# N661GT: 2018 Gulfstream Aerospace GVI (G650ER) - Status: Valid registration - Airframe: [Gulfstream Aerospace GVI (G650ER)](https://openairdocs.org/model/gulfstream-aerospace-gvi-g650er) (registry code 3980050, 22 seats) - Engine: [Rolls-Royce Deutschland BR700-725A112](https://openairdocs.org/engine/rolls-royce-deutschland-br700-725a112) (registry code 54231) - Data sheets: [TCDS T00015AT](https://openairdocs.org/tcds/T00015AT) (Gulfstream Aerospace Corporation), [TCDS E00057EN](https://openairdocs.org/tcds/E00057EN) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs) - Serial number: 6364 - Year built: 2018 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: December 7, 2018 - Certificate issued: June 20, 2019 - Expires: June 30, 2029 - Mode S code: A8B898 - Registered owner: [Rhys Vineyards LLC](https://openairdocs.org/faa-owner/RHYS%20VINEYARDS%20LLC) - Location: [San Jose, CA](https://openairdocs.org/faa-place/CA/San%20Jose) - Owner type: LLC - Owner's area on the map: 37.3466° N, 121.9097° W: Placed by OpenAirDocs at the center of ZIP code 95110, 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=661GT - Page: https://openairdocs.org/aircraft/N661GT 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): 13 in force ### Matched by airframe (Gulfstream Aerospace GVI (G650ER)) - [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026 - [AD 2026-01-02](https://openairdocs.org/ad/2026-01-02): Wings · Gulfstream Aerospace GVI. Effective Feb 24, 2026 - [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023 - [AD 2020-11-01](https://openairdocs.org/ad/2020-11-01): Flight Controls · Gulfstream Aerospace GVI. Effective Jul 27, 2020 - [AD 2020-02-18](https://openairdocs.org/ad/2020-02-18): Flight Controls · Gulfstream Aerospace GVI, GVII-G500 and GVII-G600. Effective Feb 13, 2020 - [AD 2019-23-11](https://openairdocs.org/ad/2019-23-11): Flight Controls · Gulfstream Aerospace GVI. Effective Dec 30, 2019 - [AD 2018-20-04](https://openairdocs.org/ad/2018-20-04): Flight Controls · Gulfstream Aerospace GVI. Effective Oct 15, 2018 - [AD 2018-12-07](https://openairdocs.org/ad/2018-12-07): Landing Gear · Gulfstream Aerospace GVI. Effective Jul 23, 2018 - [AD 2017-20-08](https://openairdocs.org/ad/2017-20-08): Airborne Auxiliary Power and Fuselage · Gulfstream Aerospace G-IV, GIV-X, GV and 2 more. Effective Nov 6, 2017 - [AD 2017-04-01](https://openairdocs.org/ad/2017-04-01): Flight controls · Gulfstream Aerospace GVI. Effective Mar 28, 2017 - [AD 2015-20-10](https://openairdocs.org/ad/2015-20-10): Pneumatic · Gulfstream Aerospace GVI. Effective Nov 13, 2015 ### Matched by engine (Rolls-Royce Deutschland BR700-725A112) - [AD 2014-12-03](https://openairdocs.org/ad/2014-12-03): Fuel metering units (FMUs) · Rolls-Royce Deutschland BR700-725A1-12. Effective Jul 17, 2014 - [AD 2013-12-03](https://openairdocs.org/ad/2013-12-03): Fuel pump tube · Rolls-Royce Deutschland BR700-725A1-12. Effective Jun 14, 2013 ### Historical (superseded or no longer in force) - [AD 2015-24-06](https://openairdocs.org/ad/2015-24-06) (historical): Landing gear · Gulfstream Aerospace GVI. Effective Dec 4, 2015 ## Information bulletins (advisory) (2 in force) - [SAIB CE-19-20](https://openairdocs.org/saib/CE-19-20): Flight Compartment Windows. Issued Dec 5, 2019 - [SAIB NM-13-25](https://openairdocs.org/saib/NM-13-25): Landing Gear: Nose Wheel Steering. Issued Mar 22, 2013 ## NTSB investigations None matched to N661GT. ## FAA accident and incident