- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500389
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- December 16, 2016
- Certificate issued
- September 5, 2025
- Expires
- September 30, 2032
- Mode S code
- A4B57E
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 N402QSMatched 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 N402QSMatched 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 · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026092509835Strut · dischargedDURING GEAR RETRACTION AFTER TAKEOFF, THE NOSE GEAR INDICATED IN TRANSIT AND NEVER FULLY RETRACTED. LG LEVER DISAG CAS MESSAGE DISPLAYED. HYDRAULIC PRESSURE WAS NORMAL. ALL GEAR EXTENDED NORMALLY WHEN SELECTED DN. SERVICED NLG STRUT. OPS CHECK GOOD. IAW PHENOSDR DXTA2024091300509Unknown · odorODORS IN COCKPIT / CABIN: IN FLIGHT PIC SMELLED FUMES RESEMBLING BURNING RUBBER, BUT SIC COULD NOT SMELL IT. THE SMELL PASSED, BUT RE-APPEARED ON ARRIVAL INTO KTEX STRONGER THAN BEFORE. UPON LANDING A VERY STRONG SMELL OF FUMES RESEMBLING BURNING RUBBER/WIRES SDR DXTA2023051686230Unknown · unknownSTRONG MUSTY ODOR LIKE WET SOCK WHEN AIR-CONDITIONING TURNED ON. REMOVED AND REPLACED THE FWD EVAPORATOR UNIT AND THE RECEIVER DRYER ASSY WITH NJA SUPPLIED NEW PARTS. SUCCESSFUL OPERATIONAL CHECKS/ FUNCTIONAL CHECKS WERE PERFORMED. REF. EMBR-505 AMM 21-52-03,SDR DXTA2023020780090Not Reported · not reportedNLG: UPON RETRACTION AFTER LIFTOFF MAIN GEAR CAME UP AND LOCKED, NOSE GEAR DID NOT FULLY RETRACT AND WE RECEIVED A RED/WHITE CHECKERED INDICATION ON NOSE GEAR LIGHT AS WELL AS RED MESSAGE "LDG LEVER DISAGREE" WE FOLLOWED THE CHECKLIST FOR GEAR ISSUES AND ITSDR DXTA2021112952570Warning Message · false activationAFTER LEVEL-OFF AT FL290, DUCT 1 OVERTEMP CAS MESSAGE DISAYED. RAN THE QRH AND RETURNED AND LANDED WITH NR 1 ENGINE IDLED PER QRH. WE WERE ABLE TO SMELL THE HOT CONDITION IN. PERFORMED CMC DOWNLOAD AND SENT TO CONTACT CENTER FOR EVALUATION. CONTACT CENTER SUGSDR DXTA2021111251700Flap System · failedFLAP FAIL YELLOW CAS: FLAPS FAILED BETWEEN THE 1 AND 2 POSITION. PERFORMED OPERATIONAL CHECKS OF THE FLAP SYSTEM WITH NO DEFECTS NOTED PERFORMED OPS CHECKS WITH GPU & WHILE ENGINES RUNNING NEVER GOT FLAP FAIL CAS MESSAGE NOTIFIED MCC OF FINDINGS ORIGINAL CONSDR DXTA2021020104663Battery Pack · inoperativeIN FLIGHT, WITH EMER LTS IN THE ARM POSITION, ALL MAIN CABIN EMERGENCY LIGHTS ARE ILLUMINATED. ABOUT 50 MIN INTO THE FLIGHT AT FL400 THE CABIN EMERGENCY LIGHTS BEGAN TO FLICKER. REPLACED THE NO.1 AND NO.2 EMERGENCY LIGHT BATTERIES WITH TESTED UNITS IAW PHENOMSDR 2021FA0000018Balance 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 (12 EACH BELOW MINIMUM OF 84G), HORN MASS WEIGHT PSDR 2021FA0000017Balance 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 (12 EACH BELOW MINIMUM OF 84G), HORN MASS WEIGHT P
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