# N864GT: 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-2B67B](https://openairdocs.org/engine/ge-genx-2b67b) (registry code 30165) - Data sheets: [TCDS E00078NE](https://openairdocs.org/tcds/E00078NE) (General Electric Company GE Aerospace) (OpenAirDocs) - Serial number: 60117 - Year built: 2015 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: October 20, 2024 - Certificate issued: October 2, 2024 - Expires: October 31, 2031 - Mode S code: ABDE5B - 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=864GT - Page: https://openairdocs.org/aircraft/N864GT 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): 16 in force ### Matched by airframe (Boeing 747-83QF) None in force. ### Matched by engine (GE GENX-2B67B) - [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 2013-16-15](https://openairdocs.org/ad/2013-16-15): Booster anti-ice (BAI) air duct · General Electric GEnx-2B67B. Effective Sep 23, 2013 - [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 N864GT. ## FAA accident and incident reports None matched to N864GT. ## Service difficulty reports (23) 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 UIEA2026081200746](https://openairdocs.org/sdr/UIEA2026081200746), Aug 12, 2026: FLASHLIGHT. INOPERATIVE. CPTS FLASHLIGHT INOPERATIVE. TRANSFER TO DMI 257381 PER MEL 25-60-03-01 CAT C DUE DATE 22AUG26. REMOVED AND REPLACED CAPT FLASHLIGHT ASSY IAW AMM 25-60-60/201. - [SDR UIEA2026060300428](https://openairdocs.org/sdr/UIEA2026060300428), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER S-21R STA 2360 AFT SIDE.(

1. PERFORMED REPAIR IAW W/S 60375 (SRM 53-80-03-2R-3 REV 48). 2. JOB COMPLETED AND CONDITION CHECK NOR - [SDR UIEA2026060300431](https://openairdocs.org/sdr/UIEA2026060300431), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER S-20L STA 2360 AFT SIDE.(

1. PERFORMED REPAIR IAW W/S 60374 (SRM 53-80-03-2R-3 REV 48). 2. JOB COMPLETED AND CONDITION CHECK NOR - [SDR UIEA2026060300432](https://openairdocs.org/sdr/UIEA2026060300432), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER S-12R STA 2180 FWD AND AFT SIDE. PERFORMED REPAIR IAW W/S 60371 (SRM 53-60-03-2R-3 ALTERNATIVE 4, REV 48). JOB COMPLETED AND CONDI - [SDR UIEA2026060300433](https://openairdocs.org/sdr/UIEA2026060300433), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER S-12L STA 2180 FWD AND AFT SIDE AND SPLICE CRACK. PERFORMED REPAIR IAW W/S 60370 (SRM 53-60-03-2R-3 ALTERNATIVE 4, REV 48). JOB CO - [SDR UIEA2026060300434](https://openairdocs.org/sdr/UIEA2026060300434), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER S-7R STA 2360 FWD SIDE. PERFORMED REPAIR IAW W/S 60392 (SRM 53-60-03-2R-8 REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026060300435](https://openairdocs.org/sdr/UIEA2026060300435), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER S-10R STA 1960 FWD AND AFT SIDE. PERFORMED REPAIR IAW W/S 60419 (SRM 53-60-03-2R-4 ALTERNATIVE 4, REV 48). JOB COMPLETED AND CONDI - [SDR UIEA2026060300436](https://openairdocs.org/sdr/UIEA2026060300436), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER S-12L STA 1960 FWD AND AFT SIDE. PERFORMED REPAIR IAW W/S 60417 (SRM 53-60-03-2R-4 ALTERNATIVE 4, REV 48). JOB COMPLETED AND CONDI - [SDR UIEA2026060300437](https://openairdocs.org/sdr/UIEA2026060300437), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER S-9R STA 1960 FWD AND AFT SIDE. PERFORMED REPAIR IAW W/S 60418 (SRM 53-60-03-2R-4 ALTERNATIVE 4, REV 48). JOB COMPLETED AND CONDIT - [SDR UIEA2026060300438](https://openairdocs.org/sdr/UIEA2026060300438), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER S-10R STA 2180 FWD AND AFT SIDE. PERFORMED REPAIR IAW W/S 60416 (SRM 53-60-03-2R-3 ALTERNATIVE 4, REV 48). JOB COMPLETED AND CONDI - [SDR UIEA2026060300439](https://openairdocs.org/sdr/UIEA2026060300439), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER S-1R STA 2360 FWD SIDE.(

1. PERFORMED REPAIR IAW W/S 60391 (SRM 53-60-03-2R-8 REV 48). 2. JOB COMPLETED AND CONDITION CHECK NORM - [SDR UIEA2026060300440](https://openairdocs.org/sdr/UIEA2026060300440), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER S-46R STA 2360 FWD SIDE.(

1. PERFORMED REPAIR IAW W/S 60393 (SRM 53-60-03-2R-8 REV 48). 2. JOB COMPLETED AND CONDITION CHECK NOR - [SDR UIEA2026060300441](https://openairdocs.org/sdr/UIEA2026060300441), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGE ON THE STRINGER S-38L STA 2360 FWD SIDE. PERFORMED REPAIR IAW W/S 60394 (SRM 53-60-03-2R-8 REV 48). JOB COMPLETED AND CONDITION CHECK NORMAL.

