# N842FD: 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: 38969
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 22, 2017
- Certificate issued: February 9, 2022
- Expires: February 28, 2029
- Mode S code: AB87C8
- 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=842FD
- Page: https://openairdocs.org/aircraft/N842FD

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 N842FD.

## FAA accident and incident reports

None matched to N842FD.

## 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 FDEA202610081491](https://openairdocs.org/sdr/FDEA202610081491), Oct 8, 2026: LAMP. FAILED. PRE-FLT MX INSP, (1EA) DIRECT GALLEY OVERHEAD EMERGENCY LIGHT INOP. REPLACED THE LAMPS, IAW AMM 33-51-04-2. LIGHTS TESTED SATIS, ITEM OK FOR SVC.
- [SDR FDEA202608261230](https://openairdocs.org/sdr/FDEA202608261230), Aug 26, 2026: LAMP. INOPERATIVE. POST-FLT INSP, (1EA) OVRHD SUPRNMRY AREA EMERGENCY LIGHT INOP. RE-LAMPED, IAW AMM: 33-51-04-2. LIGHT TESTS SATIS, OK FOR SVC.
- [SDR FDEA202606040672](https://openairdocs.org/sdr/FDEA202606040672), Jun 4, 2026: LAMP. NO TEST. EMERGENCY LIGHT OVER THE GALLEY TESTS BAD. AMM 33-50-00-2 RELAMPED EMER LIGHT OVER THE GALLEY. OPS TEST OK. AIRCRAFT GOOD TO GO.
- [SDR FDEA202511172187](https://openairdocs.org/sdr/FDEA202511172187), Nov 17, 2025: LAMP. FAILED. FOUND RT DOOR FWD EXIT SIGN - LAMP INOPERATIVE. AMM: 33-51-01-2 IAW AMM 33-51-01-2, REPLACED EXIT SIGN LAMPS, OPS TEST GOOD. OK TO CONTINUE. IAW AMM 33-51-01-2,
- [SDR FDEA202507171232](https://openairdocs.org/sdr/FDEA202507171232), Jul 17, 2025: OIL SYSTEM. LEAKING. OIL QTY ON RIGHT ENGINE WENT TO 4 QTS ABOUT 3.5 HOURS INTO FLIGHT. EVENTUALLY DECREASED TO ZERO OIL QTY ABOUT 1.5 HOURS LATER. OIL PRESSURE DECREASED TO 35 IN D
- [SDR FDEA202408091095](https://openairdocs.org/sdr/FDEA202408091095), Aug 9, 2024: SKIN. DELAMINATED. RH WING OB FLAP LWR SURFACE FOUND DENT WITH DISBOND AT 275 IN AWAY FROM OB, 10 IN AWAY TO AFT EDGE. REPAIRED RH WING OB FLAP LWR SURFACE DENT AT OTEF STA 251 AS
- [SDR FDEA202408081093](https://openairdocs.org/sdr/FDEA202408081093), Aug 8, 2024: SKIN. DENTED. DURING PERFORM E.A :G-5330-T0368078 - FUSELAGE - PLATES&SKINS - AFT FUSELAGE SKIN PANEL STA 1902.5 - 1907.5, STR 46R - 47R, THE DENT DAMAGE FOR CAT C INTERIM RE
- [SDR FDEA202408021078](https://openairdocs.org/sdr/FDEA202408021078), Aug 2, 2024: BULB. FAILED. SVC CK, (1EA) SUPRNMRY AREA OVERHEAD EMERGENCY LIGHT INOP. RE-LAMPED, REF B777 AMM: 33-50-00-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA202403110276](https://openairdocs.org/sdr/FDEA202403110276), Mar 11, 2024: WIRE HARNESS. DAMAGED. DURING TAXI OUT MAIN GEAR STEERING ALERT ON EICAS - FLASHED UP & DISAPPEARED DURING ONE OF FOUR TURNS TO RUNWAY. AFTER LINE UP & TOGA PRESSED - MAIN GEAR STEERI
- [SDR FDEA202311081841](https://openairdocs.org/sdr/FDEA202311081841), Nov 8, 2023: LIGHT. INOPERATIVE. POST-FLT INSP, R-1 DOOR OVRHD EMERGENCY LT INOP. RE-LAMPED, REF B777 AMM: 33-51-04-2. LT'S TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA202203180568](https://openairdocs.org/sdr/FDEA202203180568), Mar 18, 2022: NONE. NONE. POST-FLT INSP, R-1 EXTERIOR EMERGENCY LT INOP. RE-LAMPED, REF B777 AMM: 33-51-04-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA202202140291](https://openairdocs.org/sdr/FDEA202202140291), Feb 14, 2022: ANGLE. UNKNOWN. WHILE ACCOMPLISHING EA G-5710-T0366056A P2 RIGHT HAND LOWER CHORD INSTALLATION ON STEP (10.E), MENTIONED IN EA, FASTENER WET INSTALL WITH BMS 5-95 SEALANT (GENE
