- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500671
- Year built
- 2022
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- June 28, 2022
- Certificate issued
- December 30, 2025
- Expires
- December 31, 2032
- Mode S code
- A57AF9
Embraer Executive EMB-505TCDS A60CEAirframe · Embraer Executive EMB-505TCDS E00053ENEngine · Pratt & Whitney Canada PW535E
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 13
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2011 | 1 |
|---|---|
| 2012 | 1 |
| 2013 | 1 |
| 2014 | 1 |
| 2016 | 1 |
| 2018 | 1 |
| 2020 | 1 |
| 2022 | 2 |
| 2023 | 4 |
| 2024 | 1 |
| 2025 | 2 |
| 2026 | 2 |
Airframe · Embraer Executive EMB-505
AD 2026-10-18Flight Control SystemAD 2026-03-05Autopilot Main ServoAD 2024-22-06Cabin Equipment/FurnishingsInformation bulletins that may apply · 2
Advisory, not mandatory.
Airframe · Embraer Executive EMB-505
SAIB CE-16-23Navigation; Degraded Attitude and Heading Reference System (AHRS) Performance When Operating in Areas of Unreliable or Unavailable Global Positioning System (GPS) SignalSAIB CE-10-46Navigation; Embraer EMB-505 Terrain Awareness Warning System (TAWS) Instructions in Airplane Flight ManualNTSB investigations
No NTSB investigations matched to N452QSMatched 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 Embraer Executive EMB-505 aircraft
FAA incident reports
No FAA accident or incident reports matched to N452QSMatched 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 Embraer Executive EMB-505 aircraft
Reports on N452QS not matched to an aircraft · 1
They name N452QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026100609998Dcu · defectiveWHILE IN CRUISE AT FL410 WE REVIEWED MULTIPLE CAS MESSAGES AND AN AURAL AUTO PILOT. THE MESSAGES WERE AP FAIL, SWPS FAULT, YD FAIL, BLEED 2 OFF, STBY BARO NOCOMP, SWPS ICE SPEED, GSD 1 FAIL(HIGHLIGHTED), AND HSDB FAULT. IN ADDITION, THE LT MLG INDICATED TRANSSDR DXTA2026100509998Multiple · malfunctionedWHILE IN CRUISE AT FL410 WE REVIEWED MULTIPLE CAS MESSAGES AND AN AURAL AUTO PILOT. THE MESSAGES WERE AP FAIL, SWPS FAULT, YD FAIL, BLEED 2 OFF, STBY BARO NOCOMP, SWPS ICE SPEED, GSD 1 FAIL (HIGHLIGHTED), AND HSDB FAULT. IN ADDITION, THE LT MLG INDICATED TRANSDR DXTA2026081209208Strut · faultyON TAKEOFF UPON GEAR RETRACTION WE GOT A LANDING GEAR LEVER DISAGREE CAS MESSAGE NOSE GEAR DID NOT GO ALL THE WAY UP. LEVELED OFF COMPLETED QRH PROCEDURE. GEAR CAME DOWN WITH A THREE GREEN INDICATION. CORRECTIVE ACTION: REMOVED NLG STRUT ASSY DUE TO NLG STRUTSDR DXTA2025093005120Skin · dentedBIRD STRIKE TO LEADING EDGE OF LEFT WING APPROX 3 FEET OUTWARD FROM FUSELAGE. THERE IS A NOTICEABLE DENT. INSTALLED REPAIRED LEADING EDGE IAW AMM 57-40-00. LEADING EDGE ALL OPS AND LEAK CHECKS SATISFACTORY.SDR DXTA2025061603852Control Unit · faultyWORN BRAKES: ON TAXI