# N843FD: 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: 39286
- Year built: 2011
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 9, 2017
- Certificate issued: March 10, 2022
- Expires: March 31, 2029
- Mode S code: AB8B7F
- 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=843FD
- Page: https://openairdocs.org/aircraft/N843FD

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 N843FD.

## FAA accident and incident reports

None matched to N843FD.

## Service difficulty reports (19)

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 FDEA202609171359](https://openairdocs.org/sdr/FDEA202609171359), Sep 17, 2026: HOSE. LOOSE. HYD QTY LOW C EICAS AT 3:45 AFTER TAKEOFF. EICAS WAS REVIEWED AND EVENT RECORD AT 1246Z. THEN RESERVE BRAKES/STRG EICAS OCCURRED. EICAS WAS REVIEWED AND DECISIO
- [SDR FDEA202602110221](https://openairdocs.org/sdr/FDEA202602110221), Feb 11, 2026: SAFETY WIRE. INCORRECT. REF FEA G2560-F0386294 REV C P1 FOUND INCORRECT SAFETY WIRE ON RIGHT DOOR SLIDE. REMOVED AND REPLACED R1 DOOR SLIDE IAW AMM 25-66-01-4-0.
- [SDR FDEA202411011627](https://openairdocs.org/sdr/FDEA202411011627), Nov 1, 2024: LAMP. FAILED. POST-FLT INSP, R1 DOOR EXTERIOR EMERGENGY LT INOP. AMM: 33-51-04-2 RE-LAMPED, REF AMM: 33-51-04-2. EMERGENCY LT'S TEST SATIS, ITEM OK FOR SVC.
- [SDR FDEA202407231045](https://openairdocs.org/sdr/FDEA202407231045), Jul 23, 2024: SKIN. DELAMINATED. LH WING OB FLAP LWR SURFACE FROM IB TO OB 163 INCH CROSS TE TO LE 11 INCH FOUND DELAMINATION. REPAIRED LH WING OB FLAP LWR SURFACE AT OTEF STA188 DELAMINATION A
- [SDR FDEA202201200104](https://openairdocs.org/sdr/FDEA202201200104), Jan 20, 2022: PAN. CORRODED. FOUND WASTE DRAIN VALVE ASSEMBLY INSTALLATION HOLE SURROUND CORROSION. WASTE DRAIN VALVE ASSEMBLY INSTALLATION CORROSION WASTE WATER SERVICE PANEL REMOVED AND R
- [SDR FDEA202201180077](https://openairdocs.org/sdr/FDEA202201180077), Jan 18, 2022: DOUBLER. FAILED. DURING PERFORMING EA T G-5710-T0366180 A P2 STEP 11.C.(5), 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 RHS FOUND TOO CLOSE TO EDGE OF MACHINED
- [SDR FDEA202201180076](https://openairdocs.org/sdr/FDEA202201180076), Jan 18, 2022: DOUBLER. FAILED. DURING PERFORMING EA T G-5710-T0366180 A P1 STEP 11.C.(5), 01EA ZLJ-8(BACB30NY8K*) COUNTERSUNK FASTENER AT STA998 STGR35 LHS FOUND TOO CLOSE TO EDGE OF MACHINED
- [SDR FDEA202201100038](https://openairdocs.org/sdr/FDEA202201100038), Jan 10, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL PN:152W8351-29 FOUND CRACKED AT STA 1031 LBL86. MAIN DECK CARGO FLOOR PANEL PN:152W8351-29 AT STA 1031 LBL 86 REPAIRED AS PER B777 S
- [SDR FDEA202201100037](https://openairdocs.org/sdr/FDEA202201100037), Jan 10, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL PN:152W8351-30 FOUND CRACKED AT STA 1023 RBL88. MAIN DECK CARGO FLOOR PANEL PN:152W8351-30 AT STA 1023 RBL 88 REPAIRED AS PER B777 S
- [SDR FDEA202201100036](https://openairdocs.org/sdr/FDEA202201100036), Jan 10, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL PN:152W8451-17 FOUND CRACKED AT STA 1264 LBL108. MAIN DECK CARGO FLOOR PANEL PN:152W8451-17 AT STA 1264 LBL 108 REPAIRED AS PER B777
- [SDR FDEA202201100035](https://openairdocs.org/sdr/FDEA202201100035), Jan 10, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL PN:152W8451-19 FOUND CRACKED AT STA 1375 LBL36. MAIN DECK CARGO FLOOR PANEL PN:152W8451-19 AT STA 1375 LBL 36 REPAIRED AS PER B777 S
- [SDR FDEA202201100034](https://openairdocs.org/sdr/FDEA202201100034), Jan 10, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL PN:152W8451-21 FOUND CRACKED AT STA 1355 LBL43. MAIN DECK CARGO FLOOR PANEL PN:152W8451-21 AT STA 1355 LBL 43 REPAIRED AS PER B777 S
- [SDR FDEA202201100033](https://openairdocs.org/sdr/FDEA202201100033), Jan 10, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL PN:152W8451-15 FOUND CRACKED AT STA 1321 LBL43.
- [SDR FDEA202201100032](https://openairdocs.org/sdr/FDEA202201100032), Jan 10, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL PN:152W8651-1 FOUND CRACKED AT STA 1475 RBL101. MAIN DECK CARGO FLOOR PANEL PN:152W8651-1 AT STA 1475 RBL 101 REPAIRED AS PER B777 S
- [SDR FDEA202201100031](https://openairdocs.org/sdr/FDEA202201100031), Jan 10, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL PN:152W8651-6 FOUND CRACKED AT STA 1434 RBL35. MAIN DECK CARGO FLOOR PANEL PN:152W8651-6 AT STA 1434 RBL 35 REPAIRED AS PER B777 SRM
- [SDR FDEA202201100030](https://openairdocs.org/sdr/FDEA202201100030), Jan 10, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL PN:152W8651-4 FOUND CRACKED AT STA 1455 RBL71. MAIN DECK CARGO FLOOR PANEL PN:152W8651-4 AT STA 1455 RBL 71 REPAIRED AS PER B777 SRM
- [SDR FDEA202201100029](https://openairdocs.org/sdr/FDEA202201100029), Jan 10, 2022: FLOOR PANEL. CRACKED. MAIN DECK CARGO FLOOR PANEL PN:152W8451-18 FOUND CRACKED AT STA 1276 RBL105. MAIN DECK CARGO FLOOR PANEL PN:152W8451-18 AT STA 1276 RBL 105 REPAIRED AS PER B777
- [SDR FDEA202010092455](https://openairdocs.org/sdr/FDEA202010092455), Oct 9, 2020: TIRE. LOW PRESSURE. AT 4 HOURS ELAPSED TIME AT FL 370 RECEIVED MESSAGE TIRE PRESS NR 10 TIRE. NOTIFIED MOC. TIRE PRESSURE CONTINUED TO DECREASE TO 139 PSI DURING LANDING PHASE. NOT
- [SDR FDEA201711103222](https://openairdocs.org/sdr/FDEA201711103222), Nov 10, 2017: SLIDE. UNSECURE. CLOSED THE L1 DOOR, BUT THEN OPENED IT, THE SLIDE FELL OUT BUT DID NOT INFLATE. REMOVED AND REPLACED THE SLIDE/RAFT AND L1 DOOR RESEVOIR IAW MM 25-66-01-4, AND 

## 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

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.