# N5116: 2026 Gulfstream Aerospace GVII-G600 - Status: Valid registration - Airframe: [Gulfstream Aerospace GVII-G600](https://openairdocs.org/model/gulfstream-aerospace-gvii-g600) (registry code 3980219, 9 seats) - Engine: [Pratt & Whitney Canada PW815GA](https://openairdocs.org/engine/pratt-whitney-canada-pw815ga) (registry code 52376) - Data sheets: [TCDS T00021AT](https://openairdocs.org/tcds/T00021AT) (Gulfstream Aerospace Corporation), [TCDS E00093EN](https://openairdocs.org/tcds/E00093EN) (Pratt & Whitney Canada Corp.) (OpenAirDocs) - Serial number: 73215 - Year built: 2026 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: April 21, 2026 - Certificate issued: September 25, 2026 - Expires: September 30, 2033 - Mode S code: A66850 - Registered owner: [N5116 LLC](https://openairdocs.org/faa-owner/N5116%20LLC) - Location: [Kansas City, MO](https://openairdocs.org/faa-place/MO/Kansas%20City) - Owner type: LLC - Owner's area on the map: 39.1061° N, 94.5903° W: Placed by OpenAirDocs at the center of ZIP code 64105, 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=5116 - Page: https://openairdocs.org/aircraft/N5116 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): 10 in force ### Matched by airframe (Gulfstream Aerospace GVII-G600) - [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 2026-01-03](https://openairdocs.org/ad/2026-01-03): Main Landing Gear · Gulfstream Aerospace GVII-G500 and GVII-G600. Effective Feb 24, 2026 - [AD 2024-25-03](https://openairdocs.org/ad/2024-25-03): Fuel · Gulfstream Aerospace GVII-G500 and GVII-G600. Effective Feb 12, 2025 - [AD 2024-10-15](https://openairdocs.org/ad/2024-10-15): Powerplant · Gulfstream Aerospace GVII-G500 and GVII-G600. Effective Jun 7, 2024 - [AD 2024-05-04](https://openairdocs.org/ad/2024-05-04): Fuel Boost Pump · Gulfstream Aerospace GVII-G500 and GVII-G600. Effective May 2, 2024 - [AD 2023-14-08](https://openairdocs.org/ad/2023-14-08): Flight Controls · Gulfstream Aerospace GVII-G600. Effective Aug 24, 2023 - [AD 2023-11-09](https://openairdocs.org/ad/2023-11-09): Flight controls · Gulfstream Aerospace GVII-G500 and GVII-G600. Effective Jul 18, 2023 - [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 2022-10-05](https://openairdocs.org/ad/2022-10-05): Flight controls · Gulfstream Aerospace GVII-G500 and GVII-G600. Effective May 9, 2022 - [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 ### Matched by engine (Pratt & Whitney Canada PW815GA) None in force. ### Historical (superseded or no longer in force) - [AD 2020-23-04](https://openairdocs.org/ad/2020-23-04) (historical): Fuel Boost Pump · Gulfstream Aerospace GVII-G500 and GVII-G600. Effective Nov 24, 2020 - [AD 2020-05-12](https://openairdocs.org/ad/2020-05-12) (historical): Flight controls · Gulfstream Aerospace GVII-G500 and GVII-G600. Effective Mar 13, 2020 ## Information bulletins (advisory) None matched. ## NTSB