# N865GT: 2015 Boeing 747-83QF

- Status: Valid registration
- Airframe: [Boeing 747-83QF](https://openairdocs.org/model/boeing-747-83qf) (registry code 13848QF, 467 seats)
- Engine: [GE GENX-2B67](https://openairdocs.org/engine/ge-genx-2b67) (registry code 30234)
- Data sheets: [TCDS E00078NE](https://openairdocs.org/tcds/E00078NE) (General Electric Company GE Aerospace) (OpenAirDocs)
- Serial number: 60118
- Year built: 2015
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: August 14, 2024
- Certificate issued: August 8, 2024
- Expires: August 31, 2031
- Mode S code: ABE212
- Registered owner: [Umb Bank Na Trustee](https://openairdocs.org/faa-owner/UMB%20BANK%20NA%20TRUSTEE)
- Location: [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City)
- Owner type: Corporation
- Owner's area on the map: 40.6171° N, 111.6866° W: Placed by OpenAirDocs at the center of ZIP code 84121, within about 5 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=865GT
- Page: https://openairdocs.org/aircraft/N865GT

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): 15 in force

### Matched by airframe (Boeing 747-83QF)

None in force.

### Matched by engine (GE GENX-2B67)

- [AD 2026-14-03](https://openairdocs.org/ad/2026-14-03): Engine Fuel Distribution · General Electric Company GE Aerospace GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2 and 17 more. Effective Aug 21, 2026
- [AD 2026-04-09](https://openairdocs.org/ad/2026-04-09): Turbine Engine Compressor Section · General Electric GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2 and 17 more. Effective Mar 11, 2026
- [AD 2024-25-07](https://openairdocs.org/ad/2024-25-07): Turbine Engine Compressor Section · General Electric GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2 and 17 more. Effective Feb 12, 2025
- [AD 2022-25-20](https://openairdocs.org/ad/2022-25-20): Turbine Engine Compressor Section, Turbine Section · General Electric GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2 and 17 more. Effective Jan 26, 2023
- [AD 2022-20-12](https://openairdocs.org/ad/2022-20-12): Turbine Engine Compressor Section, Turbine Section · General Electric GEnx-1B54/P2, GEnx-1B58/P2, GEnx-1B64/P2 and 13 more. Effective Nov 16, 2022
- [AD 2022-03-16](https://openairdocs.org/ad/2022-03-16): Turbine Section · General Electric GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2 and 17 more. Effective Mar 21, 2022
- [AD 2022-04-07](https://openairdocs.org/ad/2022-04-07): Fuel Controlling System · General Electric GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2 and 17 more. Effective Mar 9, 2022
- [AD 2021-21-05](https://openairdocs.org/ad/2021-21-05): Engine Controls · General Electric GEnx-1B64, GEnx-1B64/P1, GEnx-1B64/P2 and 17 more. Effective Dec 28, 2021
- [AD 2021-13-16](https://openairdocs.org/ad/2021-13-16): Engine Fuel Distribution · General Electric GEnx-2B67, GEnx-2B67/P and GEnx-2B67B. Effective Aug 25, 2021
- [AD 2021-11-07](https://openairdocs.org/ad/2021-11-07): Turbine Engine Compressor Section · General Electric Genx-1B76A/P2, GEnx-1B64, GEnx-1B64/P1 and 17 more. Effective Jul 30, 2021
- [AD 2020-13-04](https://openairdocs.org/ad/2020-13-04): Engine Controls · General Electric Genx-1B76A/P2, GEnx-1B54, GEnx-1B54/P1 and 28 more. Effective Jul 24, 2020
- [AD 2019-02-01](https://openairdocs.org/ad/2019-02-01): Turbine section · General Electric Genx-1B76A/P2, GEnx-1B54, GEnx-1B54/P1 and 28 more. Effective Feb 25, 2019
- [AD 2018-21-12](https://openairdocs.org/ad/2018-21-12): Engine Fuel Distribution · General Electric GEnx-2B67, GEnx-2B67/P and GEnx-2B67B. Effective Jan 4, 2019
- [AD 2013-23-14](https://openairdocs.org/ad/2013-23-14): Critical rotating life-limited parts (LLPs) · General Electric GEnx-2B67 and GEnx-2B67B. Effective Jan 7, 2014
- [AD 2012-19-08](https://openairdocs.org/ad/2012-19-08): Fan mid shafts (FMS) · General Electric GEnx-1B54, GEnx-1B54/P1, GEnx-1B58 and 13 more. Effective Sep 21, 2012

### Historical (superseded or no longer in force)

- [AD 2018-16-07](https://openairdocs.org/ad/2018-16-07) (historical): Turbine Section · General Electric Genx-1B76A/P2, GEnx-1B54, GEnx-1B54/P1 and 28 more. Effective Aug 15, 2018
- [AD 2017-09-06](https://openairdocs.org/ad/2017-09-06) (historical): Engine · General Electric Genx-1B76A/P2, GEnx-1B54, GEnx-1B54/P1 and 28 more. Effective Jun 9, 2017
- [AD 2015-15-03](https://openairdocs.org/ad/2015-15-03) (historical): Power loss in ice crystal icing (ICI) conditions · General Electric GEnx-1B54, GEnx-1B54/P1, GEnx-1B54/P2 and 26 more. Effective Aug 24, 2015

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N865GT.

## FAA accident and incident reports

None matched to N865GT.