- [SDR FDEA202202140290](https://openairdocs.org/sdr/FDEA202202140290), Feb 14, 2022: ANGLE. UNKNOWN. WHILE ACOMPLISHING EA G-5710-T0366056A P1 LEFT HAND LOWER CHORD INSTALLATION ON STEP (10.E), MENTIONED IN EA, FASTENER WET INSTALL WITH BMS 5-95 SEALANT (GENERA
- [SDR FDEA202201160074](https://openairdocs.org/sdr/FDEA202201160074), Jan 16, 2022: DOUBLER. UNKNOWN. WHILE ACCOMPLISHING RIGHT HAND E.A.#G-5710-T0366056A P2 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35R NEAR MILLED EDGE. COMPLIED W
- [SDR FDEA202201160073](https://openairdocs.org/sdr/FDEA202201160073), Jan 16, 2022: DOUBLER. UNKNOWN. WHILE ACCOMPLISHING LEFT HAND E.A.#G-5710-T0366056A P1 FOUND NEW FUSELAGE SKIN DOUBLER EXISTING HOLE AT STATION 998 STRINGER S-35L NEAR MILLED EDGE COMPLIED WIT
- [SDR FDEA202201160072](https://openairdocs.org/sdr/FDEA202201160072), Jan 16, 2022: SKIN. CRACKED. DURING ACCOMPLISHMENT OF HIGH FREQUENCY EDDY CURRENT INSPECTION ON RIGHT HAND EXTERIOR FUSELAGE SKIN COMMON TO UNDERWING LONGERON FITTING, FOUND 01 EACH CRACK A
- [SDR FDEA202201120052](https://openairdocs.org/sdr/FDEA202201120052), Jan 12, 2022: STRINGER. CRACKED. LOWER BULK CARGO COMPARTMENT STATION 1979 RIGHT BUTT LINE 49.5 STRINGER FOUND WITH CRACK AS MARKED. LOWER BULK CARGO COMPARTMENT STATION 1979 RIGHT BUTT LINE 49
- [SDR FDEA202201120051](https://openairdocs.org/sdr/FDEA202201120051), Jan 12, 2022: STRINGER. CRACKED. LOWER BULK CARGO COMPARTMENT STATION 1937, RIGHT BUTT LINE 41.5 STRINGER FOUND WITH CRACK AS MARK. LOWER BULK CARGO COMPARTMENT STATION 1937 RIGHT BUTT LINE 41.
- [SDR FDEA202108242079](https://openairdocs.org/sdr/FDEA202108242079), Aug 24, 2021: TIRE. LEAKING. TIRE PRESSURE EICAS. COMPLIED WITH EICAS PROCEDURES. EMERGENCY DECLARATION MADE BY ATC IN ORDER FOR US TO USE RUNWAY 36C TO LAND. FOUND NO VISUAL DEFECTS WITH T
- [SDR FDEA202107041676](https://openairdocs.org/sdr/FDEA202107041676), Jul 4, 2021: FAN. FAILED. RH LOWER RECIRCULATION FAN IS CREATING VERY LOAD HUMING SOUND DURING OPERATION. FOUND R/H RECIRCULATION FAN INBOARD FILTER DEFORMED AND DRAWN DOWN INTO THE R/H 
- [SDR FDEA2020071091476](https://openairdocs.org/sdr/FDEA2020071091476), Jul 9, 2020: LAMP. INOPERATIVE. POST-FLT INSPECTION, L1 DOOR OVRHD EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS.
- [SDR FDEA2020071091475](https://openairdocs.org/sdr/FDEA2020071091475), Jul 9, 2020: LAMP. INOPERATIVE. POST-FLT INSPECTION, L1 OVERHEAD EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM 33-51-04-2. LIGHT TESTED SATISFACTORY, OK FOR SERVICE.
- [SDR FDEA202007031438](https://openairdocs.org/sdr/FDEA202007031438), Jul 3, 2020: BRAKE ASSY. FIRE. NR 2 BRAKE CAUSED OVERHEAT AND THERMAL OF NR 2 MAIN WHEEL ASSY. REMOVED AND REPLACED THE NR 2 BRAKE IAW 32-45-07-4.
- [SDR FDEA2020070631438](https://openairdocs.org/sdr/FDEA2020070631438), Jul 3, 2020: BRAKE. OVERHEATED. NR 2 BRAKE CAUSED OVERHEAT AND THERMAL OF NR 2 MAIN WHEEL ASSY. MPN: C20558000 POS: 2 SRL: 11467, REMOVED AND REPLACED NR 2 BRAKE PER 32-45-07-4 MAIN LANDING GE