reports None matched to N661GT. ## Service difficulty reports None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. ## Service difficulty reports on N661GT not matched to an aircraft (153, newest 50) They name N661GT, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR UIEA201805160469](https://openairdocs.org/sdr/UIEA201805160469), May 11, 2018: RUB STRIP. CORRODED. NR 2 ENGINE, RT CORE COWL EXTERIOR SURFACE FWD UPPER WEAR STRIP FOUND CORRODED. THE WEAR STRIPS WAS REMOVED AND REPLACED IAW SRM 51-40-02 REV 106. - [SDR UIEA201805160470](https://openairdocs.org/sdr/UIEA201805160470), May 11, 2018: RUB STRIP. WORN. NR 2 ENGINE, RT CORE COWL UPPER AFT EDGE WEAR STRIP FOUND WORN. THE WEAR STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160471](https://openairdocs.org/sdr/UIEA201805160471), May 11, 2018: SEAL. TORN. NR 2 ENGINE, LT CORE COWL UPPER FWD EDGE SEAL FOUND TORN. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160472](https://openairdocs.org/sdr/UIEA201805160472), May 11, 2018: SHIM. TORN. NR 1 ENGINE, RT CORE COWL MID & AFT HINGE ASSY ATTACH SHIMS FOUND TORN. THE SHIMS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160474](https://openairdocs.org/sdr/UIEA201805160474), May 11, 2018: SHIM. TORN. NR 2 ENGINE, LT CORE COWL MID & AFT HINGE ASSY ATTACH SHIMS FOUND TORN. THE SHIMS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160494](https://openairdocs.org/sdr/UIEA201805160494), May 11, 2018: RUB STRIP. WORN. NR 2 ENGINE, RT CORE COWL FAIRING ASSY INTERIOR SURFACE AFT UPPER EDGE RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED SRM 51-40-02, REV 106. - [SDR UIEA201805160497](https://openairdocs.org/sdr/UIEA201805160497), May 11, 2018: RUB STRIP. WORN. NR 1 ENGINE, RT CORE COWL FAIRING ASSY INTERIOR SURFACE AFT UPPER EDGE RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160498](https://openairdocs.org/sdr/UIEA201805160498), May 11, 2018: RUB STRIP. WORN. NR 1 ENGINE. LT CORE COWL FAIRING ASSY, INTERIOR SURFACE AFT UPPER AFT EDGE RUB STRIP FOUND WORN. THE RUB STRIP WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 1 - [SDR UIEA201805160499](https://openairdocs.org/sdr/UIEA201805160499), May 11, 2018: RIVET. DAMAGED. NR 1 ENGINE, RT CORE COWL UPPER AFT EDGE WEAR STRIP ATTACH RIVETS FOUND DAMAGED. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160500](https://openairdocs.org/sdr/UIEA201805160500), May 11, 2018: RIVET. DAMAGED. NR 2 ENGINE, LT CORE COWL UPPER AFT EDGE WEAR STRIP ATTACH RIVETS FOUND DAMAGED. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160501](https://openairdocs.org/sdr/UIEA201805160501), May 11, 2018: SEAL. CRACKED. NR 1 ENGINE, RT CORE COWL FAIRING ASSY UPPER EDGE AFT STRIP SEAL FOUND CRACKED. THE FAIRING ASSY SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160503](https://openairdocs.org/sdr/UIEA201805160503), May 11, 2018: FASTENER. CORRODED. NR 2 ENGINE, RT CORE COWL INTERIOR SURFACE AFT SHEAR PLATE ATTACH FASTENERS FOUND RUSTY. THE FASTENERS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160502](https://openairdocs.org/sdr/UIEA201805160502), May 11, 2018: SEAL. CRACKED. NR 1 ENGINE, LT CORE COWL FAIRING ASSY. UPPER EDGE AFT STRIP SEAL FOUND CRACKED. THE SEAL WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160504](https://openairdocs.org/sdr/UIEA201805160504), May 11, 2018: FASTENER. CORRODED. NR 2 ENGINE, RT CORE COWL MID AND AFT HINGE ATTACH FASTENERS FOUND RUSTY. THE FASTENERS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160505](https://openairdocs.org/sdr/UIEA201805160505), May 