investigations None matched to N5116. ## FAA accident and incident reports None matched to N5116. ## 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 N5116 not matched to an aircraft (15) They name N5116, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft. - [SDR UG8A08GM08181](https://openairdocs.org/sdr/UG8A08GM08181), Aug 20, 2008: BLEED VALVE. INOPERATIVE. THE "L-BLEED PRESSURE HIGH" AMBER CAS WAS NOTED ON TAKEOFF ROLL BEGINNING. LT ENG BLEED AIR PRESSURE REGULATING VALVE FAILED TO REGULATE PROPERLY. TROUBLESHOOTI - [SDR UG82004F00002](https://openairdocs.org/sdr/UG82004F00002), Mar 31, 2004: SMOKE DETECTOR. DIRTY. DURING DESCENT, BAGGAGE SMOKE LIGHT (EICAS) CAME ON. NO SMOKE OR FUMES DETECTED ON INSPECTION AFTER LANDING. BAGGAGE SMOKE DETECTOR FOUND TO BE VERY DIRTY. REMO - [SDR GM0409](https://openairdocs.org/sdr/GM0409), Mar 31, 2004: SMOKE DETECTOR. DIRTY. BAGGAGE SMOKE LIGHT(EICAS) CAME ON. NO SMOKE OR FUMES DETECTED ON INSPECTION AFT LANDING. BAGGAGE SMOKE DETECTER FOUND TO BE VERY DIRTY. INITATED A FLEET INSPEC - [SDR 2004F00088](https://openairdocs.org/sdr/2004F00088), Feb 2, 2004: ACTUATOR. INOPERATIVE. BLUE YAW DAMPER, FAIL LOWER 'B' CAS MESSAGE, AMBER YAW DAMPER OFF LOWER CAS MESSAGE AND PRI STAB TRIM FAIL AND MACH TRIM OFF CAS MESSAGE CAME ON DURING FLIGHT. - [SDR 2003F00511](https://openairdocs.org/sdr/2003F00511), Jun 20, 2003: STARTER. FAILED. RIGHT ENGINE REPORTED AS SMOKING BY TOWER AND OTHER AIRCRAFT DURING TAXI OUT. RIGHT ENGIEN STARTER FAILED TO DISENGAGE AFTER START. STARTER WAS REPLACED, SERVIC - [SDR 2003F00359](https://openairdocs.org/sdr/2003F00359), May 20, 2003: LIMITER. FAILED. DURING PILOT'S PREFLIGHT, WITH APU RUNNING, THE 'RUDDER LIMIT FAIL' RED CAS MESSAGE ANNUNCIATED. ANOTHER AIRCRAT WAS UTILIZED FOR THE TRIP. THE RUDDER LIMITER F - [SDR 2003F00227](https://openairdocs.org/sdr/2003F00227), Mar 1, 2003: BEARING. SEIZED. MAIN CABIN DOOR IS HARD TO OPEN FROM THE INSIDE. REPLACED AFT CABLE ASSEMBLY, SPRING PIVOT BEARINGS ANDLONG SHAFT. RIGGED THE DOOR PER CESSNA MM. OPERATIONAL CH - [SDR UG82002F00002](https://openairdocs.org/sdr/UG82002F00002), May 16, 2002: ENGINE. OUT OF TOLERANCE. RIGHT ENGINE OIL PRESSURE OUT OF LIMITS, HI/RED 106 PSI AT 80-90 KTS. ENGINE INTERNAL BEARING SEAL AIR LEAKAGE WHICH MAY OCCUR AS ENGINE APPROACHES ITS MIDLIFE - [SDR 2002F00984](https://openairdocs.org/sdr/2002F00984), Jan 23, 2002: PROXIMITY SWITCH. FAULTY. PSP - MAIN CABIN DOOR WARNING LIGHT WOULD NOT EXTINGUISHED WHEN CLOSED. FAULTY DOOR HANDLE PROXIMITY SWITCH. PROBLEM WAS CORRECTED BY REPLACEMENT OF THE SWITCH. - [SDR UG82001F00009](https://openairdocs.org/sdr/UG82001F00009), Oct 18, 2001: POWER UNIT. FAILED. VIBRATION FELT ON CABIN FLOOR AS WELL AS HUM. LT HYD (A) SYSTEM FLUCTUATED BETWEEN 2400-3300 PSI. WHEN GEAR WAS SELECTED DOWN LT HYD PRES WAS 2100 AND RT HAD AN - [SDR UG82001F00008](https://openairdocs.org/sdr/UG82001F00008), Oct 5, 2001: HYDRAULIC SYSTEM. MALFUNCTIONED. VIBRATION FELT ON CABIN FLOOR AS WELL AS HUM. LEFT HYDRAULIC (A) SYSTEM FLUCTUATED BETWEEN 2400-3300 PSI. WHEN GEAR WAS SELECTED DOWN LEFT HYDRAULIC PRESSURE WA - [SDR 2001F00330](https://openairdocs.org/sdr/2001F00330), Jul 27, 2001: O-RING. DAMAGED. IND - PILOT WALKAROUND PRIOR TO DEPARTURE, TWO HYD PUDDLES UNDER TAIL OF A/C. 