# N702GT: 2012 Boeing 777F16 - Status: Valid registration - Airframe: [Boeing 777F16](https://openairdocs.org/model/boeing-777f16) (registry code 138527Q, 11 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: 38091 - Year built: 2012 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: September 9, 2012 - Certificate issued: July 8, 2021 - Expires: July 31, 2028 - Mode S code: A95CA4 - Registered owner: [U S Bank Na Trustee](https://openairdocs.org/faa-owner/U%20S%20BANK%20NA%20TRUSTEE) - Location: [Hartford, CT](https://openairdocs.org/faa-place/CT/Hartford) - Owner type: Corporation - Owner's area on the map: 41.7651° N, 72.6708° W: Placed by OpenAirDocs at the center of ZIP code 06103, 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=702GT - Page: https://openairdocs.org/aircraft/N702GT 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 777F16) 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 N702GT. ## FAA accident and incident reports None matched to N702GT. ## Service difficulty reports (32) 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 UIEA2026090600854](https://openairdocs.org/sdr/UIEA2026090600854), Sep 6, 2026: EXTINGUISHER. EXPIRED. PORTABLE WATER FIRE EXTINGUISHER EXPIRED. R & R PORTABLE WATER FIRE EXTINGUISHER FWD IAW AMM 26-26-02, REV 107, & IPC 26-26-02-01, REV 25. NO FURTHER DEFECTS NO - [SDR UIEA2026082600800](https://openairdocs.org/sdr/UIEA2026082600800), Aug 26, 2026: SEAL. BROKEN. CAPT LIFE VEST TAMPER SEAL BROKEN. REMOVED AND REPLACED THE LIFE VEST IAW AMM 25-62-01-960-005. OPS CHKD OK. - [SDR UIEA2026081400756](https://openairdocs.org/sdr/UIEA2026081400756), Aug 14, 2026: BULB. INOPERATIVE. CAPTAIN FLASHLIGHT INOPERATIVE. TRANSFER TO MDDR 257506 PER MEL 25-64-02C CAT C. R/R CAPT FLASHLIGHT AND HOLDER IAW AMM 25-64-01. OPS CHK AND FUNCTIONAL CHK GOO - [SDR UIEA2026072400647](https://openairdocs.org/sdr/UIEA2026072400647), Jul 23, 2026: CONTACT. DIRTY. FO`S FLASHLIGHT GREEN LIGHT INOPERATIVE. CLEANED ELECTRICAL CONTACTS & OPS CHK FLASHLIGHT PRESS TO TEST, NORMAL IAW AMM 25-64-01. FLASHLIGHT TURNS ON NML

) - [SDR UIEA2026061500500](https://openairdocs.org/sdr/UIEA2026061500500), Jun 11, 2026: BUTTON. INOPERATIVE. 1ST OBS O2 MASK RESET BUTTON INOPERATIVE. SWAPPED 1ST OBS O2 MASK & STOWAGE BOX WITH 2ND OBS O2 MASK & STOWAGE BOX PER AMM 35-11-19 & IPC 35-11-18-01. OPS & - [SDR UIEA2026051100310](https://openairdocs.org/sdr/UIEA2026051100310), May 11, 2026: BATTERY. INOPERATIVE. CAPTAIN FLASHLIGHT HOLDER LIGHT TEST INDICATION INOP. TRANSFER TO DMI 252376 PER MEL 25-64-02C CAT C. REMOVED AND REPLACED BATTERY PACK CAPT'S SIDE IAW AMM 25-6 - [SDR UIEA2026040800151](https://openairdocs.org/sdr/UIEA2026040800151), Apr 8, 2026: PLACARD. UNSECURE. RIGHT SIDE EVAS OPEN FOR EMERGENCY USE ONLY PLACARD NOT SECURED(

FO EVAS INSP OK AND R/R TAMPER SEAL PER AMM 25-60-99 REV 106. NO FURTHER DEFECTS NOTED. DMI 2 - [SDR UIEA2026033000115](https://openairdocs.org/sdr/UIEA2026033000115), Mar 29, 2026: SEAL. BROKEN. CAPTAIN'S EVAS SEAL BROKEN. INSTALLED MISSING TAMPER SEAL IAW AMM 25-64-00. NO FURTHER DEFECTS NOTED. - [SDR UIEA2026020800046](https://openairdocs.org/sdr/UIEA2026020800046), Feb 8, 2026: FLASHLIGHT. NO TEST. CAPT EMERGENCY FLASHLIGHT INDICATES RED WHEN PRESS TO TEST TO SEE IF FLASHLIGHT WORKS(