) - [SDR UIEA2026060300442](https://openairdocs.org/sdr/UIEA2026060300442), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGE ON THE STRINGER S-44L STA 2360 FWD SIDE. REPAIRED DAMAGED AREA IAW W/S 60395 (SRM 53-60-03-2R-8 REV 48) AND EI T2026A53M-1112 REV 0. JOB COMPLETED - [SDR UIEA2026060300443](https://openairdocs.org/sdr/UIEA2026060300443), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGE ON THE STRINGER S-16R STA 2360 FWD SIDE. PERFORMED REPAIR IAW EI T2026A53M-1042 REV 2. JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026060300444](https://openairdocs.org/sdr/UIEA2026060300444), Jun 3, 2026: SKIN. DENTED. DENT ON FUSELAGE AT BS 640, STRINGER 43R - 44R WITHIN SRM LIMITS, ACCOMPLISHED EI T2026A53M-1074 REV 1 AND SRM 53-00-01-2R-10 REPAIR 10 REV 48. 2. JOB COMPLETED - [SDR UIEA2026060300445](https://openairdocs.org/sdr/UIEA2026060300445), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGE ON THE STRINGER S-42L STA 2598 AFT SIDE. PERFORMED REPAIR IAW W/S 60361 (SRM 53-80-03-2R-1 REV 48) AND EI T2026A53M-1093 REV 1. JOB COMPLETED AND C - [SDR UIEA2026060300446](https://openairdocs.org/sdr/UIEA2026060300446), Jun 3, 2026: STRINGER. CRACKED. CRACK DAMAGED ON THE STRINGER S-25R BS 2598 AFT SIDE. REPAIRED IAW EI T2026A53M-1037 REV 1. 2. JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2026060300447](https://openairdocs.org/sdr/UIEA2026060300447), Jun 3, 2026: SKIN. DAMAGED. CRACK AND BROKEN DAMAGE ON SKIN PANEL ASSY OF LT WING NR 9 V.C FLAP. REPAIRED CRACK AND BROKEN DAMAGE ON SKIN PANEL ASSY OF LT WING NR 9 V.C FLAP IAW EGAT EI T2 - [SDR UIEA2026060300448](https://openairdocs.org/sdr/UIEA2026060300448), Jun 3, 2026: SPAR. DAMAGED. FOUND OTBD ELEVATOR FRONT SPAR INNER CHORD DAMAGE AT LT LE HSS 231. ACCOMPLISHED EO 1955A065 PART 1 REV 0 AND DWG 65B05731 SH 8 REV A, SH 9 REV A AND EI T2026A5 - [SDR UIEA2026060300449](https://openairdocs.org/sdr/UIEA2026060300449), Jun 3, 2026: SPAR. DAMAGED. FOUND OTBD ELEVATOR FRONT SPAR INNER CHORD DAMAGE AT RT LE HSS 314 AND WEB ORIGINAL REPAIR.. ACCOMPLISHED EO 1955A064 REV 1 & 2. JOB COMPLETED AND CONDITION CHE - [SDR UIEA2026060300450](https://openairdocs.org/sdr/UIEA2026060300450), Jun 3, 2026: SKIN. CRACKED. FOUND OTBD ELEVATOR FRONT SPAR LE SKIN CRACKED AT RT L/E HSS 260. ACCOMPLISHED EO 1955A064 REV 1.& 2. JOB COMPLETED AND CONDITION CHECK NORMAL. - [SDR UIEA2025060600733](https://openairdocs.org/sdr/UIEA2025060600733), Jun 7, 2025: ENGINE. FAILED. ENGINE 3 FAILURE ON TAKEOFF ROLL AT 110 KNOTS REJECTED TAKEOFF AND CLEARED RUNWAY. NR 3 ENG BORESCOPE INSPECTION PERFORMED IAW AMM 72-00-00-290-801-G00, FOUND H ## 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-2B67B engine: https://openairdocs.org/engine/ge-genx-2b67b.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.