'A' HYD SYSTEM INDICATES 25 PERCENT. APPEARS TO BE COMING FROM ELEVATOR. REPLACED - [SDR 2001F00336](https://openairdocs.org/sdr/2001F00336), Jul 22, 2001: SQUAT SWITCH. OUT OF ADJ. DTW - NOSE GEAR WOULD NOT RETRACT. ADJUSTED NOSE GEAR SQUAT SWITCH RAMP. (M) - [SDR 20010511CW013](https://openairdocs.org/sdr/20010511CW013), Apr 24, 2001: ALTERNATOR. FAILED. CREW STATED RIGHT HAND WINDSHIELD HEAT INOPERATIVE. TROUBLESHOT TO FAULTY LEFT HAND ALTERNATOR. UPON ALTERNATOR REMOVAL, NOTICED THAT THE COOLING FAN BLADES ON - [SDR 98ZZZX340](https://openairdocs.org/sdr/98ZZZX340), Dec 1, 1997: STRUT. MALFUNCTION. THE AIRCRAFT DEPARTED DTW AND ON CLIMB-OUT, THE LANDING GEAR HANDLE WOULD NOT MOVE TO THE RETRACT POSITION. THE AIRCRAFT RETURNED TO DTW AND MAINTENANCE WAS UNA ## STCs that may be installed (OpenAirDocs) (9) 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 GVII-G600) - [STC ST04570AT](https://openairdocs.org/stc/ST04570AT): Installation of SpaceX Starlink Aviation System. Gulfstream Aerospace Corporation - [STC ST04343AT-D](https://openairdocs.org/stc/ST04343AT-D): Installation of Air Ionization System. Gulfstream Aerospace Corporation - [STC ST04347AT-D](https://openairdocs.org/stc/ST04347AT-D): Installation of Satcom Direct Plane Simple System. Gulfstream Aerospace Corporation - [STC ST00105IB](https://openairdocs.org/stc/ST00105IB): Introduction of Activation of Wireless Charging Systems for Portable Electronic Devices. AMAC AEROSPACE SWITZERLAND AG - [STC ST04346AT-D](https://openairdocs.org/stc/ST04346AT-D): Installation of Satcom Direct Router (SDR) Databus Wire Harness. Gulfstream Aerospace Corporation - [STC ST04319AT-D](https://openairdocs.org/stc/ST04319AT-D): Installation of Satcom Direct Gateway (SDR-G) System. Gulfstream Aerospace Corporation - [STC ST04324AT-D](https://openairdocs.org/stc/ST04324AT-D): Installation of an Airplane Interior. Gulfstream Aerospace Corporation - [STC ST04325AT-D](https://openairdocs.org/stc/ST04325AT-D): Installation of Gogo AVANCE L5. Gulfstream Aerospace Corporation - [STC ST04326AT-D](https://openairdocs.org/stc/ST04326AT-D): lnstallation of Ka-Band Jetwave High Speed Data (HSD) System. Gulfstream Aerospace Corporation ## Related - Other Gulfstream Aerospace GVII-G600 aircraft: https://openairdocs.org/model/gulfstream-aerospace-gvii-g600/aircraft.md - The Pratt & Whitney Canada PW815GA engine: https://openairdocs.org/engine/pratt-whitney-canada-pw815ga.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.