- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500237
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- November 21, 2014
- Certificate issued
- April 22, 2025
- Expires
- April 30, 2032
- Mode S code
- A3E9F3
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 N351QSMatched 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 N351QSMatched 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 · 15
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026050807948Electronic Unit · failedRETRACTED FLAPS AFTER TAKEOFF, FLAP FAIL CAS AND YELLOW FLAP 0 MFD FLAP INDICATION. CONDUCTED FLAP FAIL APPROACH QRC. FLAPS REMAINED STUCK AT 0. REMOVED FCE 2. REMOVED FCE 1, AND INSTALLED IN ORIGINAL FCE 2 POSITION. INSTALLED REPAIRED FCE 1, IAW AMM 27-03-0SDR DXTA2026032307324Door Seal · defectiveREPEAT WRITE UP. DURING CRUISE AND DESCENT THERE WAS A HIGH PITCH SQUEAL FROM THE MAIN CABIN DOOR. MAX ALTITUDE WAS FL230. CABIN PRESSURE WAS NOT AFFECTED. REMOVED THE OLD SEALANT FROM THE DOOR FRAME THEN CLEANED THE DOOR FRAME. REPLACED MAIN DOOR RUBBER SEALSDR DXTA2026031707254Seal · pinchedREPEAT WRITEUP: LOUD CONTINUOUS HISSING NOISE COMING FROM LOWER LEFT SIDE MAIN DOOR ENROUTE. UPPER RIGHT SIDE DOOR SEAL PINCHED BY COVER PLATE WITH DOOR OPEN. CORRECTIVE ACTION: REPLACED AFT ASHROUD ASSY. OPS CHECK GOOD. IAW EMB505 AMM 25-23-05SDR DXTA2026030907147Handle · fracturedMAIN DOOR HANDLE FELL OFF WHEN TRYING TO OPEN DOOR. RED BAR SEPARATED FROM AIRCRAFT. LEFT IN BAGGAGE FOR MX. PERFORMED INSPECTION OF MAIN CABIN ENTRY DOOR AT SIGNATURE T1 FOLLOWING REPORTS OF ENTRY DIFFICULTY. FOUND MAIN DOOR HANDLE FRACTURED WITH ONLY A PARSDR DXTA2025122306266Modulating Valve · faultedWHILE ON CLIMB OUT WE NOTICED A BURNING SMELL IN THE FLIGHT DECK ACCOMPANIED BY HIGH COCKPIT TEMPERATURE. SHORTLY AFTER WE RECEIVED THE DUCT 1 OVERTEMP YELLOW CAS MESSAGE. THE ECS SYSTEM SYNOPTIC PAGE SHOWED A YELLOW HX VALUE FOR THE LEFT SIDE AT 320°F. WE ACSDR DXTA2025080504454Strut · dirtyMAIN PAX DOOR WARNING ILLUMINATED SEVERAL TIMES DURING FLIGHT SPOKE WITH PILOTS AND RECREATED THE BINDING. THE SUPPORT STRUT WAS CREATING A CHATTER NOISE BUT WAS NOT CAUSING THE DOOR TO OPERATE IMPROPERLY. WAITED FOR AIRCRAFT TO COME INTO HANGER TO FURTHER EVASDR DXTA2024081600203Light · faultedCABIN EMERGENCY LIGHTS ARE ON WHEN THE EMER LT SWITCH IS IN THE ARM POSITION. FOUND DOOR SWITCH TO BE STICKING. REMOVED AND REINSTALLED SWITCH. OPS CHECKED SATISFACTORYSDR DXTA2024081400181Battery · weakCABIN EMERG LIGHT: CABIN EMER LIGHTS ILLUMINATE INTERMITTENTLY DURING FLIGHT. REMOVED THE #1 AND #2 EMERGENCY BATTERIES REFERENCING PHENOM 300 MM TASK 33-52-01-000-801-A INSTALLED THE #1 AND #2 EMERGENCY BATTERIES REFERENCING PHENOM 300 MM TASK 33-52-01-400-80SDR DXTA2023042184640Battery · inoperativeEMER LIGHT UNARMED AMBER CAS MESSAGE DISPLAYED WHEN SWITCH IS ARMED DURING ENGINE START. MULTIPLE INTERIOR EMERGENCY LIGHTS AND OVERHEAD INTERIOR LIGHTS FLASH UPON PLACING EMERGENCY LIGHT TO THE ARMED POSITION. REMOVED AND REPLACED #1 EMERGENCY BATTERY AND #2SDR DXTA2023020179610None · noneCABIN EMERG LIGHT: DURING CRUISE WITH EMER LT SWITCH IN ARM POSITION, ALL CABIN EMER LIGHTS BEGAN FLASHING. TURNED EMER LT SWITCH TO OFF POSITION FOR A FEW SECONDS AND TURNED IT BACK TO ARM POSITION. CABIN EMER LIGHTS REMAINED CONTINUOUSLY FLASHING UNTIL SHUT SDR DXTA2022112874810Light · inoperativeEMERGENCY WHITE LIGHT BY SEAT 3 HAS FALLEN OUT OF ITS HOLDER. THE LIGHT STILL FUNCTIONS. SECURED FLOOR EMERGENCY WHITE LIGHT ASSY. NEAR #3 SEAT IN REF TO AMM 33-52-11SDR DXTA2021100449770Battery · defectiveCABIN EMER LIGHT: EMERGENCY LIGHTS REMAIN ON IN THE ARMED POSITION // SIGNOFF // INSTALLED K-BALLED EMER BATT P/N:7450LS-00 S/N:005549 FROM A/C N353QS A/C S/N:50500263 A/C TIME: 5,032.5 A/C CYCLES: 3947. WORK DONE IAW PHENOM 300 AMM 32-52-01-01. PERFOMED SATISSDR DXTA2021081346850Adc · defectiveFIRST OFFICER AIRSPEED INDICATION: SHORTLY AFTER TAKEOFF WE HAD AN IAS FLAG. WHEN ATTEMPTING TO PUT AUTOPILOT ON, WE GOT AUTOPILOT FAIL, YD FAIL, SWPS FAULT, AND VENTRAL RUDDER FAIL. UNRELIABLE AIRSPEED ENSUED. RETURNED TO AIRPORT. UPON LANDING, NOTICED BUSDR JGVR202011111001Counterbalance · damagedWHILE COMPLYING WITH EMBRAER SB 505-55-0004 FOUND THE FOLLOWING FLIGHT CONTROL BALANCE WEIGHTS NOT ACCEPTABLE AND REQUIRING REPLACEMENT: RT ELEVATOR (10 ADJUSTABLE BALANCE WEIGHTS P/N PE915109-L33), RT ELEVATOR (BALANCE WEIGHT HORN P/N PE915109-L42), RT ELEVATSDR DXTA2016010406153Precooler · odorIN FLIGHT DURING INITIAL CLIMB OUT, THERE WAS A CABIN ODOR PRESENT THAT SMELLED OF BURNING RUBBER. ODOR WAS STRONG & PERSISTED THROUGHOUT FLIGHT & THE RETURN TO AIRPORT. ODOR SEEMED STRONGER IN CABIN. REPLACED SEPARATED PRECOOLER WITH NEW UNIT IAW MM 34-11-
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
Earlier aircraft with this N-number · 1
This aircraft carried N351QS before the one registered now. The FAA can assign a mark to another aircraft once a registration is cancelled.