# N844FD: 2011 Boeing 777FHT

- Status: Valid registration
- Airframe: [Boeing 777FHT](https://openairdocs.org/model/boeing-777fht) (registry code 138527M, 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: 37138
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: February 15, 2017
- Certificate issued: March 31, 2022
- Expires: March 31, 2029
- Mode S code: AB8F36
- Registered owner: [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.7558° N, 111.8843° W: Placed by OpenAirDocs at the center of ZIP code 84111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=844FD
- Page: https://openairdocs.org/aircraft/N844FD

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 777FHT)

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 N844FD.

## FAA accident and incident reports

None matched to N844FD.

## Service difficulty reports (24)

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 FDEA202605280682](https://openairdocs.org/sdr/FDEA202605280682), May 28, 2026: FAN. FAILED. PRIOR TO PUSH, HEARD A LOUD POP ON THE FLIGHT DECK. STATUS MESSAGE: EQUIP VENT FAN. REPLACED EQUIPMENT COOLING VENT FAN PER MM 21-27-20-4, FOUND REMOVED FAN WIT
- [SDR FDEA202510202055](https://openairdocs.org/sdr/FDEA202510202055), Oct 20, 2025: SWITCH. OUT OF POSITION. AT FL350 AFTER APPROXIMATELY 2 HOUR STARRED RECEIVING INTERMITTENT OVERSPEED WARNING AND THE UPPER ZIPPER KEPT MOVING UP AND DOWN. THEN AFTER 10 MIN OVERSPEED W
- [SDR FDEA202501130060](https://openairdocs.org/sdr/FDEA202501130060), Jan 13, 2025: LAMP. FAILED. DEBRIEF WITH CREW ENERGENCY LIGHT NEAR GALLEY DOES NOT ILLUMINATE WITH PERFLIGHT EMER LIGHT/TEST LIGHT CHECK. AMM: 33-50-00-2 PER AMM 33-50-00-2, RELAMP ENERGEN
- [SDR FDEA202409281383](https://openairdocs.org/sdr/FDEA202409281383), Sep 28, 2024: PAN. ERODED. LH I/B MAIN FLAP OB SIDE SEAL PAN FOUND EROSION. REPAIRED LH I/B MAIN FLAP OB SIDE SEAL PAN EROSION AS PER B777 SRM 57-53-01-2R-1 AND SRM 51-70-04-2R-10 REV 47.
- [SDR FDEA202203250683](https://openairdocs.org/sdr/FDEA202203250683), Mar 25, 2022: FLOOR PANEL. DELAMINATED. MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 FOUND DELEMINATION AT BL0 STA 1600,1640,1660. MAIN DECK CARGO FLOOR PANEL P/N:152W8650-3 AT BL0 STA 1600,1640,1660 RE
- [SDR FDEA202203040411](https://openairdocs.org/sdr/FDEA202203040411), Mar 4, 2022: DOUBLER. MISALIGNED. DURING PERFORMING EA T G-5710-T0366182 A P2 STEP 11.C.(5), FOUND 01EA ZLJ-8 (BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS TOO CLOSE TO EDGE OF MACHINE
- [SDR FDEA202203040410](https://openairdocs.org/sdr/FDEA202203040410), Mar 4, 2022: DOUBLER. UNKNOWN. DURING PERFORMING EA T G-5710-T0366182 A P1 STEP 11.C.(5), FOUND 01EA ZLJ-8 (BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 LHS TOO CLOSE TO EDGE OF MACHINE
- [SDR FDEA202202250371](https://openairdocs.org/sdr/FDEA202202250371), Feb 25, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL PN: 152W8151-1 AT STA 403-424 LBL 74 FOUND CRACKED. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MA
- [SDR FDEA202202230361](https://openairdocs.org/sdr/FDEA202202230361), Feb 23, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8351-29 FOUND CRACKED AT STA 1015 LBL86. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJO
- [SDR FDEA202202230360](https://openairdocs.org/sdr/FDEA202202230360), Feb 23, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8451-21 FOUND CRACKED AT STA 1331 LBL43. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJO
