- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500273
- Year built
- 2015
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- June 1, 2015
- Certificate issued
- August 4, 2026
- Expires
- August 31, 2033
- Mode S code
- A427BC
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 N367QSMatched 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 N367QSMatched 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
Reports on N367QS not matched to an aircraft · 1
They name N367QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another 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 DXTA2026010506415Door · faultedMED INTERIOR RED HANDLE DOES NOT EASILY GO TO THE FULL OPEN POSITION. IT MUST BE FORCED TO THE FULL OPEN POSITION AFTER THE DOOR IS DOWN OR ELSE THE 2 PINS CLOSEST TO THE HINGE WILL DRAG OR CATCH. PERFORMED GVI OF THE RED HANDLE, NO DEFECTS NOTED. UNABLE TO DSDR DXTA2026010206415Handle · bindingMED INTERIOR RED HANDLE DOES NOT EASILY GO TO THE FULL OPEN POSITION. IT MUST BE FORCED TO THE FULL OPEN POSITION AFTER THE DOOR IS DOWN OR ELSE THE 2 PINS CLOSEST TO THE HINGE WILL DRAG OR CATCH.SDR DXTA2025120806001Battery Pack · inoperativeEMERGENCY LIGHTS TURN ON WHEN ARMED, & FLICKER IN FLT. REPLACED BOTH EMERGENCY LIGHT BATTERY PACKS DUE TO NOT HOLDING CHARGE & OPS CHKD GOOD IAW AMM 33-52-01.SDR DXTA2024071112327Battery · defectiveEMER LIGHTS FLASH CONTINUOUSLY IN ARM POSITION. PERFORMED T/SHOOTING FOUND AFT CABIN(LAV AREA) EMERGENCY BATTERY INOP, MCC REQUESTED TO R/R BOTH EMER. BATTERY. REMOVED ANO REPLACED FWD ANO AFT CABIN EMERGENCY BATTERY WITH CUSTOMER SUPPLIED NEW PARTS, PERFORMESDR DXTA2023101197670Shutoff Valve · faultedDURING CRUISE AT FL410 HAD EMER BRK LO PRESS YELLOW CAS MESSAGE. ACCUMULATOR PRESSURE BLED DOWN SLOWLY FROM 1600 PSI UNTIL APROX 1100 PSI THEN DROPPED TO 100 PSI & STAYED FOR THE REMAINDER OF FLT. ACCOMPLISHED QRH & LANDED NORMAL, NO ISSUES. AFTER TOUCHDOWN, NSDR DXTA2022081668140Battery · defectiveCABIN EMERG LIGHT: WHEN EMER LT SWITCH IS MOVED FROM THE OFF TO THE ARM POSITION, FOR ENGINE START, LIGHTS REMAIN ILLUMINATED FOR ABOUT 5 MINUTES BEFORE EXTINGUISHING.//CORRECTIVE ACTION//REMOVED THE FAILED FWD EMERGENCY BATTERY AND INSTALLED A NEW EMERGENCY BSDR 2020FA0000496Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SERVICE BULLETIN 505-55-0004 REV 01 (DATED 06/24/2020) WE NOTED THE FOLLOWING MASS BALANCE WEIGHTS BELOW TOLERANCE AT LEFT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (10 EACH BELOW MINIMUM OF 84G), HORN MASS WEIGHT PSDR DXTA2020080503940Electronic Unit · faultedCRUISE FLIGHT FL360, GOT THE FOLLOWING: SWPS FAULT EICAS, FLAP FAIL EICAS, PTRIM BKP FAIL EICAS, SPOILER FAULT WHITE EICAS. YELLOW X'S DISPLAYED IN FLAP INDICATOR AND TRIM INDICATOR ***CORRECTIVE ACTION*** UPON POWER-UP AND SETTING PITCH TRIM TO NORMAL, PITCSDR 2018FA0000491Control Cable · chafedDURING INSPECTION IT WAS FOUND THAT THE LH AND RH AFT UPPER SECTION OF RUDDER CABLES WERE CHAFED BEYOND LIMITS. IT WAS NOTED THAT THE CHAFING IS HAPPENING AT THE FAIRLEADS/CABLE SUPPORTS. THE CABLE TENSION IS 5 LBS SO THE CABLES LAY ON THE FAIRLEADS, THEREFORESDR 2019F00019Support · crackedDURING SCHEDULED MAINTENANCE IT WAS NOTED THAT LEFT HAND ADJUSTABLE RUDDER TORQUE TUBE SUPPORT ROD WAS FOUND TO HAVE A 2 INCH LONGITUDINAL CRACK (SEPARATED). AFTER CLOSER EVALUATION IT SEEMS THAT WATER INTRUSION WAS THE ROOT CAUSE, THE WATER SEEMED TO HAVE FROSDR DXTA2016090606297Brake Assy · contaminatedAIRCRAFT PULLS TO THE LT WHILE APPLYING BRAKES. BIRD REMAINS DISCOVERED IN BRAKE FROM THE BIRD STRIKE THIS WORK ORDER. REMOVED BIRD REMAINS FROM AROUND BRAKE AREA. CLEANED WHEEL AND BRAKE AS NEEDED. TAXIED ACFT ON RAMP AND PERFORMED SEVERAL BRAKE CHECKS. SDR DXTA2016062406261Valve · inoperativeNR 1 DUCT OVERTEMP MESSAGE APPEARED WHILE LEVELING AT FL400. CREW PERFORMED QRH AND AFTER SWITCHING TO ECS 2, NR 2 DUCT OVERTEMP MESSAGE APPEARED. HAD BOTH NR 1 AND 2 OVERTEMP MESSAGES ON SIMULTANEOUSLY. BOTH DUCT TEMPERATURES WERE VERIFIED OVER 200 DEGREES ON
Reports on N367QS not matched to an aircraft · 21
They name N367QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA200811193363Relief Valve · inoperativeAT GEAR RETRACTION, THE GREEN LIGHTS WENT OUT BUT THE RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED AND THE HYD PRESS LIGHT REMAINED ILLUMINATED. REPEAT WRITE UP. FOUND HYD SYS RELIEF VALVE OPENING AND REGULATING AT 1100 PSI. SHOULD BE 1500 PSI. REMOVED AND RESDR DXTA2008111903363Warning System · activatedAT GEAR RETRACTION, THE GREEN LIGHTS WENT OUT BUT THE RED GEAR UNLOCKED LIGHT REMAINED ILLUMINATED.SDR DXTA200811173362Pivot · lack of lubeON LANDING ROLL RT THRUST REVERSER UNLOCKED BUT WOULD NOT DEPLOY, TRIED AGAIN ON TAXI & NO DEPLOY. ON THE THRUST REVERSER CHECK PRE-FLT, DEPLOYED. ACTUATED THRUST REVERSERS SEVERAL TIMES. THRUST REVERSER DEPLOYED & LIGHT ILLUMINATED. INSPECTED THRUST REVERSER
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