- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500483
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- October 18, 2018
- Certificate issued
- August 6, 2026
- Expires
- August 31, 2033
- Mode S code
- A51358
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 N426QSMatched 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 N426QSMatched 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 · 14
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2025120806026Battery Pack · inoperativeEMERGENCY LIGHTS WILL NOT ILLUMINATE WHEN SWITCH IS IN ON POSITION. CONTACTED MCC, THEY REQUESTED BOTH FWD AND AFT EMERGENCY BATTERIES BE REPLACED. GAINED ACCESS TO AIRCRAFT. REMOVED BOTH PILOT & CO-PILOT SEATS. REMOVED COCKPIT FLOOR PANEL 223CLF. R & R FWD SDR DXTA2025082904731Warning Message · illuminatedFLAP FAIL YELLOW CAS. CYCLED TWICE, SAME INDICATION AT 0. 3RD CYCLE FLAPS FUNCTIONED NORMAL. AFTER LANDING, FLAPS RETRACTED TO 0. POWERED ACFT. NO FAULT MESSAGES. PERFORMED FLAP ACTUATOR OIL LEVEL CHECK, ALL OIL LEVELS CHKED GOOD IAW MM 12-18-00-612-802-A. SDR DXTA2025060903780Control Unit · defectiveBRK FAIL YELLOW CAS: YELLOW BRAKE FAIL CAS MESSAGE APPEARED AFTER ENTERING A RUNWAY FOR TAKEOFF. BRAKES STARTING GRABBING THEN FAILED. I SLOWLY TAXIED OFF OF THE RUNWAY TO THE CLOSE BY TAXIWAY AND USED THE EMERGENCY BRAKE TO STOP CORRECTIVE ACTION: REMOVED ANDSDR DXTA2025021902399Handle · brokenTHE MAIN CABIN DOOR HANDLE BROKE RIGHT OFF THE DOOR. MAIN DOOR HANDLE: THE MAIN CABIN DOOR HANDLE BROKE RIGHT OFF THE DOOR. PICTURES ARE ATTACHED. REMOVED BROKEN HANDLE AND INSTALLED NEW HANDLE; COMPLETED OPS CHECK WITH NO DEFECTS NOTED, ALL WORK ACCOMPLISHED SDR DXTA2025013002159Cable · looseMAIN DOOR CABLE: TENSION ON MAIN CABIN DOOR IS LOOSE. WHEN OPENED, THE DOOR WILL TRY TO FALL COMPLETELY OPEN WITH LITTLE TO NO RESISTANCE. CORRECTIVE ACTION: MADE ADJUSTMENTS IAW AMM MPP TASK 52-10-00-820-804-A AND EMB-505 AMM 52-10-00. OPS CHECK GOOD.SDR DXTA2024061912093Door · leakingHIGH FREQUENCY VIBRATION & NOISE FROM RT OF FUSELAGE. EMERGENCY EXIT HANDLE RATTLES & EXIT DOOR NOISE. INSPECTED LATERAL SEAL FOUND LIFTNG ON BOTH LT & RT OF ACFT, APPLIED RTV ALONG LENGTH OF SEAL FROM AFT WING ROOF TO T/E WHERE FLAP SEAL STARTS. INSPECTED RT SDR DXTA2024012610734Battery · defectiveCABIN EMERG LIGHT: EMERGENCY LIGHTS BEGAN FLASHING 1.5 HOURS INTO THE FLIGHT. EMER LT SWITCH WAS IN THE ARM POSITION. REMOVED AND REPLACED FWD (1) AND AFT (2) EMERGENCY BATTERY SUPPLY'S OPS CHECK GOOD REF PHENOM 300 M/M 33-52-01.FWD P/N ON 7450LS-00 FWD S/NSDR DXTA2024011910663Battery · defectiveEMERG