- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500263
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- December 4, 2014
- Certificate issued
- March 6, 2025
- Expires
- March 31, 2032
- Mode S code
- A3F161
Embraer S A EMB-505TCDS A60CEAirframe · Embraer S A 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 S A 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 S A 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 N353QSMatched 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 S A EMB-505 aircraft
FAA incident reports
No FAA accident or incident reports matched to N353QSMatched 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 S A EMB-505 aircraft
Reports on N353QS not matched to an aircraft · 1
They name N353QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another 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 DXTA2026070908718Wire · brokenDOOR PAX OPEN CAS MESSAGE DISPLAYED BRIEFLY WHILE CLIMBING THROUGH 11,000 FEET. CLIMBING THROUGH FL210 THE MESSAGE RETURNED. WE RAN THE QRH AND BEGAN THE REQUIRED DESCENT TO 10,000 FEET. AT SOME POINT IN THE DESCENT THE MESSAGE CLEARED AND REMAINED OFF THROUGHSDR DXTA2026070708691Proximity Switch · failedRED WARNING CAS DOOR PAX OPEN CAME ON MULTIPLE TIMES WITHIN FLIGHT. ONCE AT FL380, ONCE AT FL400, BOTH TIME IT WENT AWAY WITHIN A COUPLE MINUTES. FOLLOWED THE QRH AND DESCENDED TO 10,000FT WHERE THE CAS MESSAGE CAME ON AGAIN. REMOVED AFT LOWER MED MICROSWITCHSDR DXTA2025030402548Seal · unsecureFUSELAGE PLATES / SKINS / PANELS: REPEAT WRITE UP, 3RD TIME. INTERMITTENT, LOUD, NOTICEABLE HUMMING SOUND AND VIBRATION COMING FROM THE RIGHT SIDE OF THE AIRCRAFT. VIBRATION MOSTLY NOTICEABLE NEAR RIGHT MIDDLE PASSENGER SEAT, AND NOISE IS LOUDER IN THE CABIN TSDR DXTA2024121901538Seal · damagedDURING CLIMB OUT AROUND 25,000FT A VERY LOUD BUZZING/HUMMING NOISE WAS HEARD. WE COULD FEEL THE VIBRATIONS IN THE FLOOR BOARD IN THE COCKPIT. WHEN WE LEVELED OFF AT 31,000FT THE FO WENT BACK AND CONFIRMED THE NOISE ORIGINATED FROM THE RT SIDE OF ACFT OVER WINGSDR DXTA2023112210123Unknown · unknownCABIN EMERG LIGHT: GO FROM THE OFF POSTION TO ARM POSITION THE EMR LIGHTS COME ON. THEY STAY ON FOR AROUND 3 SECONDS IN THE ARM POSITION THEN GO OFF. PERFORMED OPS CHECK/TEST OF CABIN EMERG LIGHTS WITH NO DEFECTS NOTED, FOUND EMERG LIGHTS TO OPERATE NORMAL. SDR DXTA2023062689580Unknown · unknownIMMEDIATELY AFTER TAKEOFF "AUTO PILOT FAIL" "AUTO TRIM FAIL" AND "PICH TRIM NORM FAIL" EICAS MESSAGES ILLUMINATED. AIRCRAFT FLOWN TO A LANDING WITH THE BACKUP MANUAL TRIM FUNCTION.