- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500444
- Year built
- 2017
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- December 27, 2017
- Certificate issued
- March 6, 2025
- Expires
- March 31, 2032
- Mode S code
- A4EF90
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 N417QSMatched 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 N417QSMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025110305525Starter Gen · faultedGEN 1 OFF BUS YELLOW CAS IN FLIGHT WITH ASSOCIATED VIBRATION. RAN CHECKLIST AND EVENTUALLY SHUT DOWN LEFT ENGINE PER QRH. PERFORMED UNEVENTFUL ONE ENGINE INOPERATIVE LANDING AND SHUT DOWN OPERATING ENGINE. CORRECTIVE ACTION: REMOVED STARTER PN: 400SG180Q-6 SN SDR DXTA2025011001871Battery · defectiveCABIN EMERG LIGHT ALL CABIN EMERGENCY LIGHT REMAIN ILLUMINATED WITH THE SWITCH IN THE ARM POSITION. LIGHTS ALSO FLICKER ON AND OFF WHILE IN THE ARM POSITION. CORRECTIVE ACTION: REPLACED FORWARD EMERGENCY BATTERY. OPS CHECK GOOD. PHENOM 300 AMM 33-52-01-400-801SDR DXTA2024052011817Rod · detachedLEFT MAIN CABIN DOOR TELESCOPING ROD IS SEPARATING FROM THE MAIN CABIN DOOR. COMPLIED WITH REPAIR OF THE MED AND INSTALLED A NEW TELESCOPING ROD FITTING PN 500-09754-011.SDR DXTA2024013110765Warning Message · illuminatedLG LEVER DISAG RED CAS: ON FINAL APPROACH, WE RECIEVED A LG LEVER DISAG CASS MESSAGE. WE COMPLIED WITH THE QRH PROCEEDURE (EAP12-3). AFTER CYCLING THE GEAR, A LOUD BANG WAS NOTED COMING FROM THE NOSE GEAR. THE FREE FALL HANDLE WAS THEN PULLED TO GET A THREE GRSDR DXTA2023082193450Unknown · unknownCAPTAIN ALTITUDE/AIRSPEED INDICATION: DURING DECENT WE RECIEVED ALT MISCOMPARE ICON ON BOTH PFDS. JUST AFTER THAT WE RECIEVED A SWPS FAULT YELLOW MESSAGE. WE LEVELED OFF AT 10000FT TO TROUBLE SHOOT AND RUN THE CHECKLIST. THE CAPTAIN SIDE ALTIMETER WAS APPX SDR DXTA2023072191370Battery · failedAFTER ENGINE START, EMER LT NOT ARMED CAS ILLUMINATED WITH SWITCH IN THE ARM OR ON POSITION. CABIN EMER LIGHTS REMAIN ON WITH SWITCH IN ON OR ARM POSTITON. CONDITION OCCURS WITH AIRCRAFT POWERED OR UNPOWERED. NO SUCCESS WITH RESET PROCEDURE. REPLACED #1 AND #SDR DXTA2022122777190Battery Pack · defectiveALL CABIN EMERGENCY LIGHTS STAY ILLUMINATED WHEN THE SWITCH IS IN THE ARM POSITION. ATTEMPTED TO CHARGE BATTERIES, OPS CHECK FAILED. DISCONNECTED CONNECTOR PLUG FROM AFT BATTERY AND LIGHTS WORKED AS THEY SHOULD. REMOVED AND REPLACED AFT BATTERY WITH NEW BATTESDR DXTA2021061643750Control Module · faultedBRK FAIL YELLOW CAS: BRK FAIL ON LONG APPROACH, COMPLETED THE QRH AND PERFORMED A NORMAL LANDING. "CORRECTIVE ACTION" REMOVED BRAKE CONTROL MODULE, INSTALLED INSPECTED MODULE, REMOVED BRAKE CONTROL MODULE P/N DAP00101-02, S/N 0044RH. INSTALLED INSPECTED MODULESDR DXTA2019030402103Controller · defectiveBLEED 1 LEAK YELLOW CAS ILLUMINATED - BLEED 1 LEAK AMBER CAS MESSAGE ILLUMINATED IN CRUISE FLIGHT AT 13,000 FEET. THE BLEED 1 AND 2 SWITCHES AND XBLEED KNOB WERE SELECTED OFF IN THE APPROPRIATE SEQUENCE AS DIRECTED BY THE QRH PROCEDURE. THE BLEED 1 LEAK CAS ME
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