- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500356
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- June 28, 2016
- Certificate issued
- March 23, 2026
- Expires
- March 31, 2033
- Mode S code
- A48F5D
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 N393QSMatched 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 N393QSMatched 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 · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025122606275Brake Assy · weakWHILE AT TAXI SPEED BRAKES BECOME SPONGY AND REQUIRES A LOT MORE PRESSURE TO STOP. BRAKES ACT NORMALLY DURING LANDING. PERFORMED BRAKE BLEED, PERFORMED TAXI RUN WITH SUCCESS,REF EMB505 AMM 32-40-00SDR DXTA2025012202059Handle · defectiveWHILE CLOSING MAIN DOOR, OUTSIDE DOOR HANDLE BROKE OFF. CORRECTIVE ACTION: REPLACED DOOR HANDLE. OPS CHECK GOOD. IAW EMB-505 AMM 52-11-24SDR DXTA2024121101427Battery · faultedAFTER DEPARTURE ENROUTE WE SHUT OFF THE CABIN LIGHTS AND NOTICED THAT THE EMERGENCY LIGHTS STAYED ON. IF WE SELECT THE EMER LIGHTS TO OFF THEY WILL GO OUT BUT COME BACK ON WHEN WE SELECT THEM TO ARM. REMOVED FWD AND AFT EMERGENCY LIGHTS AND REPLACED BOTH IAW PSDR DXTA2024071612361Control Unit · defectiveBRAKES PULSATING ON LANDING &TAXI. PER CRC RECOMMENDATION, PERFORMED A VISUAL INSP OF BRAKE SYS & NO FAULTS. BLED HYD SYS. CHECKED & FOUND HYD SYS PROPERLY SERVICED. PERFORMED INCOMING PART CHECK & FOUND THE BCU RECEIVED WAS THE WRONG P/N REQUIRED. CONTACTEDSDR DXTA2024052311844Shutoff Valve · faultedRECEIVED ECS VALVE FAIL MESSAGES, FOLLOWED THE QRC, AND DURING DESCENT RECEIVED CAB ALTITUDE HI MESSAGE, WHICH RESULTED IN 1 SET OF PAX MASKS DROPPING IN THE CABIN. REMOVED FAULTY RH FCSOV, P/N 1300250-11, S/N 1643, INSTALLED MODIFIED RH FCSOV, P/N 1300250-11SDR DXTA2023080892520Unknown · unknownON ROTATION CAPTAINS YOKE MADE A CLUNK AND IS LOOSE. FOUND PILOT'S YOKE SUPPORT LOOSE. REMOVED AND REPLACED PILOT'S VOICE SUPPORT NUT AND WASHERS. REF AMM 27-01-01-400-801-A, AND 27-40-00-710-801-A. OPS CHECK GOOD. NO DEFECTS NOTED.SDR DXTA2023052286860Control Module · defectiveRIGHT MLG BRAKE: REPEAT WRITE-UP. ON LANDING AND TAXI IN, A NOTICEABLE BRAKE PULSE OR OSCILLATION. MOST NOTABLE FROM 80 KTS DOWN TO ABOUT 20 KTS. NOT SURE IF ITS LEFT OR RIGHT SIDE, MOST PROBABLY BOTH SIDES, AS THERE IS NO PULLING TO ONE DIRECTION. R & R BRASDR DXTA2022060963560Battery · defectiveCABIN EMERG LIGHT: AFTER LANDING AND SHUT DOWN THE EMERGENCY LIGHTS STAYED ON. TRIED TURNING THE BATTERYS ON AND RECYLED THE THE SWITCH AND BEFORE WE TRYED THE SWITCH WITH THE BATTERYS ON THE LIGHTS WENT OUT SO TURNED BATTERYS OFF AND THEY WENT BACK ON. LIGHTSSDR DXTA2021122754100None · defectiveEMERGENCY LIGHTING: ALL OF THE EMERGENCY LIGHTS ILLUMINATE IN BOTH THE ARM AND ON POSITION WITH AIRCRAFT POWER AVAILABLE. THE LIGHTS WILL SHUT OFF IF THE EMER LT SWITCH IS IN THE OFF POSITION. THE LIGHTS WILL COME BACK ON WHEN THE SWITCH IS MOVED BACK TO THE ASDR DXTA2021021204724Battery Pack · defectiveEMERGENCY LIGHTS BATTERY: EMERGENCY EXIT LIGHTS BEGAN FLASHING IN FLIGHT. FLASHED ON/OFF FOR THE LAST 10 MINUTES OF FLIGHT. LIGHT SWITCH WAS IN ARM POSITION.///SIGN-OFF/// REMOVED AND REPLACED EMERGENCY BATTERIES IAW EMB AMM 33-52-01 CHECKED GOOD.SDR DXTA202101054560Light · inoperativeEMERGENCY EXIT LOWER SIGN DOES NOT ILLUMINATE. REMOVED COVERS AND LAMP ASSEMBLY. CHECKED WIRING AND SWAPPED POSITIONS WITH THE FWD LAMP ASSEMBLY. BOTH LAMPS ARE WORKING IN THE SWAPPED POSITION, REF THE EMB 505 AMM 33-00-00.SDR DXTA2019011501913Warning System · false activationSWPS FAULT YELLOW CAS ILLUMINATED - DURING INITIAL DESCENT FROM CRUISE FLIGHT, WE HAD MULTIPLE CAS FAIL AND FAULTS LIGHTS INCLUDING PTRIM BKP FAIL, SWPS FAULT, TRIM FAIL, SPOILER FAULT. AS WELL, NO MATTER THE SPEED, THE AIRCRAFT WAS INDICATING A FLASHING MAXSP
Reports on N393QS not matched to an aircraft · 19
They name N393QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA200811253373Throttle · out of rigDURING SPEED BRAKE CHECK, WHEN LT THROTTLE WAS BROGHT FWD AND RETURNED TO IDLE, ENGINE ROLLED BACK AND SHUT DOWN. RIGGED THROTTLE LINKAGE AND RAN ACFT STILL SHOT DOWN PERFORMED COMPLETE RIG ON THROTTLE, SAME AS NEW ENGINE INSTALL RAN ACFT TRIED SEVERAL TIMES SDR DXTA2008112603373Engine · shutdownDURING SPEED BRAKE CHECK, WHEN LT THROTTLE WAS BROUGHT FWD AND RETURNED TO IDLE, ENGINE ROLLED BACK AND SHUTDOWN.SDR DXTA2008111003343Brake Sys · malfunctionedAT END OF LANDING ROLL OUT RIGHT SEAT PILOT LOST BRAKE PRESSURE WITH PEDALS PRESSED 3/4 THROW. RELEASED BRAKES AND REAPPLIED WITH SAME RESULT (NO BRAKING). WHILE PRESSED THIS SECOND TIME BRAKE KICKED IN AFTER A ONE TO TWO SECOND DELAY AND THEN FUNCTIONED NOR
See all 19 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