- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500201
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- March 26, 2014
- Certificate issued
- July 17, 2024
- Expires
- July 31, 2031
- Mode S code
- A3AD88
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 N336QSMatched 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 N336QSMatched 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
Service difficulty reports · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026081709286Downlock Sensor · damagedGEAR SELECTED UP AFTER T/O. LG LEVER DISAG. NLG INDICATED RED DASHED BOX. SELECTED GEAR DOWN PER QRH AND HEARD A SHORT GRINDING NOISE IN NLG. LANDED NORMALLY. REMOVED DAMAGED NLG DOWN LOCK SENSOR P/N 80-057-01 S/N 35254 AND INSTALLED NEW SENSOR IAW AMM 32-SDR DXTA2023120410227Battery · inoperativeDURING FLIGHT, EMERGENCY LIGHTS OVER THE DOORS AND THREE CENTER AISLE OVERHEAD LIGHTS BEGAN FLICKERING WITH THE SWITCH IN THE ARM POSITION. REMOVED FORWARD EMERGENCY BATTERY AND INSTALLED TESTED EMERGENCY BATTERY. REMOVED AFT EMERGENCY BATTERY AND INSTALLEDSDR DXTA2023040583730Unknown · unknownMLG BRAKE PRESSURE: HAVING TO APPLY ASYMMETRICAL BRAKING ON LANDING. LEFT SIDE LOWER THAN RIGHT DURING BRAKING. MX TEAM COMPLETED THE SERVICING OF HYDRAULIC RESERVOIR EMB505 AMM 12-13-00 AND ADDED 2 QUARTS OF HYDRAULIC FLUID. STARTED R/H ENGINE AND EXCISED TSDR 2020FA0000426Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SB 505-55-0004 REV 01 (DATED 06/24/2020), WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (3 EACH BELOW MINIMUM OF 84G); HORN MASS WEIGHT PART NUMBER PE915SDR JGVR20200129001Balance Weight · corrodedDURING COMPLIANCE OF SERVICE BULLETIN 505-55-A004 REV 5 MASS BALANCE AND ATTACHMENT PARTS - (INSPECTION, CORROSION FOUND ON ALL BALANCE WEIGHTS. WEIGHTS WERE CLEANED AND TREATED PER SB INSTRUCTIONS. NO FLIGHT CONTROL WEIGHT CHANGES AT THIS TIME.SDR DXTA2019121983222Warning Message · false indicationFOLLOWING CAS MSGS ILLUMINATED IN FLIGHT: SWPS FAULT AMS CTRL FAIL AP FAIL YD FAIL GSD2 FAIL SWPS ICE SPEED HSDB FAULT//SIGNOFF// PERFORMED GSD 2 OPERATIONAL CHECK AS PER AMM MPP 31-41-01- 710-801-A AND PERFORM FIM 31-42-00-810-812-A - FAILURE OF THE HSDB BETWSDR DXTA2018012500512Unknown · odorCOCKPIT ODOR DURING CLIMB OUT. PERFORMED VISUAL INSPECTION FOR ANY WET INSULATION BLANKETS AND SURROUNDING AREA AROUND LAV, NO DEFECTS NOTED. RAN ENGINES FOR 1 HOUR CHANGED POWER LEVELS TO TRY AND DUPLICATE ODOR. NO DEFECTS NOTED, ALL WORK PERFORMED IAW MM SDR DXTA2015061606032Brake · fireAFTER LANDING, DURING SPEED & NORMAL BRAKING, WHEN SETTING PARKING BRAKE AT TERMINAL, GND PERSONNEL REPORTED RT FRONT BRAKE ON FIRE. BEFORE FIRE BOTTLE ARRIVED FIRE WAS OUT. FRONT PAD LOOKS TO BE SINGED. NO EXCESSIVE HEAT FELT ON BRAKES. REMOVED RT MLG WH
Reports on N336QS not matched to an aircraft · 21
They name N336QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2010020103963Pedal · bindingON LANDING WHILE APPLYING BRAKES, PEDALS SEEMED SOLID INITIALLY, THEN THERE WAS ADDITIONAL TRAVEL TO MAINTAIN THE SAME BRAKING. WHEN THE BRAKE PEDALS WERE RELEASED, THE LT PEDAL IS BINDING AND A LOUD "SNAPING" SOUND IS HEARD AND FELT. R & R RUDDER PEDAL BRACSDR DXTA2009120103876Control Valve · overheatedWINDSHIELD O'HEAT ANNUNCIATOR CAME ON IN FLIGHT WHILE WINDSHIELD HEAT WAS ON, -20ºC RAT. ANNUNCIATOR DID NOT EXTINGUISH AUTOMATICALLY AND WAS ACCOMPANIED BY BURNING ODOR. BOTH WERE RESOLVED WHEN WINDSHIELD HEAT WAS TURNED OFF. REPLACED TEMPERATURE CONTROL VASDR DXTA2009092803799Brake Assy · malfunctionedBRAKES SPONGY AT HIGH SPEED ROLL OUT AND PULL LEFT AS YOU INCREASE PRESSURE. WHEN AC REACHES 30 KTS & SLOWER BRAKES GRAB AS IF ANTI-SKID IS WORKING. BLED BRAKES AS REQUIRED IAW MM 32-42-08. ALSO CHECKED BOTH LT AND RT WHEEL SPEED TRANSDUCERS WITH NO DEFECTS
See all 21 unmatched reportsSTCs 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