- [SDR FDEA2020031980593](https://openairdocs.org/sdr/FDEA2020031980593), Mar 18, 2020: LIGHT. INOPERATIVE. MDIS 842 33-50 3495 18MAR20 MEM POST-FLT INSP L-1 EXTERIOR EMERGENCY LT INOP. FACT 18MAR20 07:12 MEM RE-LAMPED, REF B777 AMM: 33-51-04-2. EMERGENCY LT'S TEST SA
- [SDR FDEA201908302047](https://openairdocs.org/sdr/FDEA201908302047), Aug 30, 2019: UNKNOWN. MALFUNCTIONED. ON TAXI IN ATTEMPTED TO MAKE LEFT TURN TILLER BECAME EXTREMELY STIFF AND THE AIRCRAFT WAS SLOW TO TURN. STOPPED TURN COORDINATED WITH GROUND TO TAXI STRAIGTH AH
- [SDR FDEA201812043425](https://openairdocs.org/sdr/FDEA201812043425), Dec 4, 2018: LIGHT. INOPERATIVE. POST-FLT INSP, R1 DOOR EXTERIOR EMERGENCY EXIT LT INOP ON LIGHT TEST. RELAMPED, REF AMM 33-51-04-2. LT TESTS SATIS, ITEM OK FOR SVC.
- [SDR FDEA201809192588](https://openairdocs.org/sdr/FDEA201809192588), Sep 19, 2018: LAMP. INOPERATIVE. POST-FLT INSPECTION, R-1 DOOR OUTSIDE EMERGENCY LIGHT INOPERABLE. RE-LAMPED, REF B777 AMM: 33-51-04-2. EMERGENCY LIGHTS TEST SATISFACTORY, ITEM OK FOR SERVICE.
- [SDR FDEA201809192587](https://openairdocs.org/sdr/FDEA201809192587), Sep 19, 2018: LAMP. INOPERATIVE. POST-FLT INSPECTION, R-1 DOOR OUTSIDE EMERGENCY LIGHT INOPERABLE RE-LAMPED, REF B777 AMM 33-51-04-2. EMERGENCY LIGHTS TEST SATISFACTORY, ITEM OK FOR SERVICE.
- [SDR FDEA2018092692587](https://openairdocs.org/sdr/FDEA2018092692587), Sep 19, 2018: LAMP. NO TEST. POST-FLT INSP, R-1 DOOR OUTSIDE EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMP IAW AMM: 33-51-04-2. EMERGENCY LIGHTS TESTED SATISFACTORY, OK FOR SERVICE.
- [SDR FDEA2020021092589](https://openairdocs.org/sdr/FDEA2020021092589), Sep 19, 2018: LAMP. INOPERATIVE. POST-FLT INSP, R-1 DOOR OUTSIDE EMERGENCY LT INOP RE-LAMPED, REF B777 AMM: 33-51-04-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA2020021092588](https://openairdocs.org/sdr/FDEA2020021092588), Sep 19, 2018: LAMP. INOPERATIVE. POST-FLT INSP, R-1 DOOR OUTSIDE EMERGENCY LT INOP RE-LAMPED, REF B777 AMM: 33-51-04-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA2020021092587](https://openairdocs.org/sdr/FDEA2020021092587), Sep 19, 2018: LAMP. INOPERATIVE. POST-FLT INSP, R-1 DOOR OUTSIDE EMERGENCY LT INOP RE-LAMPED, REF B777 AMM: 33-51-04-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA2018092092589](https://openairdocs.org/sdr/FDEA2018092092589), Sep 19, 2018: LIGHT. INOPERATIVE. POST FLT INSP, R1 DOOR OUTSIDE EMERGENCY LIGHT INOP. RE-LAMPED, REF AMM 33-51-04-2. EMERGENCY LIGHTS TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA2018092092588](https://openairdocs.org/sdr/FDEA2018092092588), Sep 19, 2018: LIGHT. INOPERATIVE. POST FLT INSP, R1 DOOR OUTSIDE EMERGENCY LIGHT INOP. RE-LAMPED, REF AMM 33-51-04-2. EMERGENCY LIGHTS TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA2018092092587](https://openairdocs.org/sdr/FDEA2018092092587), Sep 19, 2018: LIGHT. INOPERATIVE. POST FLT INSP, R1 DOOR OUTSIDE EMERGENCY LIGHT INOP. RE-LAMPED, REF AMM 33-51-04-2. EMERGENCY LIGHTS TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA201711173253](https://openairdocs.org/sdr/FDEA201711173253), Nov 17, 2017: LENS. DETACHED. L1 DOOR AFT EMERGENCY LENS DETACHED. COMPLIED WITH EA G-3350-T0336667, PART 3. INSTALLED THE LIGHT ASSY AND OPS CHECKED GOOD IAW MM 33-51-01-2.

## 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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