11, 2018: SKIN. DAMAGED. NR 1 ENGINE, LT CORE COWL FAIRING SKIN INTERIOR SURFACE AT THE UPPER AFT CUT-OUT SECTION FOUND DAMAGED. THE FAIRING SKIN WAS REPAIRED IAW SRM 54-45-01, REPAIR 1 - [SDR UIEA201805160506](https://openairdocs.org/sdr/UIEA201805160506), May 11, 2018: SKIN. DAMAGED. NR 2 ENGINE, RT CORE COWL FAIRING SKIN INTERIOR SURFACE ON THE UPPER AFT CUT-OUT SECTION FOUND DAMAGED. THE FAIRING SKIN WAS REPAIRED IAW SRM 54-45-01, REPAIR 1 - [SDR UIEA201805160636](https://openairdocs.org/sdr/UIEA201805160636), May 11, 2018: ADAPTER. WORN. NR 1 ENGINE, RT CORE COWL HOLD OPEN ROD STOW PIN ADAPTER WAS FOUND WORN. THE ADAPTER WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160637](https://openairdocs.org/sdr/UIEA201805160637), May 11, 2018: ADAPTER. WORN. NR 2 ENGINE, RT CORE COWL HOLD OPEN ROD STOW PIN ADAPTER FOUND WORN. THE ADAPTER WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160638](https://openairdocs.org/sdr/UIEA201805160638), May 11, 2018: BRACKET. WORN. NR 2 ENGINE, LT CORE COWL HOLD OPEN ROD STOW PIN BRACKET FOUND WORN. THE BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160639](https://openairdocs.org/sdr/UIEA201805160639), May 11, 2018: ADAPTER. WORN. NR 1 ENGINE, LT CORE COWL HOLD OPEN ROD STOW PIN ADAPTER FOUND WORN. THE ADAPTER WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160640](https://openairdocs.org/sdr/UIEA201805160640), May 11, 2018: STRUCTURE. DAMAGED. NR 1 ENGINE, RT CORE COWL PRESSURE RELIEF DOOR CUTOUT HINGE BUSHINGS HOLE FOUND ELONGATED. THE BUSHING WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160641](https://openairdocs.org/sdr/UIEA201805160641), May 11, 2018: ATTACH BRACKET. WORN. NR 1 ENGINE, RT CORE COWL PRESSURE RELIEF DOOR CUTOUT LATCH ATTACH BRACKET FOUND WORN. THE ATTACH BRACKET WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160662](https://openairdocs.org/sdr/UIEA201805160662), May 11, 2018: BRACKET. WORN. NR 1 ENGINE, LT FAN COWL FWD HOLD OPEN ROD STOW BRACKET FOUND WORN. REMOVED AND REPLACED THE STOW BRACKET IAW AMM 70-50-00, REV 123. - [SDR UIEA201805160684](https://openairdocs.org/sdr/UIEA201805160684), May 11, 2018: SKIN. SCRATCHED. NR 1 ENGINE, LT CORE COWL SKIN EXTERIOR SURFACES FOUND SCRATCHED. THE SCRATCHES WERE REMOVED AND FOUND WITHIN LIMITS IAW SRM 54-45-01-1A-1, FIG 101, TABLE 101, - [SDR UIEA201805160663](https://openairdocs.org/sdr/UIEA201805160663), May 11, 2018: LUG. DAMAGED. NR 2 ENGINE, RT CORE COWL PRESSURE RELIEF DOOR LANYARD LUG ATTACH HOLES FOUND ELONGATED. THE PRESSURE RELIEF DOOR WAS REMOVED AND REPLACED IAW AMM 71-11-09, REV - [SDR UIEA2018050160664](https://openairdocs.org/sdr/UIEA2018050160664), May 11, 2018: STRUCTURE. WORN. NR 2 ENGINE, LT CORE COWL HOLD OPEN ROD WELD ASSY FOUND WORN. REMOVED AND REPLACED THE HOLD OPEN ROD WELD ASSY IAW AMM 70-50-00, REV 123. - [SDR UIEA201805160666](https://openairdocs.org/sdr/UIEA201805160666), May 11, 2018: BRACKET. WORN. NR 2 ENGINE, RT FAN COWL FWD HOLD OPEN ROD STOW BRACKET FOUND WORN. REMOVED AND REPLACED THE STOW BRACKET IAW AMM 70-50-00, REV 123. - [SDR UIEA201805160667](https://openairdocs.org/sdr/UIEA201805160667), May 11, 2018: BRACKET. WORN. NR 2 ENGINE, LT FAN COWL FWD HOLD OPEN ROD STOW BRACKET FOUND WORN. REMOVED AND REPLACED THE STOW BRACKET IAW AMM 70-50-00, REV 123. - [SDR UIEA201805160668](https://openairdocs.org/sdr/UIEA201805160668), May 11, 2018: BRACKET. WORN. NR 1 ENGINE, LT CORE COWL HOLD OPEN ROD WELD