# N853FD: 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: 37724
- Year built: 2009
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: November 24, 2009
- Certificate issued: November 24, 2009
- Expires: November 30, 2028
- Mode S code: ABB2FE
- 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=853FD
- Page: https://openairdocs.org/aircraft/N853FD

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 (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB OPS26LA027](https://openairdocs.org/ntsb/OPS26LA027), Mar 18, 2026: Boeing 777-FS2 (N853FD), Newark, NJ, incident, no damage, investigation ongoing

## FAA accident and incident reports

None matched to N853FD.

## Service difficulty reports (31)

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 FDEA202508201514](https://openairdocs.org/sdr/FDEA202508201514), Aug 20, 2025: SKIN. CRACKED. UT&OPEN HOLE HFEC INSPECTION ON THE RIGHT WING UPPER WING SKIN COMMON TO FASTENERS 0-6 AND FOUND 02EA CRACK ON THE HOLE #5. RIGHT WING UPPER WING SKIN #5 HOLE C
- [SDR FDEA202508171484](https://openairdocs.org/sdr/FDEA202508171484), Aug 17, 2025: SKIN. DENTED. LEFT OTBD FLAP LWR SURFACE FROM IB TO OB 40 INCHES CORSS TE TO LE 12 INCHES FOUND ONE DENT. REPAIRED LH OB FLAP LWR SURFACE DENT AT OTEF STA 73 AS PER B777 SRM 
- [SDR FDEA202508171483](https://openairdocs.org/sdr/FDEA202508171483), Aug 17, 2025: SKIN. DENTED. LEFT OTBD FLAP LWR SURFACE FROM OB TO IB 93 INCHES CORSS TE TO LE 4 INCHES FOUND ONE DENT. REPAIRED LH OB FLAP LWR SURFACE DENT AT OTEF STA 434 AS PER B777 SRM 
- [SDR FDEA202508171482](https://openairdocs.org/sdr/FDEA202508171482), Aug 17, 2025: SKIN. DENTED. FOUND RHW T/E O/B FLAP LOWER SURFACE 01 EA DENT AT THE CROSS OTEF 428 AND T/E 4 INCHES. REPAIRED RHW T/E O/B FLAP LOWER SURFACE 01 EA DENT AT OTEF STA 428 AS PE
- [SDR FDEA202508171481](https://openairdocs.org/sdr/FDEA202508171481), Aug 17, 2025: SKIN. DENTED. FOUND RHW T/E O/B FLAP LOWER SURFACE 01EA DENT AT THE CROSS OTEF 127 AND T/E 01 INCHES. REPAIRED RHW T/E O/B FLAP LOWER SURFACE 01EA DENT AT OTEF STA 127 AS PER
- [SDR FDEA202508171480](https://openairdocs.org/sdr/FDEA202508171480), Aug 17, 2025: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8302-33 FOUND CRACKED AT STA 1010 LBL 85 - LBL 113. MAIN DECK CARGO FLOOR PANEL P/N:152W8302-33 CRACKED AT STA 1010 LBL 85 
- [SDR FDEA202508171479](https://openairdocs.org/sdr/FDEA202508171479), Aug 17, 2025: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8302-34 FOUND CRACKED AT STA 1010 RBL 85. MAIN DECK CARGO FLOOR PANEL P/N:152W8302-34 CRACKED AT STA 1010 RBL 85. DAMAGE SI
- [SDR FDEA202508161478](https://openairdocs.org/sdr/FDEA202508161478), Aug 16, 2025: SKIN. CRACKED. UT & OPEN HOLE HFEC INSPECTION ON THE LEFT WING UPPER WING SKIN COMMON TO FASTENERS 0-6 AND FOUND 01EA CRACK ON THE HOLE #5. THE LEFT WING UPPER SKIN #5 FASTENE