## Service difficulty reports (13)

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 UIEA2026083100835](https://openairdocs.org/sdr/UIEA2026083100835), Aug 29, 2026: SKIN. BROKEN. BROKEN SKIN & STRIP, LT WING NR 9 VC FLAP FRONT MOLDING. PERFORM PERMANENT REPAIR. DAMAGE ON SKIN PANEL ASSY OF LT WING NR 9 VC FLAP IAW EGAT EI T2026A57M.1713,
- [SDR UIEA2026083100836](https://openairdocs.org/sdr/UIEA2026083100836), Aug 29, 2026: STRINGER. CRACKED. CRACK DAMAGE ON STRINGER 1L, BS 2360, FWD SIDE. PERFORMED REPAIR IAW SRM 53-60-03-2R-8, REV 49. JOB COMPLETED AND CONDITION CHKD NORMAL.
- [SDR UIEA2026083100837](https://openairdocs.org/sdr/UIEA2026083100837), Aug 29, 2026: STRINGER. CRACKED. CRACK DAMAGE ON STRINGER 2R, BS 2360, FWD SIDE. PERFORMED REPAIR IAW SRM 53-60-03-2R-8, REV 49. JOB COMPLETED AND CONDITION CHK NORMAL.
- [SDR UIEA2026083100838](https://openairdocs.org/sdr/UIEA2026083100838), Aug 29, 2026: STRINGER. CRACKED. CRACK DAMAGE ON STRINGER 10R, BS 2180, AFT SIDE. ACCOMPLISHED SRM 53-60-03-2R-3, ALTERNATIVE 3, REV 49. JOB COMPLETED, NO FURTHER DEFECTS NOTED.
- [SDR UIEA2026083100839](https://openairdocs.org/sdr/UIEA2026083100839), Aug 29, 2026: STRINGER. CRACKED. CRACK DAMAGE ON STRINGER 11R, BS 1960, AFT SIDE. REPAIRED DAMAGED AREA IAW SRM 53-60-03-21-4, ALTERNATIVE 3, REV 49. JOB COMPLETED, NO FURTHER DEFECTS NOTED.
- [SDR UIEA2026083100840](https://openairdocs.org/sdr/UIEA2026083100840), Aug 29, 2026: STRINGER. CRACKED. CRACK DAMAGE ON STRINGER 10L, BS 1960, FWD SIDE. ACCOMPLISHED SRM 53-60-03-2R-4, ALTERNATIVE 2, REV 49. JOB COMPLETED, NO FURTHER DEFECTS NOTED.
- [SDR UIEA2026083100841](https://openairdocs.org/sdr/UIEA2026083100841), Aug 29, 2026: STRINGER. CRACKED. CRACK DAMAGE ON STRINGER 1R, BS 2360, FWD SIDE. REPAIRED DAMAGE AREA IAW SRM 53-60-03-2R-8, REV 49. JOB COMPLETED. NO FURTHER DEFECTS NOTED.
- [SDR UIEA2026083100842](https://openairdocs.org/sdr/UIEA2026083100842), Aug 29, 2026: STRINGER. CRACKED. CRACK DAMAGE ON STRINGER 7R, BS 2360, FWD SIDE. REPAIRED DAMAGED AREA IAW SRM 53-60-03-2R-8 REV 49. JOB COMPLETED, NO FURTHER DEFECTS NOTED.
- [SDR UIEA2026083100843](https://openairdocs.org/sdr/UIEA2026083100843), Aug 29, 2026: STRINGER. CRACKED. CRACK DAMAGE ON STRINGER 2L, BS 2360, FWD SIDE. REPAIRED DAMAGED AREA IAW SRM 53-60-03-2R-8, REV 49. JOB COMPLETED, NO FURTHER DEFECTS NOTED.
- [SDR UIEA2026022300066](https://openairdocs.org/sdr/UIEA2026022300066), Feb 22, 2026: PUMP. FAULTED. HYD PRESS #4 EICAS MESSAGE HYDRAULIC DEMAND PUMP #4 FAILED IN CRUISE. REPLACED ENGINE DRIVEN PUMP TO SUPPLY HYDRAULIC PRESSURE. ENG #4 HYD DEMAND PUMP TRANSFER 
- [SDR UIEA2024111701094](https://openairdocs.org/sdr/UIEA2024111701094), Nov 17, 2024: ACTUATOR. FAULTED. GEAR TILT EICAS MSG(<P>REPLACED NEW BUSHINGS P/N 163U2511-1, BOLT ASSY P/N 65B05481-3 AND POSITION ACTUATOR P/N 293U4202-1 AND HYD BLEEDING AND LEAK CHECK NORMA
- [SDR UIEA2024091600909](https://openairdocs.org/sdr/UIEA2024091600909), Sep 16, 2024: CONTROL MODULE. FAULTED. DURING ALTERNATE GEAR EXTENSION OF THE NOSE AND BODY EICAS GEAR TILT MESSAGE DISPLAYED.(<P>R/R LH BODY GEAR TILT SENSOR (S2653) &AMP; RH BODY GEAR TRUCK TILT SE
- [SDR UIEA2024091300908](https://openairdocs.org/sdr/UIEA2024091300908), Sep 13, 2024: PSEU. FAULTED. GEAR TILT MSG DURING ALTERNATE EXTENSION OF LANDING GEAR. RECEIVED GEAR TILT MESSAGE. GEAR TILT, GEAR DISAGREE, GEAR MONITOR STS MSG(<P>ACCOMPLISHED ALTERNATE E

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Related

- Other Boeing 747-83QF aircraft: https://openairdocs.org/model/boeing-747-83qf/aircraft.md
- The GE GENX-2B67 engine: https://openairdocs.org/engine/ge-genx-2b67.md

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