BRACKET FOUND WORN. REMOVED AND REPLACED THE BRACKET IAW AMM 70-50-00, REV 123. - [SDR UIEA201805160669](https://openairdocs.org/sdr/UIEA201805160669), May 11, 2018: ROD. WORN. NR 2 ENGINE, RT CORE COWL HOLD OPEN ROD WELD ASSY FOUND WORN. REMOVED AND REPLACED ROD WELD ASSY IAW AMM 70-50-00, REV 123. - [SDR UIEA201805160670](https://openairdocs.org/sdr/UIEA201805160670), May 11, 2018: ADAPTER. WORN. NR 2 ENGINE, LT CORE COWL HOLD OPEN ROD STOW ADAPTER FOUND FOUND WORN. REMOVED AND REPLACED THE STOW ADAPTER IAW AMM 70-50-00, REV 123. - [SDR UIEA201805160671](https://openairdocs.org/sdr/UIEA201805160671), May 11, 2018: ADAPTER. WORN. NR 2 ENGINE, RT CORE COWL HOLD OPEN ROD STOW ADAPTER FOUND WORN. REMOVED AND REPLACED THE STOW ADAPTER IAW AMM 70-50-00 REV 123. - [SDR UIEA201805160672](https://openairdocs.org/sdr/UIEA201805160672), May 11, 2018: ADAPTER. WORN. NR 1 ENGINE, LT CORE COWL HOLD OPEN ROD STOW ADAPTER FOUND WORN. REMOVED AND REPLACED THE HOLD OPEN ROD STOW ADAPTER IAW AMM 70-50-00, REV 123. - [SDR UIEA201805160673](https://openairdocs.org/sdr/UIEA201805160673), May 11, 2018: ADAPTER. WORN. NR 1 ENGINE, RT CORE COWL HOLD OPEN ROD STOW ADAPTER FOUND WORN. REMOVED AND REPLACED THE HOLD OPEN ROD STOW ADAPTER IAW AMM 70-50-00, REV 123. - [SDR UIEA201805160675](https://openairdocs.org/sdr/UIEA201805160675), May 11, 2018: BRACKET. WORN. NR 2 ENGINE, RT CORE COWL PRESSURE RELIEF DOOR CUTOUT LATCH ATTACH BRACKETS FOUND WORN. THE BRACKETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160674](https://openairdocs.org/sdr/UIEA201805160674), May 11, 2018: NUT. LOOSE. NR 2 ENGINE, RT CORE COWL HOLD OPEN ROD JAM NUT FOUND LOOSE. THE NUT WAS TIGHTEN IAW AMM 70-50-00, REV 123. - [SDR UIEA201805160676](https://openairdocs.org/sdr/UIEA201805160676), May 11, 2018: SUPPORT PLATE. WORN. NR 2 ENGINE, RT CORE COWL HOLD OPEN ROD END SUPPORT PLATE FOUND WORN. THE SUPPORT PLATE WAS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA20180516 0677](https://openairdocs.org/sdr/UIEA20180516%200677), May 11, 2018: RIVET. DAMAGED. NR 1 ENGINE, LT CORE COWL EXTERIOR SURFACE FWD LOWER WEAR STRIPS ATTACH RIVETS FOUND DAMAGED. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA201805160685](https://openairdocs.org/sdr/UIEA201805160685), May 11, 2018: SKIN. SCRATCHED. NR 1 ENGINE, R CORE COWL SKIN EXTERIOR SURFACES SCRATCHED. SCRATCHES REMOVED AND FOUND WITHIN LIMITS IAW SRM 54-45-01-1A-1, FIG 101, TABLE 101, DETAIL II, REV 1 - [SDR UIEA201805160686](https://openairdocs.org/sdr/UIEA201805160686), May 11, 2018: SKIN. SCRATCHED. NR 2 ENGINE, LT CORE COWL SKIN EXTERIOR SURFACES FOUND SCRATCHED. SCRATCHES REMOVED AND FOUND WITHIN LIMITS IAW SRM 54-45-01-1A-1, FIG 101, TABLE 101, DETAIL II - [SDR UIEA201805160688](https://openairdocs.org/sdr/UIEA201805160688), May 11, 2018: SKIN. SCRATCHED. NR 2 ENGINE, RT CORE COWL SKIN EXTERIOR SURFACES FOUND SCRATCHES. SCRATCHES REMOVED AND FOUND WITHIN LIMITS IAW SRM 54-45-01-1A-1, FIG 101, TABLE 101, DETAIL II - [SDR UIEA201804160690](https://openairdocs.org/sdr/UIEA201804160690), May 11, 2018: CHANNEL. WORN. NR 2 ENGINE, RT CORE COWL FAIRING ASSY, INTERIOR SURFACE UPPER AFT CHANNEL FOUND WORN ADJACENT TO MID HINGE SECTION. REMOVED AND REPLACED IAW SRM 51-40-02, REV - [SDR UIEA2018041600706](https://openairdocs.org/sdr/UIEA2018041600706), May 11, 2018: ROD. WORN. NR 1 ENGINE, RT CORE COWL HOLD OPEN ROD WELD ASSY FOUND WORN. REMOVED AND REPLACED IAW AMM 70-50-00, REV 123. - [SDR UIEA201805160708](https://openairdocs.org/sdr/UIEA201805160708), May 