//CORRECTIVE ACTION// REMOVED FAULTY FCE NO 2 P/N: 462900-1017 S/N: 0112. INSTALSDR DXTA2023061288480Unknown · unknownCOCKPIT/CABIN NOISE: CLIMBING ABOVE 38000 FT THE CABIN CLIMB RATE BEGAN TO SPIKE AND DESCEND BETWEEN PLUS/MINUS APPROXIMATELY 1800 FT PER MIN FOLLOWED BY A LOUD AIR NOISE ON THE COPILOT'S SIDE. WE DONNED THE MASKS AND DESCENDED AND RETURN TO OUR DEPARTURE AIRPSDR DXTA2022062464550Proximity Sensor · out of adjustBOTH EMERGENCY AIRSTAIR STEP LIGHTS INOP WITH THE EMER LT SWITCH IN THE ON POSTION. // SIGNOFF// RESECURED FLOOR PROXIMITY LIGHT IN REFERENCE TO EMBRAER PHENOM AMM 33·52·11. NO FURTHER DEFECTS NOTED AT THIS TIME.SDR DXTA2022061964200Landing Gear · warning lightLG LEVER DISAG RED CAS: RED CAS LG LEVER DISAG NOTED DURING GEAR RETRACTION AFTER T/O. NO ISSUES NOTED DURING EXTENSION AND RETURN LANDING.//CORRECTIVE ACTION//PERFORMED FIM TASKS 32-61-00-810-808-A AND
32-61-00-810-808-A NO ACTIVE FAULTS LISTED IN CAS WINDSDR DXTA2022040659730None · noneRIGHT ENGINE ENGINE FAN BLADE: DURING TAKEOFF ROLL AT ROTATION, WE HAD A VERY LARGE BIRD STRIKE WITH INGESTION IN THE RIGHT ENGINE.SDR DXTA2021082447530Relay · abnormalCABIN EMERG LIGHT: CABIN EMERGENCY LIGHTING WAS OBSERVED TO BE BLINKING ON AND OFF DURING FLIGHT WITH THE EMER LIGHT IN THE ARMED POSITION. TROUBLESHOT DISCREPANCY TO A BAD PILOT CONTROL EMERGENCY LIGHT RELAY. REMOVED RELAY PN M83536/15-022L NSN AND INSTALLEDSDR DXTA2021072945980Battery · defectiveCABIN EMERG LIGHT: ENROUTE TO KADS THE CABIN EMERGENCY LIGHTING BEGAN FLASHING AND CONTINUED THROUGH THE DURATION OF THE FLIGHT. //SIGNOFF// T/S SYSTEM REMOVED FWD EMERGENCY BATTERY AND INSTALLED A NEW BATTERY IAW PHENOM 300 AMM 33-52-01-400 ALL OPS CHECKS GOOSDR DXTA2021011804609Controller · defectiveIN LEVEL CRUISE AT 41,000 FEET, PRESSURIZATION STARTED TO CLIMB RATHER SWIFTLY. WITH O2 MASKS ON, WE STARTED AN EMERGENCY DECENT. WITH O2 MASK ON, CABIN PRESSURE REACHED APPROX 20FT, PICTURES ATTACHED. SEVERAL CAS MESSAGES WERE ASSOCIATED. PAX MASKS ALSO DSDR DXTA2020121604475Door · obstructedMAIN CABIN DOOR WILL NOT OPEN HAD TO EXIT THE AIRPLANE THROUGH THE EMERGENCY EXIT DOOR. FOUND TRIM PIECE GETTING STUCK ON DOOR FRAME. REMOVED AND PROPERLY INSTALLED DOOR TRIM, IAW EMB300 MM 25-23-04/400. OPENED AND CLOSED DOOR SEVERAL TIMES, CHECKED GOOD EA
Reports on N353QS not matched to an aircraft · 10
They name N353QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2011100204741Anti-Skid Valve · inoperativeBRAKES GRAB HARD WHEN PEDALS ARE APPLIED AND PULL ACFT TO THE LT. THE LT PULL IS MORE PROMINENT FROM THE RT SEAT. INSTALLED PRESS. GAGE'S FOUND RT SIDE ERRATIC. REMOVED GAGES' BLED BRAKES IAW MM 32-42-00. TAXIED ACFT. RT SPONGEY & LT GRABS WITH SLIGHT PRESDR DXTA2010112204316Brake · dirtyTHE LT BRAKE GRABBING WHEN PRESSURE IS APPLIED. BRAKE IS STILL SMOKING A LITTLE AFTER SHUTDOWN. REMOVED LEFT BRAKE ASSY, CLEANED AND REINSTALLED. PERFORMED HIGH SPEED TAXI CHECK. OPS CHECKED GOOD IAW MM 32-42-00.SDR DXTA2010112204313Strut · leakingON LANDING ROLL, BRAKES FELT "GRABBY". UPON POST FLIGHT INSP, FOUND LT MAIN GEAR STRUT WET AND FLUID DRIPPING FROM MAIN STRUT INBD SIDE OF STRUT. LT STRUT IS LESS THAN A CREDIT CARDS WIDTH. RESEALED LT STRUT AND SERVICED. R & R LT BRAKE ASSY. R & R LT MAI
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