- [SDR FDEA202508151453](https://openairdocs.org/sdr/FDEA202508151453), Aug 15, 2025: SKIN. WORN. #7 SLAT OUTER SKIN TRAILING EDGE FASTENER HOLE AT ISS 184 FOUND WORN. LH WING #7 SLAT OUTER SKIN TRAILING EDGE AT ISS 184 WORN FASTENER HOLE REPAIRED AS PER B77
- [SDR FDEA202505200769](https://openairdocs.org/sdr/FDEA202505200769), May 20, 2025: POWER SUPPLY. NO TEST. EMERGENCY LIGHTS OF SUPERNUMERARY LEFT AREA SIDE DID NOT WORK WHEN EMER LIGHT ON MODE. AMM: 33-51-06-2 REMOVED AND REPLACED LEFT DOOR EMER PWR SUPPLY (M33093) (
- [SDR FDEA202203070436](https://openairdocs.org/sdr/FDEA202203070436), Mar 7, 2022: NONE. NONE. 1859Z AT FL 290 ENCOUNTERED SEVERE TURBULENCE. TWO OVER SPEEDS WERE NOTED DURING THE EVENT OVER SPEED WAS APPROXIMATELY 40 KNOTS . OVERALL AIRSPEED LOSS AND GAI
- [SDR FDEA2020062571140](https://openairdocs.org/sdr/FDEA2020062571140), Jun 7, 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 HAND UNDERWING
- [SDR FDEA2020062571139](https://openairdocs.org/sdr/FDEA2020062571139), Jun 7, 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 FDEA2020060871140](https://openairdocs.org/sdr/FDEA2020060871140), Jun 7, 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 HAND UNDERWING
- [SDR FDEA2020060871139](https://openairdocs.org/sdr/FDEA2020060871139), Jun 7, 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 FDEA2020062641124](https://openairdocs.org/sdr/FDEA2020062641124), Jun 4, 2020: SPAR. CRACKED. DURING ULTRASONIC INSPECTION ON THE VERTICAL FLANGE OF THE SPAR CHORD AND HIGH FREQUENCY EDDY CURRENT OPEN HOLE INSPECTION CARRIED OUT ON REMOVED FASTENER HOLES
- [SDR FDEA2020060541124](https://openairdocs.org/sdr/FDEA2020060541124), Jun 4, 2020: LONGERON. CRACKED. HIGH FREQUENCY EDDY CURRENT, OPEN HOLE INSPECTION CARRIED OUT ON. REMOVED FASTENER HOLES AT RIGHT HAND SIDE UNDERWING LONGERON LOWER WING BASE STATION 1035. VER
- [SDR FDEA202005291077](https://openairdocs.org/sdr/FDEA202005291077), May 29, 2020: LONGERON. CRACKED. ULTRASONIC INSPECTION OF THE RIGHT HAND UNDERWING LONGERON FOUND CRACK AT BASE STATION 1035. COMPLIANCE WITH E.O. # G-5310-E0332629 E P6. TITEL: FUSELAGE Ï¿½ MA
- [SDR FDEA202005291076](https://openairdocs.org/sdr/FDEA202005291076), May 29, 2020: LONGERON. CRACKED. ULTRASONIC INSPECTION OF THE LEFT HAND UNDERWING LONGERON FOUND CRACKED AT BS 1035. COMPLIANCE WITH E.O. # G-5310-E0332629 E P5. TITEL: FUSELAGE Ï¿½ MAINFRAME Ï
- [SDR FDEA201807191787](https://openairdocs.org/sdr/FDEA201807191787), Jul 19, 2018: LIGHT. INOPERATIVE. SUPERNUMERARY EMERGENCY LIGHT TEST PERFORMED. CEILING LIGHT CLOSEST TO GALLEY INOP. RELAMPED SUPERNUMERARY EMERGENCY AREA LIGHT AS PER AMM 33-51-03-2 AND TEST O
