- Registered owner
- 1111 Giv LLC
- Location
- Downey, CA
- Owner type
- LLC
- Serial number
- 1111
- Year built
- 1989
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 20, 1995
- Certificate issued
- March 2, 2024
- Expires
- March 31, 2031
- Mode S code
- A66608
Gulfstream Aerospace G-IVTCDS A12EAAirframe · Gulfstream Aerospace G-IVEngine modelRolls-Royce TAY-611SER
From the FAA registry file of October 20, 2026.
On this page
Airworthiness directives that may apply · 39
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1988 | 1 |
|---|---|
| 1989 | 3 |
| 1990 | 2 |
| 1991 | 3 |
| 1993 | 3 |
| 1994 | 3 |
| 1995 | 1 |
| 1996 | 1 |
| 2000 | 1 |
| 2001 | 2 |
| 2002 | 1 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 1 |
| 2009 | 3 |
| 2010 | 1 |
| 2012 | 1 |
| 2016 | 2 |
| 2017 | 2 |
| 2018 | 2 |
| 2019 | 1 |
| 2020 | 1 |
| 2022 | 1 |
| 2023 | 2 |
| 2026 | 1 |
Airframe · Gulfstream Aerospace G-IV
AD 2026-13-02NavigationAD 2023-08-03Flight ControlsAD 2023-10-02Indicating/Recording System, NavigationInformation bulletins that may apply · 5
Advisory, not mandatory.
NTSB investigations
No NTSB investigations matched to N511KAMatched by N-number and event date. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Gulfstream Aerospace G-IV aircraft
FAA incident reports
No FAA accident or incident reports matched to N511KAMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Gulfstream Aerospace G-IV aircraft
Service difficulty reports · 3
SDR 99ZZZX3199Check Valve · failedOXC/BDL - EN ROUTE ON A PRE-POSITIONING FLIGHT, THE CREW REPORTED THE OIL PRESSURE STARTED TO DECLINE ON THE LEFT ENGINE. AT 15 PSI, THE LEFT ENGINE WAS SHUT DOWN. THE AIRCRAFT LANDED WITHOUT INCIDENT AT BDL. AN INVESTIGATION REVEALED THAT OIL WAS LEAKING FSDR 99ZZZM6Seal · failedEN ROUTE FROM BOS-BWI, THE REAR BAY OVERHEAT LIGHT ILLUMINATED. ENGINE POWER WAS REDUCED AND THE LIGHT EXTINGUISHED. POWER WAS REAPPLIED AND THE LIGHT DID NOT ILLUMINATE. THE AIRCRAFT DIVERTED TO OXC AS A PRECAUTION AND LANDED WITHOUT INCIDENT. THE AIRCRAFTSDR 97ZZZX3062Static Plate · froze upTTN/AUS - AFTER TAKING OFF IN HEAVY RAIN WHILE AT CRUISE ALTITUDE, CAPTAIN'S AIRSPEED, ALTIMETER, AND VERTICAL SPEED INDICATORS BECAME ERRATIC. AFTER DESCENT AND AS TEMPERAURE INCREASED ABOVE FREEZING, ALL INDICATIONS RETURNED TO NORMAL. THE AIRCRAFT LANDED W