- Registered owner
- Heritage Double Eagle LLC
- Location
- Queensbury, NY
- Owner type
- LLC
- Serial number
- 4210
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- November 11, 2010
- Certificate issued
- August 5, 2025
- Expires
- August 31, 2032
- Mode S code
- A1FCA6
Gulfstream Aerospace GIV-X (G450)TCDS A12EAAirframe · Gulfstream Aerospace GIV-X (G450)TCDS E25NEEngine · Rolls-Royce TAY-611-8C
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 20
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1994 | 2 |
|---|---|
| 2004 | 1 |
| 2005 | 1 |
| 2006 | 3 |
| 2007 | 1 |
| 2008 | 1 |
| 2009 | 1 |
| 2012 | 3 |
| 2013 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2018 | 2 |
| 2019 | 1 |
| 2020 | 1 |
| 2023 | 2 |
| 2026 | 1 |
Airframe · Gulfstream Aerospace GIV-X (G450)
AD 2026-13-02NavigationAD 2023-08-03Flight ControlsAD 2023-10-02Indicating/Recording System, NavigationInformation bulletins that may apply · 3
Advisory, not mandatory.
Airframe · Gulfstream Aerospace GIV-X (G450)
SAIB CE-19-20Flight Compartment WindowsSAIB NM-10-13Navigation: Flight Management SystemSAIB NM-10-12Navigation: Flight Management SystemNTSB investigations
No NTSB investigations matched to N227SVMatched 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 Gulfstream Aerospace GIV-X (G450) aircraft
FAA incident reports
No FAA accident or incident reports matched to N227SVMatched 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 Gulfstream Aerospace GIV-X (G450) 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 FOMA2018050100001Rod · crackedROUTINE POST-FLIGHT VISUAL INSPECTION NOTED LONGITUDINAL CRACKS THROUGH RIVET POINT DUE TO EXPANSION FROM METAL CORROSION ON LEFT AND RIGHT MAIN LANDING GEAR ROD ASSEMBLES, MAIN LANDING GEAR FAIRING, REMOVED THE AFFECTED PARTS AND REPLACED WITH NEW.SDR BQVA2011061300010Structure · corrodedDURING COMPLIANCE OF CMP CODES 573013 & 573014 WINGLET ATTACH HARDWARE (LEFT & RIGHT) - INSPECTION, SOME CORROSION WAS FOUND IN THE WINGLET ATTACH BORES ONCE THE BUSHINGS WERE REMOVED.SDR BQVA32306Lamp · failedLEFT BLEED AIR VALVE PBA SWITCH LAMP FAILURE, NO INDICATION OF CLOSED VALVE. RESULTED IN CABIN O2 MASK DEPLOYMENT WITH AIRCRAFT DIVERTED TO RALIEGH DURHAM, NC (RDU).
STCs that may be installed · 274
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.