- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500468
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- July 17, 2018
- Certificate issued
- June 1, 2026
- Expires
- June 30, 2033
- Mode S code
- A50833
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 N423QSMatched 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 N423QSMatched 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 DXTA2026031207195Battery · faultedWHEN MOVING EMER LIGHT SWITCH TO ARM POSITION ALL EMER LIGHTS COME ON AND STAY ON. THEY REMAIN ON WHEN MOVING TO THE ON POSITION AND BACK TO THE ARM POSITION. REMOVED AND REPLACED FWD AND AFT EMERGENCY BATTERIES WITH REPAIRED UNITS AS NEEDED. PERFORMED OPS CSDR DXTA2025081104522Handle · faultedTHE SPRING ON THE EXTERIOR RED LEVER HANDLE IS BROKEN. WHEN YOU UNSTOW THE HANDLE THE LEVER DROPS DOWN WITH NO TENSION. WHEN YOU MOVE THE LEVER BACK TO THE NEUTRAL DETENT IT WILL NOT STOW WITHOUT MANIPULATION OF THE CLASP TO STOW IN PLACE. THE CLASP ITSELF IS SDR DXTA2025062704031Selector · unserviceableWE GOT A FLAPS FAIL CAS MESSAGE WHEN BRINGING FLAPS FROM 1 TO 2. CYCLED FLAPS AND CAS MESSAGE WENT AWAY. TRIED A SECOND TIME AND WHEN BRINGING FLAPS TO 2 GOT CAS MESSAGE AGAIN. WENT THROUGH QRH AND LANDED FLAPS ZERO. CORRECTIVE ACTION: REMOVED #1 FCE AND INSTASDR DXTA2023092996840Battery · inoperativeWITH SWITCH IN ARMED POSITION, ALL EMERGENCY LIGHTS WERE ON. PERFORMED AMM 24-41-00-860-801-A/200, AND PER AMM REPLACE BATTERIES. REMOVED FORWARD AND AFT EMERGENCY BATTERIES AND REPLACED WITH SERVICABLE UNITS AND CHARGED IAW AMM 33-51-01.SDR DXTA2023050585480Not Reported · burned outDURING CLIMB THROUGH FL340 A BURNING ELECTRICAL SMELL WAS NOTICED. AFTER A FEW MINUTES MUTIPLE EICAS MESSAGES ILLUMINATED. NR 1 RADIO ON BOTH GIA'S FAILED A/P FAILED YAW DAMP FAILED & SEVERAL OTHER SYS. NR 2 RADIO WAS TRANSMITTING VERY WEAK AND AT TIMES OTHESDR DXTA2021101750340Battery · defectiveEMERG LIGHT SWITCH: EMERGENCY LIGHTS REMAIN ON WITH EMER LT SWITCH IN THE ARM POSITION.///SIGN-OFF///REPLACED BOTH BATTERIES AND PERFORMED OPS CHECKS GOOD. WORK DONE IAW PHENOM 300 AMM CHAP 33-52-01SDR DXTA2020081093956Warning Message · false activationDOOR PAX OPEN WARNING MESSAGE APPEARED AFTER START UP. CYCLED DOOR THREE TIMES, WARNING MESSAGE REMAINED ON. RAN ENGINES AND OPS CHECKED PAX DOOR NUMEROUS TIMES, NO WARNING MESSAGES APPEARED AFTER START. THERE WAS NO HISTORY ON THIS ISSUE. OPS CHECKED THE MSDR DXTA2020031603588Electronic Unit · defectiveFLAP FAIL YELLOW CAS ILLUMINATED - IN CRUISE AMBER SWPS FAULT DISPLAYED, WITH FLAP FAIL, PTRIM BKP FAIL INDICATIONS. //SIGNOFF// REPLACED #1 FCE PART # 462900-1017 SN# 1245 WITH REPAIRED UNIT IAW P-300 AMM 27-03-01-400-801-A PERFORMED FLAPS SYSTEM RIGGING IASDR DXTA2019102402971Tube · failedDURING FLIGHT HEARD A LOUD SQUEALING NOISE FOLLOWED BY A WHITE HYD SYS FAULT. FOLLOWED THE CHECKLIST. WE PULLED UP THE HYD SCHEMATIC, NOTICED THAT THE HYD PRESSURE WAS SLOWLY GOING TO ZERO. THEN GOT A HYD LO PRESS FOLLOWED BY PUSHER FAIL AND BRK FAIL. COM
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