REMOVED AND REPLACED THE CAPTAIN'S PORTABLE FLASHLIGHT IAW AMM 25-64-01 - [SDR UIEA2026021080046](https://openairdocs.org/sdr/UIEA2026021080046), Feb 8, 2026: FLASHLIGHT. FAULTED. CAPTAIN`S EMERGENCY FLASHLIGHT INDICATES RED WHEN PRESS TO TEST TO SEE IF FLASHLIGHT WORKS. TRANSFER TO DMI 247439 PER MEL 25-64-02C CAT C. - [SDR UIEA2026010200002](https://openairdocs.org/sdr/UIEA2026010200002), Jan 2, 2026: MEDICAL KIT. DAMAGED. MED KIT UNUSABLE, COULD NOT REMOVE THE TAMPER SEAL(

R/R MED KIT REF AMM 25-64-50/201. NO FURTHER DEFECTS NOTED. CLOSED DMI 245220

) - [SDR UIEA2025121601347](https://openairdocs.org/sdr/UIEA2025121601347), Dec 16, 2025: GIRT BAR. FOD. L1 DOOR WILL NOT ARM WITH NORMAL ARMING PROCEDURES. FOUND DEBRIS IN THE GIRT BAR AFTER FLOOR FITTING. CLEANED & ARMING SYSTEM OPS CHECKS GOOD IAW AMM 52-11-00-7 - [SDR UIEA2025082801146](https://openairdocs.org/sdr/UIEA2025082801146), Aug 28, 2025: OXYGEN SYSTEM. NO DISCREPANCY. 3RD SEAT OXYGEN TEST DOES NOT SHOW FULL CROSS. TOOK OUT MASK AND TESTED OXYGEN THROUGH MASK. PUT MASK BACK IN BOX AND TESTED IT, OPS CHECK GOOD PER AMM 35-00-00 - [SDR UIEA2025080201078](https://openairdocs.org/sdr/UIEA2025080201078), Aug 2, 2025: LIFE VEST. MISSING. DURING DAILY CHK, W/C C-06-001-01-08 FOUND LIFE VEST MISSING AT PAX SEAT BY R1 DOOR. INSTALLED NEW LIFE VEST AS REQUIRED AT PAX SEAT BY R1 DOOR REF W/C C-06-001 - [SDR UIEA2025072301007](https://openairdocs.org/sdr/UIEA2025072301007), Jul 23, 2025: CONTAINER. TORN. SUPERNUMERY LIFE PRESERVER BAG RIPPED OPEN. REPLACED FO SUPERNUMERY FLOTATION DEVICE PER AMM 25-62-01. MDDR 234719 CLEARED. PLACARD REMOVED. NO FURTHER DEFECTS - [SDR UIEA2025070800867](https://openairdocs.org/sdr/UIEA2025070800867), Jul 8, 2025: OXYGEN MASK. OBSTRUCTED. SAFETY HAZARD OXYGEN MASK OBSTRUCTED BY GPS CABLE, O2 IS UNUSABLE.(

ROUTED CABLE PER EO 7746A003. DOES NOT OBSTRUCT O2 MASK. NO FURTHER DEFECTS NOTED.

) - [SDR UIEA2025061400775](https://openairdocs.org/sdr/UIEA2025061400775), Jun 15, 2025: FLASHLIGHT ASSY. NO TEST. DURING PREFLIGHT CHECK PORTABLE FLASHLIGHT HOLDER DOES NOT TEST WITH TEST BUTTON BY L1 DOOR. REMOVED AND REPLACED FLASHLIGHT EMERGENCY ASSY IAW AMM 25-64-01. OP - [SDR UIEA2025051800630](https://openairdocs.org/sdr/UIEA2025051800630), May 18, 2025: OXYGEN BOTTLE. LEAKING. CREW O2 LOW.(

FOUND UPPER CREW O2 BOTTLE READING 500 PSI AND LEAKING FROM S/O VALVE. REMOVED AND REPLACED UPPER CREW O2 CYLINDER IAW AMM 12-15-08-900-801 REV - [SDR UIEA2025032400383](https://openairdocs.org/sdr/UIEA2025032400383), Mar 19, 2025: OXYGEN BOX. NO TEST. FIRST OBSERVER MASK STOWAGE BOX FAILS TO TEST. R & R OBS O2 MASK STOWAGE ASSY PER AMM 35-11-18-52. OPS CHK GOOD. DMI 227712 CLOSED. - [SDR UIEA2024070980599](https://openairdocs.org/sdr/UIEA2024070980599), Jul 6, 2024: NONE. NONE. DEVIATION FOUND DURING PERFORMING SB 777-57A0122 MODIFICATION.(

REMOVE DAMAGE PARTS I.A.W. SRM 51-40-02-0G-0, REV47. PERFORM EI NO T2024A57M-1552 REV 0.  - [SDR UIEA2024041100269](https://openairdocs.org/sdr/UIEA2024041100269), Apr 10, 2024: SLIDE. OPEN. ENTRY L1 DOOR OPENED WHILE STILL ARMED. SLIDE DID NOT DEPLOY(

