKIN #5 HOLE 
- [SDR FDEA202507031100](https://openairdocs.org/sdr/FDEA202507031100), Jul 3, 2025: SKIN. CRACKED. DURING PERFORM UT & OPEN HOLE HFEC INSPECTION OF THE RIGHT UPPER WING SKIN COMMON TO FASTENERS 0-5 AND FOUND 02EA CRCAK AT HOLE #5. RIGHT WING UPPER SKIN #5 HOL
- [SDR FDEA202507021098](https://openairdocs.org/sdr/FDEA202507021098), Jul 2, 2025: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N:152W8302-33 CRACKED AT STA1010 LBL85 DAMAGE SIZE:L=3.5" DAMAGE OUT OF ALLOWABLE LIMIT AS PER B777 SRM 53-00-50-1A ALLOWABLE DAMA
- [SDR FDEA202410011412](https://openairdocs.org/sdr/FDEA202410011412), Oct 1, 2024: ENGINE. DAMAGED. STARTING CLIMB FROM FL380 TO FL400. WHEN THRUST STARTED TO INCREASE, FELT A MAJOR JOLT FOLLOWED BY MAJOR VIBRATIONS, SMOKE & FUMES IN COCKPIT. LT GEN DRIVE & L 
- [SDR FDEA202302080230](https://openairdocs.org/sdr/FDEA202302080230), Feb 8, 2023: FLAP. DENTED. LH OB FLAP LWR SURFACE FROM OB TO IB 98 INCH CROSS TE TO LE 8 INCH FOUND ONE DENT LH O/B FLAP LWR SURACE FROM O/B TO I/B 98 INCH CROSS T/E TO L/E 8 INCH DENT DA
- [SDR FDEA202302080229](https://openairdocs.org/sdr/FDEA202302080229), Feb 8, 2023: FLAP. DAMAGED. RH WING OB FLAP LEADING EDGE FOUND BROKEN AT OTEF STA 437. RH WING OB FLAP LEADING EDGE PUNCTURE DAMAGE SIZE L X W: 1.0" X 0.5", OUT OF ALLOWABLE LIMIT PER B777
- [SDR FDEA202201210752](https://openairdocs.org/sdr/FDEA202201210752), Jan 21, 2022: POWER SUPPLY. NO TEST. EMERGENCY LIGHT TEST IN SUPERNUMERARY COMPARTMENT DID NOT TEST PROPERLY. L1 DOOR LIGHTS DID NOT ILLUMINATE. REPLACED L1 DOOR POWER SUPPLY IAW AMM 31-51-06-2, EM
- [SDR FDEA2020052230881](https://openairdocs.org/sdr/FDEA2020052230881), May 3, 2020: SKIN. CRACKED. DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHT HAN HAND UNDER
- [SDR FDEA2020050430881](https://openairdocs.org/sdr/FDEA2020050430881), May 3, 2020: SKIN. CRACKED. DURING HIGH FREQUENCY EDDY CURRENT CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE RIGHR HAND UNDERWING LONGERON A
- [SDR FDEA2020050430880](https://openairdocs.org/sdr/FDEA2020050430880), May 3, 2020: SKIN. CRACKED. DURING HIGH FREQUENCY EDDY CURRENT INSPECTION CARRIED OUT ON EXTERNAL SURFACE OF FUSELAGE WITHIN A 2 INCH RADIUS OF ALL HOLES COMMON TO THE LEFT HAND UNDERWING 
- [SDR FDEA202004300852](https://openairdocs.org/sdr/FDEA202004300852), Apr 30, 2020: STRUCTURE. CRACKED. DURING ACCOMPLISHMENT OF HIGH FFEQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON LEFT FRONT LOWER CHORD 04 EACH FASTENER HOLES AT STATION 1035 LEFT BUTT LINE 82 AND
- [SDR FDEA202004300851](https://openairdocs.org/sdr/FDEA202004300851), Apr 30, 2020: SPAR. CRACKED. DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION ON RIGHT HAND FRONT LOWER SPAR CHORD 04 EACH FASTENER HOLES AT STATION 1035 RIGHT BUTT
- [SDR FDEA202004270801](https://openairdocs.org/sdr/FDEA202004270801), Apr 27, 2020: LONGERON. CRACKED. ULTRASONIC INSPECTION CARRIED OUT AND FOUND THE LEFT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 WITH CRACK INDICATION.
- [SDR FDEA202004270800](https://openairdocs.org/sdr/FDEA202004270800), Apr 27, 2020: LONGERON. CRACKED. ULTRASONIC INSPECTION CARRIED OUT AND FOUND THE RIGHT HAND SIDE UNDERWING LONGERON AT BODY STATION 1035 WITH CRACK INDICATION.
