- Registered owner
- Dodson International Parts Inc
- Location
- Rantoul, KS
- Owner type
- Corporation
- Serial number
- 4037
- Year built
- 2006
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- January 11, 2006
- Certificate issued
- October 21, 2026
- Expires
- October 31, 2033
- Mode S code
- A55E9F
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 N445QSMatched 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 N445QSMatched 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 · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA022220213791Control Unit · faultedFIRE DETECTION LOOP FAULT CAS: DURING FLIGHT AMBER CAS "FIRE DETECTION LOOP FAULT" AND FIRE DETECTION, LEFT, LOOP A, FAULT ILLUMINATED. FOLLOWED QRH PROCEDURE. REPEAT WRITEUP // SIGN OFF // REMOVED AND REPLACED L/H FIRE DETECTION CONTROL UNIT IAW GULFSTREAM G4SDR DXTA021820213791Fault Message · illuminatedFIRE DETECTION LOOP FAULT CAS: DURING FLIGHT AMBER CAS "FIRE DETECTION LOOP FAULT" AND FIRE DETECTION, LEFT, LOOP A, FAULT ILLUMINATED. FOLLOWED QRH PROCEDURE. REPEAT WRITEUPSDR GR4D20180719005Attach Angle · corrodedFOUND CORROSION ALONG LOWER SIDE OF LT HORIZONTAL REAR BEAM (INTERNAL) ATTACH ANGLES AT SEVERAL LOCATIONS WHICH REQUIRES REPLACEMENT OF CAP ANGLE.SDR GR4D20180719004Attach Angle · corrodedFOUND CORROSION ALONG LOWER SIDE OF RT HORIZONTAL REAR BEAM (INTERNAL) ATTACH ANGLES AT SEVERAL LOCATIONS WHICH REQUIRES REPLACEMENT OF CAP ANGLE.SDR GR4D20180719003Attach Angle · corrodedFOUND CORROSION ALONG UPPER SIDE OF RT HORIZONTAL REAR BEAM (INTERNAL) ATTACH ANGLES AT SEVERAL LOCATIONS WHICH REQUIRES REPLACEMENT OF CAP ANGLE.SDR GR4D20180719002Attach Angle · corrodedFOUND CORROSION ALONG UPPER SIDE OF LT HORIZONTAL REAR BEAM (INTERNAL) ATTACH ANGLES AT SEVERAL LOCATIONS WHICH REQUIRES REPLACEMENT OF CAP ANGLE.SDR GR4D20180719001Winglet · corrodedR/H WINGLET BORES V11, V15 AND V16 MEASURE .880 AND HAVE PITTING IN BORES THAT REQUIRE MAJOR REPAIR.SDR GR4D20180502001Hinge · corrodedRT ELEVATOR NR 4 HINGE BLEEDING RUST AND BEARING SLOPPY.SDR DXTAT2PL6D005AMQQUnknown · odorSHORTLY AFTER TAKE OFF, VERY STRONG CHEMICAL ODOR FILLED THE CABIN. ODOR DISSIPATES WHEN RIGHT PACK SELECTED OFF.SDR DXTA2017072006429Reservoir · leakingVERY STRONG ODOR ON T/O FOR 2MIN .. ON DESCENT FOR ENTIRE TIME. CHEMICAL LIKE SMELL THAT U COULD TASTE AND BURNS EYES. ISOLATED ODOR TO RH PACK. RESOLUTION: R/HAND PACK OUTLET DUCTING FOUND TO BE CONTAMINATED WITH SKYDROL FROM LEAKING RESERVOIR. DUCTING REPLASDR DXTA2017061106408Duct · leakingSTRONG ODOR AT TAKE-OFF AND POWER CHANGES. SMELLS LIKE A CHEMICAL AND WET "PUP TENT". WORST ODOR ON LAST LANDING, COULD TASTE, BURNS EYES. ODOR LINGERED WELL AFTER SHUT DOWN AND DOORS OPEN . CREW ALSO REPORTED AN ODOR, WAS NEVER PRESENT WHEN APU AIR WAS USEDSDR DXTA2013040105348Dump Valve · failedFLAPS 20, SELECTED MLG DOWN. RECEIVED A RED HANDLE & LT / RT GEAR UNSAFE & NLG UNSAFE CAS MESSAGES & LT HYD LOW CAS MESSAGE. LT HYD INDICATED 1.8. PROCEEDED WITH LT HYD LOW CHECKLIST, NO CHANGE IN QTY. PROCEEDED TO MLG EXTEND CHECKLIST. USED EMERGENCY MLGSDR DXTA2011090604715Valve · stuckDURING CLIMB OUT, ON FERRY FLT, A FUEL IMBALANCE WAS OBSERVED ON FUEL GUAGES. ON FURTHER INSP FROM CABIN, FUEL WAS STREAMING OUT OF RT WING IN AREA OF PLENUM. IT WAS DECIDED BY CREW TO RETURN TO DEPARTURE. FUEL DOES NOT LEAK WHILE ACFT IS ON GROUND. AFT VENSDR DXTA2011090104037Valve · stuckINFLIGHT - A THICK TRAIL OF FUEL LEAKING FROM THE RT WING WAS BROUGHT TO OUR ATTENTION BY THE FA. AN APPROX 350 LBS FUEL IMBALANCE CONFIRMED THE RT FUEL LEVEL WAS LOWER. THE TRAIL STOPPED MOMENTARILY BUT RETURNED. WERE ABLE TO MAINTAIN FUEL BALANCE THRU THE
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.