- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500486
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Experimental, research and development
- Airworthiness date
- June 17, 2026
- Certificate issued
- May 2, 2022
- Expires
- May 31, 2029
- Mode S code
- A51E7D
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 N429QSMatched 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 N429QSMatched 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
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026010606414Altimeter · out of toleranceAT FL180 STANDBY ALTIMETER READS 90 FEET ABOVE TOLERANCE CORRECTIVE ACTION: PERFORMED A GVI OF STANDBY PITOT TUBE, NO DAMAGE OR OBSTRUCTIONS NOTED, PER TASK 34-11-02-210-801A. PERFORMED TASK 34-11-02-100-801A PITOT-STATIC PROBE -DRAIN HOLE CLEANING. GAINED ACCSDR DXTA2025062404030Sign · inoperativeEMERG EXIT SIGN/LIGHT: THE EMERGENCY EXIT SIGN LIGHT ABOVE MAIN CABIN DOOR IS INOP. RE-SECURED CONNECTOR FOR THE EMERGENCY EXIT SIGN ABOVE MAIN CABIN DOOR. EMERGENCY EXIT SIGNS OPS CHECKS GOOD AT THIS TIME, REF, EMB-505 AMM 33-50-00.SDR DXTA2024032811318Transducer · failedBRK FAIL CAS MESSAGE AND BRAKE FAILURE ON TAXI. HAD TO USE EMERGENCY BRAKE TO STOP THE AIRCRAFT. BRK FAIL YELLOW CAS: BRK FAIL CAS MESSAGE AND BRAKE FAILURE ON TAXI. HAD TO USE EMERGENCY BRAKE TO STOP THE AIRCRAFT. BRAKE FALL CAS MESSAGE. REMOVED AND REPLACEDSDR DXTA2024030811137Warning Light · false activationDURING CLIMB THROUGH FL180 WITH THE WINGSTAB SWITCH IN OFF POSSITION, WE RECIEVED A A-I WINGSTAB LEAK. CREW COMPLEATED THE A-I WINGSTAB QRH. A-I WINGSTAB CAS REMAINED ON FOR THE REMAINDER OF THE FLIGHT. NOTE THAT ALL SWITCHES ARE LEFT IN THE EMERGENCY CONDITISDR DXTA2023072491460Control Unit · defectiveRIGHT MLG BRAKE: AFTER LANDING IT BECAME VERY DIFFICULT TO MAKE RIGHT TURN ON THE TAXIWAY AND TO MAINTAIN CENTERLINE. THE RIGHT BRAKE APPEAR TO GRAB EXCESSIVELY. ENTIRE AIRFRAME SHUDDERS WHEN APPLYING RIGHT BRAKE DURING LOW SPEED TAXI. //SIGNOFF// REMOVED ANDSDR DXTA2023071991270Battery · defectiveEMERG EXIT SIGN/LIGHT STARTED FLICKERING IN CRUISE ONE HR INTO THE FLIGHT. DURING THE CHARGE PART OF TASK CARD TC·E50·33-1001 THE EMER LIGHTS WOULD NOT EXTINGUISH LN ARM. GAINED ACCESS TO BOTH #LAND #L BATTERIES AND TROUBELSHOT TO THE #L BATTERY. REMOVED ANO SDR DXTA2022030958240Brake Assy · defectiveRIGHT MLG BRAKE: ON TAXI OUT NOTICED ENTIRE AIRCRAFT SHUDDERS WHEN BRAKES WERE APPLIED. ON TAXI IN TRIED JUST LEFT BRAKE AND APPEARED TO BE SMOOTH. APPLIED JUST RIGHT BRAKE AND SHUDDER WAS EVIDENT. // SIGNOFF// REMOVED AND INSTALLED "OVERHAULED" RH BRAKE ASSESDR DXTA030120213873Indicator · contaminatedMAIN DOOR: LOWER RIGHT GREEN FLAG IS NOT VISIBLE IN THE WINDOW. SIGN OFF REMOVED MAIN ENTRY DOOR AIR STAIRS AND CLEANED DEBRIS FROM GREEN INDICATOR PAINT ON PINS AS REQUIRED REINSTALLED MAIN ENTRY DOOR AIR STAIRS IAW EMB PHENOM 300 AMM 52-14-00-400-80 1-A.
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