OUT NOTICED BRAKES WERE NOT ENGAGING WELL AND HAD A STRONG VIBRATION. FELT LIKE INTERMITTENT APPLICATION AND STRUGGLING TO GRAB. CORRECTIVE ACTION: REPLACED BRAKE CONTROL UNIT IAW EMB PH300 AMM 32-41-01 OPS CHECK GOODSDR DXTA2025060203685Computer · faultedDURING TAXI BOTH L & R BRAKES CHATTERED, PULSED AND WERE VERY GRINDY. MORE PRONOUNCED WITH LIGHT APPLICATIONS OF THE BRAKES. TAXI SPEEDS WERE UP TO 25KTS AND HAPPENED AT ALL SPEEDS. ALSO A SLIGHT BURNING SMELL FROM THE BRAKES UPON RETURN TO THE FBO. CORRECTSDR DXTA2024102800933Battery Pack · defectiveEMERGENCY LIGHTS BATTERY: EMERGENCY LIGHTS STAY ON WITH SWITCH IN ARMED POSTION. AFTER A FEW MINUTES LIGHTS START TO BLINK. CORRECTIVE ACTION: REPLACED EMERGENCY BATTERY PACKS PN 7450LS-00 SN 005917 & SN 005920 IAW EMB-505 AMM 33-52-01-400-801-A. OPS CHECK GOOSDR DXTA2024040911443Control Unit · faultedDURING TAXI OUT RIGHT BRAKE WAS BINDING. RETURNED TO FBO AND RECEIVED A BRK FAIL CAS MESSAGE UPON SETTING THE PARKING BRAKE. REMOVED FAULTY BRAKE CONTROL UNIT P/N OAP00100-11, SN 352960458 AND REPLACED IT WITH MODIFY BCU, AND PERFORMED SATISFACTORY OPERATIONALSDR DXTA2023081192770Seal · damagedAIRFRAME VIBRATION: DURING FLIGHT ABOVE 250 KNOTS AT ALL ALTITUDES THE AIRCRAFT VIBRATED AND CREATED A LOUD VIBRATION NOISE THROUGHOUT THE CABIN. THE INTENSITY OF THE VIBRATIONS AND NOISE INCREASED DURING DECENT AND INCREASE OF SPEED. THE CABIN WALL ALONG TSDR DXTA2023053087210Unknown · unknownEMERG EXIT DOOR: THE EMERGENCY EXIT DOOR IS NOT SEATED PROPERLY. FROM THE INSIDE OF THE CABIN THE TOP RIGHT CORNER IS PUSHED IN ABOUT 1/2 INCH AT THE WIDEST POINT. YOU CAN SEE SUNLIGHT SHINNING BETWEEN THE DOOR AND SIDE WALL PANEL ON THE LEFT INSIDE OF THE DOSDR DXTA2022120975910Door · lack of lubeMAIN DOOR: MAIN CABIN DOOR VERY DIFFICULT TO OPEN FROM INSIDE AND OUTSIDE OF AIRPLANE. " CORRECTIVE ACTION" OPENED THE MAIN ENTRY DOOR AND VERIFIED THAT THE DOOR WAS
DIFFICULT TO OPEN. WITH THE DOOR OPEN EXTENDED AND RETRACTED THE
MED DOOR PINS WITH DOOR HAN
Reports on N452QS not matched to an aircraft · 6
They name N452QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2012F00172Winglet · corrodedRIGHT WINGLET CORRODED IN ATTACH BORE, REF W/O 2142.23.3-23.6 FOR REPAIR.SDR DXTA2012022704888Engine · vibrationNR 1 ENGINE DISPLAYED HIGH VIBRATION, IE LP 2.25, IN FLIGHT. PRECAUTIONARY SHUTDOWN AND LANDING WITHOUT FURTHER INCIDENT. INSPECTED AIRCRAFT, NO DEFECTS NOTED.SDR DXTA2011120804819Reservoir · leakingAMBER "COMBINED HYD QUANTITY" CAS MESSAGE AT FL410. THE COMBINED HYD SYS QTY INDICATION (EICAS) READS ZERO. THE FUSELAGE COMBINED SYS GAUGE ALSO READS ZERO. NO HYD FLUID FOUND IN EQUIPMENT BAY OR OUTSIDE FUSELAGE. R & R THE COMBINED HYD RESEVOIR & FOUND SATI
STCs that may be installed · 47
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 47 STCs