EXIT SIGN/LIGHT: DURING FLIGHT THE CABIN EMERGENCY LIGHTS AND SIGNS WERE FLASHING. THEY THEN WENT OFF AND REMAINED OFF. LATER THE EMERGENCY LIGHTS AND SIGNS AGAIN ILLUMINATED AND STAYED ON. LATER THEY WENT OFF AND REMAINED OFF FOR THE REST OF THE FLIGHT.SDR DXTA2022070765410Landing Gear · noisyNOSE GEAR: WHILE BEING VECTORED FOR THE APPROACH AT 3000 FEET A LOUD THUMP CAME FROM THE NOSE AREA. A BANG COULD ALSO BE FELT THROUGH THE FLOOR. THE NOISE AND VIBRATION ARE SIMILAR TO WHAT OCCURS DURING NORMAL GEAR RETRACTION. THE LANDING GEAR SWITCH WAS NOT MSDR DXTA2021051041740Vhf Comm · defectiveCOM1 VHF COMM: CREW EXPERIENCED A VERY BRIEF ELECTRICAL BURNING SMELL IN THE COCKPIT. SHORTLY THEREAFTER, FOUND THAT COM 1 WAS NOT TRANSMITTING, BUT WAS ABLE TO RECEIVE. COM 2 FUNCTIONED NORMALLY. VERIFIED THAT COM1 WAS NOT TRANSMITTING AND COM2 WAS WORKINGSDR DXTA030120213868Wire · chafedWHILE CLIMBING THROUGH 10K, TURN ON WINDSHIELD HEAT. RECEIVED AMBER WINDSHIELD FAIL 1 & 2 & SMELLED A BURNING ODOR. TURNED BOTH WINDSHIELD HEAT SWITCHES OFF & THE AMBER CAS MESSAGES WENT AWAY ALONG WITH THE BURNING ODOR. TURNED BOTH SWITCHES OFF THEN BACK OSDR 2021FA0000019Balance 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 RIGHT ELEVATOR: ADJUSTABLE WEIGHTS PART NUMBER PE915109-L33 (2 EACH BELOW MINIMUM OF 84G). ALL WEIGHTS HAS BESDR DXTA2020082004000Light · unknownIN FLIGHT THE EMERGENCY LIGHTS BEGAN FLASHING. COMPLIED WITH EMBRAER CONTACT CENTER RECOMMENDATION. POWERED UP AIRCRAFT AND NO DEFECTS NOTED WITH EMERGENCY LIGHTING. CHARGED FOR 30 MIN AND THEN DEPLETED BATTERIES FOR 60 MIN WITH NO DEFECTS. RECHARGED BATSDR DXTA2018122801842Unknown · malfunctionedNOSE GEAR WOULD NOT EXTEND. FOLLOWED CHECKLIST AND PERFORMED MANUAL EXTENSION. TOWER VERIFIED ON FLY BY THAT THERE WAS NO NOSE GEAR EXTENDED. "SUPPLEMENTAL INFORMATION" PERFORMED VISUAL INSPECTION OF NOSE GEAR, NOSE GEAR UPLOCK ASSY AND PROXIMITY SENSORS WITH
Reports on N426QS not matched to an aircraft · 21
They name N426QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTAT2PL6D0059ZEUValve · failedFUEL COCK WOULD NOT GO OFF ON RIGHT ENGINE. SEVERAL ATTEMPTS FAILED. AFTER TROUBLESHOOTING FUEL COCK HANDLE NOT SHUTTING OFF ON RIGHT ENGING. FOUND OPERATING LEVER ON HIGH PRESSURE FUEL SHUT OFF VALVE LOCKING UP. REMOVED RT ENGINE GIGHT PRESSURE FUEL SHUTOFFSDR G02R20170322004Hinge · corrodedLEFT ELEVATOR NR 4 HINGE HAS CORROSION IN BOLT BORE.SDR G02R20170322003Attach Fitting · corrodedNR 4 ELEVATOR ATTACH POINT ON HORIZONTAL STABILIZER HAS CORROSION IN BORE.
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