- [SDR FDEA202202230359](https://openairdocs.org/sdr/FDEA202202230359), Feb 23, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8351-30 FOUND CRACKED AT STA 1014 RBL84. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJO
- [SDR FDEA202202230358](https://openairdocs.org/sdr/FDEA202202230358), Feb 23, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8351-28 FOUND CRACKED AT STA 1014 RBL71. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJO
- [SDR FDEA202202230357](https://openairdocs.org/sdr/FDEA202202230357), Feb 23, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8451-17 FOUND CRACKED AT STA 1248 LBL76. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJO
- [SDR FDEA202202230356](https://openairdocs.org/sdr/FDEA202202230356), Feb 23, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8351-27 FOUND CRACKED AT STA 1013 LBL69. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJO
- [SDR FDEA202202230355](https://openairdocs.org/sdr/FDEA202202230355), Feb 23, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8451-19 FOUND CRACKED AT STA 1398 LBL38. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJO
- [SDR FDEA202202230354](https://openairdocs.org/sdr/FDEA202202230354), Feb 23, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8451-22 FOUND CRACKED AT STA 1365 RBL46. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJO
- [SDR FDEA202202230353](https://openairdocs.org/sdr/FDEA202202230353), Feb 23, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8651-4 FOUND CRACKED AT STA 1434 RBL81. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJOR
- [SDR FDEA202202230352](https://openairdocs.org/sdr/FDEA202202230352), Feb 23, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8651-6 FOUND CRACKED AT STA 1435 RBL11. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJOR
- [SDR FDEA202202230351](https://openairdocs.org/sdr/FDEA202202230351), Feb 23, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL P/N: 152W8451-18 FOUND CRACKED AT STA 1287 RBL82. REPAIRED AS PER B777 SRM 53-00-50-2R RFEPAIR 1 REV 40.0. REPAIR CLASSIFIED AS MAJO
- [SDR FDEA202202230350](https://openairdocs.org/sdr/FDEA202202230350), Feb 23, 2022: FRAME. DENTED. MAIN DECK CARGO MAIN FRAME FOUND DEFORM AT STA 1727 S-19R. DEFORMED FRAME REPAIRED AS PER B777 SRM 53-00-07- 2R REPAIR 1 REV 40.0 AND EA G-5310-T0367399 P1, TIT
- [SDR FDEA201906071253](https://openairdocs.org/sdr/FDEA201906071253), Jun 7, 2019: FLOOR SUPPORT. CRACKED. LOWER BULK CARGO COMPARTMENT STATION 1918 RBL 49.80 FLOOR PANEL STRINGER FOUND CRACK. APPROX 0.5" LENGTH. LOWER BULK CARGO COMPARTMENT STATION 1918 RBL 49.80 FL
- [SDR FDEA201809282741](https://openairdocs.org/sdr/FDEA201809282741), Sep 28, 2018: BATTERY. DISCHARGED. L1 DOOR EPAS BATTERY PACK, STATUS LIGHT BLANK. L1 DOOR ONLY INOP DUE TO ITS EMERGENCY POWER ASSIST SYSTEM INOP. SLIDE/RAFT NOT REMOVED FROM L1 DOOR. R&R EPAS 9 
- [SDR FDEA201712223428](https://openairdocs.org/sdr/FDEA201712223428), Dec 22, 2017: LAMP. INOPERATIVE. DURING POST FLIGHT INSPECTION, EMERGENCY OVERHEAD LIGHT INOPERATIVE DURING TEST. REPLACED THE LAMPS IAW AMM 33-51-03-2. LIGHTS TESTED GOOD. OK FOR SERVICE.
- [SDR FDEA201712093354](https://openairdocs.org/sdr/FDEA201712093354), Dec 9, 2017: FLOOR PANEL. CRACKED. MDIS 844 53-21 1114 09DEC17 NRT OPEN U RAMP AGENT REPORTED THAT CRACKS ON FLOOR PANEL AT FUS. STA1250. (IT IS BETWEEN PDU 30R AND 31R.) SHGN 09DEC17 01:17 NRT U

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Boeing 777FHT aircraft: https://openairdocs.org/model/boeing-777fht/aircraft.md
- The GE GE90-110B1 engine: https://openairdocs.org/engine/ge-ge90-110b1.md

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