11, 2018: STOP. WORN. NR 2 ENGINE, RT CORE COWL FAIRING ASSY, INTERIOR SURFACE UPPER FAIRING DOORS STOPS FOUND WORN. WORN STOPS REMOVED AND REPLACED IAW SRM 51-40-02, REV 106. - [SDR UIEA2018041600709](https://openairdocs.org/sdr/UIEA2018041600709), May 11, 2018: RIVET. SHEARED. NR 2 ENGINE, R/H CORE COWL DATA SUPPORT PLATE ATTACH RIVETS FOUND SHEARED. THE RIVETS WERE REMOVED AND REPLACED IAW SRM 51-40-02. REV 106. - [SDR UIEA201805160718](https://openairdocs.org/sdr/UIEA201805160718), May 11, 2018: DUCT. WORN. NR 1 ENGINE, RT CORE COWL PRECOOLER EXIT DUCT LIP FOUND WORN. WELD REPAIRED IAW 090238, REV A . - [SDR UIEA201805160728](https://openairdocs.org/sdr/UIEA201805160728), May 11, 2018: DUCT. WORN. NR 2 ENGINE, RT CORE COWL PRECOOLER EXIT DUCT LIP FOUND WORN. WELDING REPAIR CARRIED OUT IAW 090238, REV A . - [SDR UIEA201805160736](https://openairdocs.org/sdr/UIEA201805160736), May 11, 2018: FRAME. WORN. NR 2 ENGINE, RT CORE COWL SECOND ZEE FRAME EXISTING DOUBLER PLATE FOUND WORN NEAR PRESSURE RELIEF DOOR. THE FRAME WAS REMOVED AND REPLACED IAW SRM 51-40-02. REV - [SDR UIEA2018042300760](https://openairdocs.org/sdr/UIEA2018042300760), May 11, 2018: SKIN. DENTED. NR 1 ENGINE, RT FAN COWL OUTER SKIN FOUND DENTED. REPAIRED IAW SRM 54-25-01, REPAIR 1, REV 106. - [SDR UIEA2018042300761](https://openairdocs.org/sdr/UIEA2018042300761), May 11, 2018: SKIN. DENTED. NR 1 ENGINE, RT FAN COWL OUTER SKIN FOUND DENTED. REPAIRED IAW SRM 54-25-01, REPAIR 1, REV 106. All 153: https://openairdocs.org/aircraft/N661GT/unmatched-reports.md ## STCs that may be installed (OpenAirDocs) (37) Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do. ### Approved for the airframe (Gulfstream Aerospace GVI (G650ER)) - [STC ST04603CH](https://openairdocs.org/stc/ST04603CH): Installation of SpaceX Starlink Aviation System. Nextant Aerospace - [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc - [STC ST11969AT](https://openairdocs.org/stc/ST11969AT): Installation of Gogo Galileo HDX System. Gulfstream Aerospace Corporation - [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc - [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde Inc - [STC ST04347AT-D](https://openairdocs.org/stc/ST04347AT-D): Installation of Satcom Direct Plane Simple System. Gulfstream Aerospace Corporation - [STC ST12147IB](https://openairdocs.org/stc/ST12147IB): Installation of VVIP Interior Completion. Jet Aviation AG - [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc - [STC ST04649NY](https://openairdocs.org/stc/ST04649NY): Installation of Avionic Instruments Frequency Converters. Kilroy Aviation LLC - [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc - [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine - [STC ST04541AT](https://openairdocs.org/stc/ST04541AT): Installation of an Airplane Medevac Interior. Gulfstream Aerospace Corporation - [STC ST04540AT](https://openairdocs.org/stc/ST04540AT): Installation of SpaceX Starlink Aviation System. Gulfstream Aerospace Corporation - [STC ST04348AT-D](https://openairdocs.org/stc/ST04348AT-D): Installation of Honeywell AIS-2000 High Definition (HD) Upgrade. Gulfstream Aerospace Corporation - [STC ST00126IB](https://openairdocs.org/stc/ST00126IB): Replacement of Halon agent with alternate Halon-free Portable Fire Extinguisher agent. AMAC Aerospace Switzerland AG - [STC ST00105IB](https://openairdocs.org/stc/ST00105IB): Introduction of Activation of Wireless Charging Systems for