- [SDR FDEA2019122313285](https://openairdocs.org/sdr/FDEA2019122313285), Dec 21, 2019: TIRE. WORN. RECEIVED EICAS MESSAGE OF TIRE PRESS. PRESSURE ON NR 7 INDICATED 180 PSI AND DURING FLIGHT CONTINUED DOWN TO 113 PSI. EMERGENCY WAS DECLARED AND TIRE REMAINED I
- [SDR FDEA201907151576](https://openairdocs.org/sdr/FDEA201907151576), Jul 15, 2019: SLIDE. UNWANTED DEPLOY. MDIS 851 52-10 0202 15JUL19 DEL OPEN U DURING PREFLIGHT CHECK, L1 DOOR SLIDE DEPLOYED. DURING PRE FLIGHT FOUND L1 DOOR HANDLE NOT FULLY STOWED DOWN IN OPEN POSI
- [SDR FDEA201811213348](https://openairdocs.org/sdr/FDEA201811213348), Nov 21, 2018: POWER SUPPLY. INOPERATIVE. TEST FAILS ON SUPRNMRY LIGHT TEST FOUR LIGHTS INOP. REMOVED AND REPLACED R1 OVRHD EMER LIGHTS POWER SUPPLY, REF AMM 33-51-06-2. EMER LIGHTS TEST SATIS, ITEM OK 
- [SDR FDEA201810232983](https://openairdocs.org/sdr/FDEA201810232983), Oct 23, 2018: FLOORBOARD. CRACKED. FOUND UPPER CARGO FLOORBOARD CRACKED AT STA 1000 RIGHT OUTBOARD. REMOVED AND REINSTALLED UPPER CARGE FLOORBOARD AT STA 1000 RIGHT & OUTBOARD REF B777 MM 53-01-0
- [SDR FDEA201707212014](https://openairdocs.org/sdr/FDEA201707212014), Jul 21, 2017: FLOOR SUPPORT. CRACKED. BULK CARGO BAY FLOOR SUPPORT AT BS 1958, FOUND CRACKED. REPAIRED IAW SRM 53-70-53-2R, FIGURE 202, REPAIR 2. REPAIR CLASSIFIED AS MAJOR IAW GMM 6-2-100.
- [SDR FDEA201707191993](https://openairdocs.org/sdr/FDEA201707191993), Jul 19, 2017: SLAT. DAMAGED. LEFT WING NR 1 SLAT ASSY CENTER LEADING EDGE SURFACE FOUND DAMAGED. REPAIRED IAW SRM 57-43-01, REPAIR 2, AND EA G-5750-T0334492, PT 1. REPAIR CLASSIFIED AS MAJO
- [SDR FDEA201703150918](https://openairdocs.org/sdr/FDEA201703150918), Mar 15, 2017: TRANSDUCER. OUT OF ADJUST. YOKE BECAME LOCKED IN POSITION DURING PRE TAKEOFF FLIGHT CONTROL CHECK. ADJUSTED PLATE ON CENTRAL WHEEL FORCE TRANSDUCER IAW MM 27-11-08-4-0. AILERON AND FLAPER
- [SDR FDEA201612154465](https://openairdocs.org/sdr/FDEA201612154465), Dec 15, 2016: LAMP. INOPERATIVE. R1 DOOR EXTERIOR EMERGENCY LIGHT INOP ON POST-FLT CHECK. REPLACED THE LAMP IAW AMM 33-51-04-2. EMERGENCY LIGHT TESTED GOOD, OK FOR SERVICE.
- [SDR FDEA201611224186](https://openairdocs.org/sdr/FDEA201611224186), Nov 22, 2016: LAMP. INOPERATIVE. R1 DOOR EXTERIOR EMERGENCY LIGHT INOPERATIVE. FOUND ON POST FLIGHT OPS CHECK. REPLACED THE LAMP IAW AMM: 33-51-04-2. LIGHTS TESTED GOOD, OK FOR SERVICE.
- [SDR FDEA201501210245](https://openairdocs.org/sdr/FDEA201501210245), Jan 21, 2015: SKIN. DENTED. BULK CARGO DOOR EXTERIOR SKIN FOUND DENTED. REPAIRED IAW SRM 52-30-01 FIGURE 202 REPAIR 13 AND EA G-5230-T0314944 PART 1.
- [SDR FDEA201308011737](https://openairdocs.org/sdr/FDEA201308011737), Aug 1, 2013: DOOR SEAL. LACK OF LUBE. L1 DOOR HARD TO OPEN. LUBRICATED DOOR SEAL. DOOR OPS CHECKED NORMAL AND WITHIN LIMITS IAW MM 52-11-00-5.
- [SDR FDEA201011194423](https://openairdocs.org/sdr/FDEA201011194423), Nov 19, 2010: GUARD. OUT OF RIG. EMERGENCY LIGHT SWITCH GUARD/WIRE ON OVERHEAD PANEL OUT OF RIG. CAP WILL NOT CLOSE PROPERLY WHEN EMERGENCY LIGHTS SWITCH IS IN " ARMED " POSITION. R & R SWITCH 
- [SDR FDEA201011184417](https://openairdocs.org/sdr/FDEA201011184417), Nov 18, 2010: SPRING. LOOSE. WHEN GUARD COVER ON EMERGENCY LIGHTS IS CLOSED IT TURNS THE EMERGENCY LIGHTS TO OFF. FOUND SPRING IN GUARD COVER OF EMERGENCY LIGHT SWITCH LOOSE. ADJUSTED & REI
- [SDR FDEA201004271377](https://openairdocs.org/sdr/FDEA201004271377), Apr 27, 2010: SLIDE. DISLODGED. RT EMERGENCY SLIDE DEPLOYED ON THE GROUND. ANC R RELEASED FOR SERVICE IAW MEL: 52-11-01-02 CATEGORY: C EXPIRATION: 07MAY10 "MEL 52-11-01-02: DOOR (R1 SLIDE/RAFT

## 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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