- Registered owner
- G200 LLC
- Location
- Tulsa, OK
- Owner type
- LLC
- Serial number
- 212
- Year built
- 2008
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- October 12, 2008
- Certificate issued
- December 10, 2019
- Expires
- December 31, 2029
- Mode S code
- A01527
Israel Aerospace Ind GULFSTREAM 200TCDS A53NMAirframe · Israel Aerospace Ind GULFSTREAM 200TCDS E35NEEngine · Pratt & Whitney Canada PW306A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 19
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2001 | 1 |
|---|---|
| 2002 | 3 |
| 2004 | 2 |
| 2005 | 1 |
| 2006 | 1 |
| 2007 | 3 |
| 2008 | 1 |
| 2010 | 1 |
| 2011 | 2 |
| 2023 | 2 |
| 2026 | 2 |
Airframe · Israel Aerospace Ind GULFSTREAM 200
AD 2026-16-09Time Limits/Maintenance ChecksAD 2026-13-02NavigationAD 2023-10-02Indicating/Recording System, NavigationInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N104SGMatched by N-number and event date, checked against the reported serial number, make and model. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Israel Aerospace Ind GULFSTREAM 200 aircraft
FAA incident reports
No FAA accident or incident reports matched to N104SGMatched by N-number and event date, checked against the reported make and model. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Israel Aerospace Ind GULFSTREAM 200 aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR 9JLA202202178028Flex Hose · leakingTHE FLIGHT CREW REPORTED THE LEFT ENGINE ROLLED BACK 20 TO 25% AFTER THE INITIAL POWER REDUCTION BEFORE RELIGHTING. THIS OCCURRED AT THE YOP OF DECENT AROUND 36000 FT. THE FLIGHT CREW ALSO STATED THAT THE AIRCRAFT SHUTTERED DURING THIS EVENT. AFTER RELIGHT THESDR 9JLA2021052728324Hydraulic System · false indicationTHE FLIGHT CREW REPORTED THAT THE RIGHT HYDRAULIC QUANTITY DECREASED 1% PER 15 MINUTES. NORMAL 98% AFTER SHUTDOWN. A "LOW HYDRAULIC QUANTITY" REFILL EICAS MESSAGE. THE MAINTENANCE VENDOR SERVICED THE LEFT AND RIGHT HYDRAULIC SYSTEM AS PER THE AMM. NO SERVICINGSDR 9JLA2021051828322Uplock Switch · defectiveTHE FLIGHT CREW REPORTED THAT AFTER TAKEOFF AND GEAR RETRACTION A GEAR UNSAFE INDICATION AFTER SUCCESSFUL RETRACTION. THEY RECYCLED THE LANDING GEAR WITH NO IMPROVEMENT. AFTER RUNNING THE CHECKLIST THE CREW ELECTED TO DIVERT BACK TO KPBI FOR LANDING AND REPAIR
STCs that may be installed · 155
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 155 STCs
Earlier aircraft with this N-number · 1
This aircraft carried N104SG before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.