- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500268
- Year built
- 2015
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- April 30, 2015
- Certificate issued
- March 30, 2026
- Expires
- March 31, 2033
- Mode S code
- A42405
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 N366QSMatched 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 N366QSMatched 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 · 13
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025030502561Concentrator · defectiveCENTRAL WARNING SYSTEMS: AT 40,000 RECEIVED GOLDEN CASS MESSAGE GSD1 FAIL WITH MANY OTHER CASS MESSAGES. ALSO, RECEIVED A DATA PATH HAS FAILED IN THE GTC. LASTLY, GEAR INDICATION SYSTEM SHOWED DISAGREE FOR THE LEFT MAIN. PULLED LANDING GEAR EMERGENCY HANDLESDR DXTA2025011501943Light · malfunctionedCABIN EMERGENCY LIGHTS FLASHING IN FLIGHT WITH THE EMER LT SWITCH IN ARM. THE LIGHTS STOPPED FLASHING WHEN WE TURNED THE SWITCH OFF. REPLACED BATTERY. OPS CHECK GOOD. IAW AMM 33-35-01SDR DXTA2024090500416Shimmy Dampener · defectiveRIGHT SEAT, RIGHT RUDDER PEDAL REQUIRES EXCESSIVE PRESSURE FOR A NORMAL CONTROL RESPONSE. MORE THAN NORMAL PRESSURE IS REQUIRED AT TAXI SPEEDS, EXCESSIVE PRESSURE IS REQUIRED AT TAKEOFF AND LANDING SPEEDS. THE PLANE PULLS TO THE LEFT ON TAKEOFF AND LANDING WITSDR DXTA2024081500198Battery Pack · malfunctionedEMERGENCY LIGHTS IN CABIN WERE FLICKERING WHILE TAXIING INTO FBO RAMP. AFTER SHUTDOWN, WE MOVED THE EMERGENCY-LIGHTS SWITCH TO ARM AND ALSO ON POSITIONS AND THE CABIN EMERGENCY LIGHTS FLICKERED IN BOTH POSITIONS. POWERED UP ACFT, MOVED EMERGENCY LIGHTS SWITCHSDR DXTA2024022210976Indicator · fodON POSTFLIGHT, DISCOVERED THE LOWER RIGHT MAIN CABIN DOOR LOCK INDICATOR GREEN FLAG IS NO LONGER VISIBLE THROUGH THE LOCK VISOR. THERE IS A SILVER BLANKET/TAPE MATERIAL INSIDE THE DOOR THAT HAS BEEN BEGINNING TO PARTIALLY OBSTRUCT VIEW OF THE LOCK FLAG. IT IS SDR DXTA2023071891210Unknown · defectiveCOMM 1 FAILED WITH VERY DISTINCTIVE ELECTRICAL ODOR IN FLIGHT. EVERY TIME YOU PUSHED TO TALK A YELLOW X WOULD APPEAR OVER COMM 1 IN BOTH GTCS ALONG WITH ELECTRICAL BURN SMELL. IT APPEARED THE SMELL ONLY HAPPENED WHEN YOU PRESSED PTT COMM 1. COMM 2 WORKED NORSDR DXTA2023051085770Unknown · unknownEMERG EXIT SIGN/LIGHT: EMERGENCY "EXIT" SIGN OVER MAIN CABIN DOOR (ON CEILING). THE LEFT HALF OF THE LIGHT CLUSTER IS NOT WORKING (LOOKING FROM BOTTOM OF STAIRS, UPWARD. REMOVED AND REPLACED OVERHEAD EMERGENCY EXIT SIGN IAW EMB-505 MM CHAP 33-52-09. OPS CHESDR DXTA2022112874910Battery Pack · failedDURING FLIGHT CABIN EMERGENCY LIGHTS STARTED FLICKERING AND CONTINUED TO DESTINATION. THEY