Portable Electronic Devices. AMAC AEROSPACE SWITZERLAND AG - [STC ST04787NY](https://openairdocs.org/stc/ST04787NY): Installation of True Blue Power TFC4000 AC-to-AC Converter. Sterling Helicopter - [STC ST04252AT-D](https://openairdocs.org/stc/ST04252AT-D): Installation of an Airplane Interior. Gulfstream Aerospace Corporation - [STC ST04101NY](https://openairdocs.org/stc/ST04101NY): Installation of a Honeywell Go-Direct Router. Delta Engineering Corporation - [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc - [STC ST04339AT-D](https://openairdocs.org/stc/ST04339AT-D): Installation of Air Ionizer System. Gulfstream Aerospace Corporation - [STC ST04319AT-D](https://openairdocs.org/stc/ST04319AT-D): Installation of Satcom Direct Gateway (SDR-G) System. Gulfstream Aerospace Corporation - [STC ST04334AT-D](https://openairdocs.org/stc/ST04334AT-D): Installation of Viasat Ka-Broadband High Speed Data System. Gulfstream Aerospace Corporation - [STC ST02672LA](https://openairdocs.org/stc/ST02672LA): Installation of Honeywell DU-1310-2 Display Unit in accordance. Honeywell International Inc - [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS - [STC ST04320AT-D](https://openairdocs.org/stc/ST04320AT-D): Installation of ViaSat Ka Broadband High Speed Data System. Gulfstream Aerospace Corporation - [STC ST04440AT](https://openairdocs.org/stc/ST04440AT): Installation of Aviation Clean Air Ionization Units in cold air supply Duct/ECS system. Southern Aviation Parts and Services - [STC ST00391BO](https://openairdocs.org/stc/ST00391BO): Installation of a Honeywell CNX-900 Cabin Network Accelerator and PED tolerance certification. Pro Star Aviation LLC - [STC ST04309AT-D](https://openairdocs.org/stc/ST04309AT-D): Installation of Iridium SATCOM System (FANS-1/A+Over Iridium). Gulfstream Aerospace Corporation - [STC ST04306AT-D](https://openairdocs.org/stc/ST04306AT-D): Installation of Tailwind 500 Satellite TV System. Gulfstream Aerospace Corporation - [STC ST11071SC](https://openairdocs.org/stc/ST11071SC): Demonstration of aircraft critical equipment and antenna systems tolerance of radio frequency interference (RFI) from intentional or spurious transmissions from certain Portable Electronic Devices (PEDs). Liberty Partners Inc - [STC ST03776NY](https://openairdocs.org/stc/ST03776NY): Modification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II). Scandinavian Avionics Design ApS - [STC ST04028AT-D](https://openairdocs.org/stc/ST04028AT-D): Installation of a TrueNorth Iridium Telephone/WLAN System. Gulfstream Aerospace Corporation - [STC ST04027AT-D](https://openairdocs.org/stc/ST04027AT-D): Installation of Satcom Direct Router (SDR). Gulfstream Aerospace Corporation - [STC ST04254AT-D](https://openairdocs.org/stc/ST04254AT-D): Installation of Broadband Multi-Link (BBML) System. Gulfstream Aerospace Corporation - [STC ST04277AT-D](https://openairdocs.org/stc/ST04277AT-D): Installation of a Honeywell LSZ-860 Lightning Sensor System. Gulfstream Aerospace Corporation - [STC ST04253AT-D](https://openairdocs.org/stc/ST04253AT-D): Installation of a Honeywell AIS-2000 Satellite TV System. Gulfstream Aerospace Corporation ## Related - Other Gulfstream Aerospace GVI (G650ER) aircraft: https://openairdocs.org/model/gulfstream-aerospace-gvi-g650er/aircraft.md - The Rolls-Royce Deutschland BR700-725A112 engine: https://openairdocs.org/engine/rolls-royce-deutschland-br700-725a112.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.