- Owner type
- Corporation
- Serial number
- 4014
- Year built
- 2005
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 29, 2005
- Certificate issued
- May 17, 2022
- Expires
- May 31, 2029
- Mode S code
- A4E822
Gulfstream Aerospace GIV-X (G450)TCDS A12EAAirframe · Gulfstream Aerospace GIV-X (G450)Engine modelRolls-Royce TAY-611SER
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 17
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 |
|---|---|
| 2005 | 1 |
| 2006 | 3 |
| 2007 | 1 |
| 2009 | 1 |
| 2012 | 2 |
| 2013 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2017 | 1 |
| 2018 | 2 |
| 2019 | 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 N415QSMatched 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 N415QSMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2021070644620Light · malfunctionedFLOOR EMERG EXIT LIGHT: ENTIRE BANK OF RED EMERGENCY LIGHTS AT SEAT 12 ARE INOP. UPON INITIAL POWER UP, THEY ALL BLINK ON AND GO OUT. // SIGNOFF// OPS CHECKED THE LIGHTS WITH NO DEFECTS NOTED. WORK DONE IN REF G450 AMM 33-50-00.SDR DXTA2020110204305Control Unit · defectiveJUST PRIOR TO TOP OF DESCENT, CAS MESSAGES RECEIVED: AMBER "FLAPS FAILED", BLUE "STABILIZER SYNCING". BEFORE LANDING, THE USE OF FLAPS WAS UNSUCCESSFUL. LANDED ZERO FLAPS. ACCESSED CMC AND INTERROGATED CMC, RECORDED FAULTS. ATTEMPT TO CLEAR FLAPS FAIL CAS SDR JGVR20200923001Clamp · out of positionFOUND VACUUM WASTE TUBE CLAMP TO BE CONTACTING THE UPPER WING PLANK AT FS 355 DURING COMPLIANCE WITH CUSTOMER BULLETIN 206. INSPECTED AREA AND FOUND ONLY PRIMER WAS RUBBED OFF. CLEANED, ALODINED AND PRIMED AREA, PER GULFSTREAM W/O.SDR DXTA2019121803210Control Cable · out of limits***ENTERING FOR HISTORICAL DATA*** DURING OPERATIONAL CHECK FLIGHT AT 39500', MACH .85 WITH SPED BRAKES DEPLOYED, AILERON TRIM STUCK SOLID AND COULD NOT BE MOVED FOR REST OF FLIGHT. AFTER ENGINE SHUTDOWN, TRIM COULD BE MOVED BUT FELT STIFF.///SIGN-OFF///INSPESDR DXTA2015031605997Brake Sys · contaminatedBRAKES FELT SMOOTH BUT SPONGY ON LANDING. TAXIED AIRCRAFT AND VERIFIED DISCREPANCY. EXTENSIVELY BLED AIR FROM BRAKE SYSTEM CHARGE. PERFORMED ANOTHER TAXI CHECK WITH SATISFACTORY RESULTS. WORK DONE IN REFERENCE TO AMM 32-41-00. OPS CHECK GOOD.SDR DXTA2014102705917Apu · failedAPU VIBRATED VIOLENTLY AFTER 15 MINUTES OF OPERATION AFTER ENG SHUTDOWN. APU AUTOSHUTDOWN. LARGE QTY OF SMOKE & SOME FLAMES VISIBLE FROM INTAKE. FIRE BOTTLE DISCHARGED. REMOVED AND REPLACED THE APU IAW G-450 MM 49-00-00. OPS AND LEAK CHECKED GOOD.SDR DXTA2014021005645Float Valve · stuckAFTER TAKEOFF FUEL LEAK OUT OF RT WING OTBD LOWER SIDE LOST 800 LBS FUEL IN ABOUT 4 MINUTES. REMOVED RT WING TANK ACCESS PANEL G21TB-17. AFTER ACCESSING TANK FOUND BOTH FORWARD AND AFT VENT FLOATS STUCK IN THE OPEN POSITION. REMOVED FORWARD AND AFT VENT FLOSDR DXTA2012022004879Brake Sys · malfunctionedUPON BRAKE APPLICATION, NO BRAKING UNTIL TOP OF PEDALS ARE DEPRESSED APPROX 2.5", THEN SUDDENLY 500LBS OF PRESSURE, BRAKES GRAB SUDDENLY. PERFORMED BRAKE BLEEDING PROCDURES WITH LT HYD SYS PRESSURE. NOTED AIR PRESENT WHILE BLEEDING BRAKES. ACCOMPLISHED BRAKSDR 401407092006Warning Message · activatedSTAB FAIL MESSAGE AND WOULD NOT MOVE.
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.