GOT MUCH DIMMER BY THE TIME OF LANDING. C/W FIM 488S-33-50-00-8 I 0-802. AN INCORRECT FUNCTIONING OF THE EMERGENCY LIGHTS, FLICKER OR BLINKING. FOUND EMERGENCY BATTERSDR DXTA2022102472670Battery Pack · disconnectedEMERGENCY LIGHTS REMAIN ILLUMINATED WITH EMERGENCY LIGHT SWITCH IN THE ARM POSITION. ACCESS FWD AND AFT EMERGENCY BATTERIES FOR TROUBLESHOOTING. NOTED WITH THE FWD BATTERY CONNECTED AND THE AFT BATTERY DICONNECTED AND THE SWITCH IN THE ARM POSITION THE LIGHTSSDR DXTA2021061043460Unknown · noiseEMERGENCY EXIT DOORS: LOUD HUMMING NOISE HEARD IN THE CABIN DURING CRUISE FLIGHT AT FL290. THE NOISE STARTED AROUND 270K AND WAS CONSTANT AT SPEEDS ABOVE THAT. THE NOISE STOPPED WHEN THE SPEED WAS REDUCED TO 230K. UPON INSPECTING THE CABIN WE SUSPECT THE SOUNDSDR 2020FA0000376Balance Weight · corrodedDURING ACCOMPLISHMENT OF EMBRAER SB 505-55-0004 REV 01 (DATED 06/24/2020), WE NOTED THE FOLLOWING LEFT ELEVATOR MASS BALANCE WEIGHT BELOW TOLERANCE: P/N PE915109-L33 (1 EACH) UNDER THE WEIGHT LIMITS (81 GRAMS), AS PRESCRIBED BY THE SB (MINIMUM 84 GRAMS). THE SDR DXTA2019021802035Uplock · contaminatedLOUD BANG WHEN SELECTED DOWN AND 8-10 SECONDS FOR GREEN INDICATION. BLED THE AIR FROM THE LANDING GEAR UPLOCK BOXES. CHECKED & ADJUSTED HYDRAULIC ACCUMULATOR NITROGEN CHARGE REDUCING PRECHARGE PRESSURE. PERFORMED FUNCTIONAL CHECK ON THE LANDING GEAR EXTENSSDR DXTAT2PL6D005FW9UUnknown · odorDURING CRUISE FLIGHT, A STRONG ODOR WAS PRESENT PRIMARILY IN THE COCKPIT. THE ODOR IS MOST NOTICEABLE WHEN THE AIR SYSTEM IS CALLING FOR AN INCREASE IN TEMPERATURE. COMPLIED WITH FIM 21-20-00, WITH NO DEFECTS NOTED AT THIS TIME. OK TO RELEASE AT THIS TIME.
Reports on N366QS not matched to an aircraft · 12
They name N366QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2010030104008Brake · weakBOTH CO-PILOTS SIDE BRAKES ARE SOFT. INSPECTED COPILOTS PANELS ATTACHING POINTS, MASTER CYLINDERS, LINES AND FITTINGS NO DEFECTS NOTED AT THIS TIME BLED BRAKES IAW MM CH 32-42-00 OPS CHECKS SATISFACTORY.SDR DXTA09F00143Indicator · failedDURING CLIMBOUT AT APPROX 16,000' LT OIL TEMP GAUGE DROPPED TO ZERO ANDS THEN RETURNED TO NORMAL NUMEROUS TIMES. AFTER LEVELING AT 23,000' THE GAUGE DROPPED TO ZERO AND REMAINED THERE UNTIL DESCENDING THROUGH ABOUT 17,000'. GAUGE WAS NOMAL AFTER THAT.SDR DXTA2009113003871Switch · malfunctionedON TAKEOFF ROLL, PWR APPROX 80-90 PERCENT, LT THRUST REVERSER ARM AND UNLOCK LIGHT CAME ON. AS WE TAXIED IN, FULL T/R DEPLOYMENT ON LT SIDE; EMER SWITCH STOWED T/R. REENABLED T/R SYS. CYCLED T/R'S AND DUPLICATED MALFUNCTION. GAINED ACCESS TO THROTTLE GUARD.
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