- [SDR FDEA201807101665](https://openairdocs.org/sdr/FDEA201807101665), Jul 10, 2018: CHARGER. INOPERATIVE. DURING CABIN PREFLIGHT, FOUND THAT EMERGENCY LIGHTS ON LEFT SIDE OF CABIN WOULD NOT ILLUMINATE DURING EMERGENCY LIGHT TEST. P/N INSTALLED/REMOVED MPN D717-02-00
- [SDR FDEA201705031347](https://openairdocs.org/sdr/FDEA201705031347), May 3, 2017: HANDLE. OUT OF POSITION. UNABLE TO ARM L1 OUTER DOOR HANDLE, NOT IN STOW POSITION. POSITIONED HANDLE IAW AMM 52-11-00-2.
- [SDR FDEA201511213750](https://openairdocs.org/sdr/FDEA201511213750), Nov 21, 2015: CONTAINER. SMOKE. DURING CRUISE AT FL 310 RECEIVED FIRE CARGO AFT WARNING. RAN CHECKLIST, DISCHARGED FIRE BOTTLES. FIRE WARNING CONTINUED TO DISPLAY FOR OVER 30 MINUTES. FIRE WAR
- [SDR FDEA201506031682](https://openairdocs.org/sdr/FDEA201506031682), Jun 3, 2015: ARMING LEVER. UNKNOWN. LEFT MAIN CABIN ENTRY DOOR ARMING LEVER MOVED TO THE, GREEN BAND, DISARMED POSITION ON LANDING. PERFORMED MODE SELECT MECHANISM TEST ND CHECK IAW AMM 52-11-15-2
- [SDR FDEA201505191536](https://openairdocs.org/sdr/FDEA201505191536), May 19, 2015: LIGHT. INOPERATIVE. EMERGENCY LIGHT OVER THE LT ENTRY DOOR IS OUT. R & R EMER LIGHT LAMP IAW MM 33-50-00-2. OPERATIONS CHECKED NORMAL. OK TO CONTINUE.
- [SDR FDEA201504201266](https://openairdocs.org/sdr/FDEA201504201266), Apr 20, 2015: LENS. MISSING. FOUND EPAS PRESS GAUGE VIEWPORT LENS ON LT ENTRY DOOR MISSING. REPLACED LENS. IAW S.M.P.
- [SDR FDEA201412174136](https://openairdocs.org/sdr/FDEA201412174136), Dec 17, 2014: BLADE. DAMAGED. RIGHT ENG VIBRATION DURING CLIMB PASSING 1000` AGL. ENG SECONDARY VIBRATION MONITOR DISPLAYED 5.0 N1 ON RT ENG. VIBRATION FELT IN YOKE, RUDDER PEDALS & FLOOR. N
- [SDR FDEA201304080745](https://openairdocs.org/sdr/FDEA201304080745), Apr 8, 2013: SPRING. FOULED. SPRING ON THE EMERGENCY LIGHTS APPEARS TO BE FOULED UP. ADJUSTED SPRING IAW SMP FUNCTIONED GOOD.
- [SDR FDEA201207062508](https://openairdocs.org/sdr/FDEA201207062508), Jul 6, 2012: LAMP. INOPERATIVE. LEFT SIDE EXTERIOR EMERENCY LIGHT INOPERATIVE. RELAMPED LT EMERGENCY LIGHT AND OPS CHECK NORMAL IAW AMM 33-51-04-2.
- [SDR FDEA201201030008](https://openairdocs.org/sdr/FDEA201201030008), Jan 3, 2012: SKIN. DAMAGED. FOUND LEFT PASSENGER ENTRY DOOR FWD LOWER SKIN NICK DAMAGED, 25/32" X 14/32" X 19/32". REPAIRED IAW EA G-5210-157508 PT1 AND PT2.
- [SDR FDEA201108063125](https://openairdocs.org/sdr/FDEA201108063125), Aug 6, 2011: SPRING. INOPERATIVE. EMERGENCY LIGHT SWITCH ARM/DISARM SPRING INOP. REINSTALLED SPRING. SWITCH GUARD OPERATES NORMALLY.

## 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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