CHKD FOUND DOOR SLIDE DISABLED. SUBSEQUENTLY DOOR SLIDE REMOVED AND ROUTED TO STORES. L1 DOOR ST - [SDR P5CA2024020100003](https://openairdocs.org/sdr/P5CA2024020100003), Feb 1, 2024: BATTERY. NO TEST. FD EMERGENCY LIGHT OPS CHECK FAILED(

R/R FO EMERGENCY FLASHLIGHT ASSY IAW B777 AMM 25-64-01 & 20-11-00. OPS CHECK GOOD. P/N P2-07-0015-003

) - [SDR P5CA2023112800116](https://openairdocs.org/sdr/P5CA2023112800116), Nov 28, 2023: UNKNOWN. UNKNOWN. CENTER OBS SEAT SHOULDER HARNESS RETRACTION IS WEAK.(

PFMD OPS CHK ON FIRST OBSERVER SEAT SHOULDER HARNESS, OPS CHK SATIS IAW AMM 25-11-03.

) - [SDR P5CA2023092200107](https://openairdocs.org/sdr/P5CA2023092200107), Sep 22, 2023: LIFE VEST. UNKNOWN. #3 SUPER SEAT LIFE VEST DAMAGED(

REPLACED WITH SVC LIFE VEST PER AMM 25-64-01. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2023092200106](https://openairdocs.org/sdr/P5CA2023092200106), Sep 22, 2023: LIFE VEST. UNKNOWN. SUPER SEAT #1 LIFE VEST DAMAGED(

REPLACED WITH SVC LIFE VEST PER AMM 25-64-01. NO FURTHER DEFECTS NOTED

) - [SDR P5CA2023071900036](https://openairdocs.org/sdr/P5CA2023071900036), Jul 18, 2023: BATTERY. UNKNOWN. BOTH FLASH LIGHTS IN FLIGHT DECK DO NOT TEST(

FLT DECK FLASHLIGHT BATTERIES REPLACED PER AMM 25-64-01 & TEST OK

/

P/N OFF: P2-07-0021-002  S/N - [SDR P5CA2023011300002](https://openairdocs.org/sdr/P5CA2023011300002), Jan 11, 2023: STOWAGE BOX. NO TEST. ON CHK, FND 1ST OBS OXY MASK UNABLE TO TEST.(

1ST OBS OXY MASK STOWAGE BOX REPLACED AND TEST "SATIS" IAW AMM 35-11-18

) - [SDR P5CA2022093000188](https://openairdocs.org/sdr/P5CA2022093000188), Sep 29, 2022: SIGN. DETACHED. EXIT SIGN AT L1 DOOR BROKE OFF.(

CHECKED AND DEFERRED AFT EMERGENCY LT DOOR 1L LENS BROKEN IAW MEL 33-51-01 CAT C DUE TO 09OCT22, PLACARD INSTALLED. MCC NOTIF - [SDR UIEA2022010400004](https://openairdocs.org/sdr/UIEA2022010400004), Jan 2, 2022: FLASHLIGHT. NONE. F/O FLASHLIGHT FOUND BROKEN(

REMOVED AND REPLACED F/O FLASHLIGHT IAW B777 AMM 25-60-10. OPS CHK GOOD.

) - [SDR Q2SA202001132424](https://openairdocs.org/sdr/Q2SA202001132424), Jan 12, 2020: LIGHT. INOPERATIVE. AIRCRAFT GROUNDED. EXTERNAL EMER LIGHTS NOT WORKING AT DOORS 1R AND 1L. EXTERNAL EMERGENCY LIGHT BULBS REPLACED AND TEST OK IAW AMM 33-51-04-960-801. - [SDR Q2SA2019060531422](https://openairdocs.org/sdr/Q2SA2019060531422), May 31, 2019: SKIN. SCRATCHED. AIRCRAFT GROUNDED. SCRATCH APPROX 24" LONG @ FUSELAGE STATION 1874-1895 SECTION 47 FROM STR 49L TO 46R. DAMAGE REPAIRED AS PER BOEING MESSAGE TLS-SOF-19-0015-02 - [SDR Q2SA20181229396](https://openairdocs.org/sdr/Q2SA20181229396), Dec 29, 2018: LIGHT. INOPERATIVE. AIRCRAFT GROUNDED. EXTERNAL EMERGENCY LIGHT DOOR L-1 INOP. SLIDE LOWER WING EMERGENCY LIGHT BULB DOOR L-1 REPLACED IAW AMM 33-51-01 960-801. TEST OK. ## STCs that may be installed (OpenAirDocs) None matched to this aircraft's models. ## Related - Other Boeing 777F16 aircraft: https://openairdocs.org/model/boeing-777f16/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.