- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500730
- Year built
- 2023
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- June 16, 2023
- Certificate issued
- September 4, 2026
- Expires
- September 30, 2033
- Mode S code
- A59B0A
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 N460QSMatched 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 N460QSMatched 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 · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026082509414Warning Message · false activationRAM AIR FAIL WHITE CAS ILLUMINATED WITH ASSOCIATED YELLOW X OVER THE RAM AIR VALVE ON ECS SYNOPTIC. CAS MESSAGE APPEARED INTERMITTENTLY 4 TIMES DURING THE DESCENT BETWEEN FL430 AND FL280. COMPLIED WITH SEVERAL OPERATIONAL CHECKS OF THE RAV WITH NO DISCREPANCISDR DXTA2026010906453Actuator · faultedAT FL430 THE PTRIM NML FAIL AMBER CAS MESSAGE PRESENTED (PICTURE ATTACHED). THE PITCH TRIM INDICATOR ON THE MFD INITIALLY HAD AN AMBER X AND THEN CLEARED. THE CAS MESSAGE REMAINED SUSTAINED THROUGH THE REMAINING PHASES OF FLIGHT. WE COMPLIED WITH THE QRH PROCESDR DXTA2025081804625Control Unit · faultedLEFT & RIGHT MAIN GEAR BRAKES ARE INOPERATIVE. ON INITIAL BRAKE CHECK, BRIEFLY LOCKED. ON TAXI, THE BRAKES CHATTER LOUDLY & ARE INEFFECTIVE. BRAKES FULLY APPLIED GIVE VERY WEAK CHATTERING BRAKING. TECHS PERFORMED CMC AND CVDR DOWNLOAD ADDED ON THE SHARE POSDR DXTA2025081404584Battery Pack · defectiveEMERGENCY LIGHTS STAY ON WHEN SWITCH IS IN THE ARM POSITION, AIRCRAFT ON THE GROUND TRIED WITH GPU CONNECTED AND GPU DISCONNECTED. CORRECTIVE ACTION: REPLACED #1 AND #2 EMERGENCY LIGHTING BATTERY OPS CHECK GOOD WORD DONE IAW EMBRAER EMB-505 AMMSDR DXTA2025052703590Rudder · faultedWHILE IN FLIGHT VENTRAL RUDDER FAIL WHITE CAS MESSAGE POSTED. WE RAN THE CHECKLIST. IT EXTINGUISHED BEFORE LANDING. CORRECTIVE ACTION: PERFORMED OPERATIONAL CHECK OF THE VENTRAL RUDDER IAW PHENOM 300 AMM 27-26-01-710-80-A WITH NO DEFECTS NOTED. CAS MESSAGE NESDR DXTA2025051403458Brake · malfunctionedMLG BRAKE PRESSURE: WHILE PREFLIGHTING THE AIRCRAFT WE MOTORED THE ENGINES TO CHECK OIL AND ADD PRESSURE TO THE BRAKE SYSTEM. AFTER ENGINE START WE TARTED TO TAXI AND RECEIVED A BRK FAIL AND HAD NO BRAKING ACTION WITH THE RUDDER PEDALS. HAD TO USE EMERGENCY BRSDR DXTA2023092996780Unknown · unknownVIOLENT SHUDDER WHEN BRAKES APPLIED ON RIGHT BRAKE. PERFORMED TAXI & MULTIPLE BRAKE CHECKS, NO ABNORMAL GRABBING, CHATTERING, OR NOISES, AIRCRAFT IN HANGAR, REMOVED MAIN WHEELS, INSPECTED & CLEANED LT & RT BRAKES. INSPECTED BRAKE PIN LENGTH, BRAKES ARE NOWHERSDR DXTA2023082193480Unknown · unknownMAIN DOOR: MAIN ENTRY DOOR IS VERY DIFFICULT TO OPEN OR CLOSE. WITH DOOR OPEN, MECHANISM WORKS SMOOTHLY, BUT WHEN CLOSING OR OPENING DOOR IT BINDS AND GET VERY DIFFICULT // SIGNOFF// FOUND DOOR PINS TO HAVE THE WRONG TYPE LUBRICANT(DRY FILM) ON THEM. CLEANED D
Reports on N460QS not matched to an aircraft · 14
They name N460QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 2013F00126Rod End · damagedR & R FLIGHT SPOILER PUSHROD END ASSY IAW CB 203. PART DETERMINED TO NO LONGER BE SERVICABLE, PN 1159CM20263.SDR 2013F00125Fitting · corrodedWHILE REMOVING BOLT FROM RT FLAP TRACK FITTING, FOUND THE UPPER FITTING TO HAVE EXTREME CORROSION ON INBD FACE OF FITTING.SDR DXTA2010122004369Hydraulic System · warning lightAFTER APPROX 50 MINUTES IN FLT, DURING CRUISE AT FL 380, AMBER HYD QTY LOW CAS ILLUMINATED. HYD PAGE QTY SHOWED COMBINED QTY JUST ABOVE LOW MARK. OVER THE NEXT 50 MIN IT SLOWLY DECREASED BELOW THE LOW MARK & WENT FROM WHITE TO RED. DURING APPROACH & LANDING,
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