- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500507
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- March 6, 2019
- Certificate issued
- March 27, 2026
- Expires
- March 31, 2033
- Mode S code
- A52844
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 N431QSMatched 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 N431QSMatched 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 · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026091409664Brake · abnormalRIGHT MLG BRAKE: RIGHT BRAKE PULSATES NOTICEABLY AT ALL SPEEDS (MOST NOTICEABLE AT TAXI SPEED) WHEN BRAKE PEDAL PRESSURE APPLIED. DURING TAXI BRAKE APPLICATION, THE BRAKES CONSTANTLY GRABBED AND RELEASED. THIS PROCEEDED TO GET WORSE AS AIRCRAFT SLOW SPEED CAUSSDR DXTA2025090404815Lever · faultedFLAP FAIL, CAS MESSAGE ILLUMINATED ATTEMPTED RESET PROCEDURE PER THE CHECKLIST UNSUCCESSFULLY. LANDED ZERO FLAPS UNEVENTFULLY. COULD NOT DUPLICATE FLAPS FAIL CAS MESSAGE. PER CONTACT CENTER PREFORMED A GVI OF FLAPS.FLAP ROLLERS, FLAP TRACKS AND FLAP WELLS SDR DXTA2025060203678Unknown · odorREPEAT X3 WRITE UP. STRONG MOLD ODOR AFTER ENGINE START AND PROGRESSED DURING FLIGHT. ODOR EXTREMELY STRONG WITH BOTH CREW MEMBERS DEVELOPING A HACKING COUGH AND SINUS ISSUES DURING THE FLIGBT AND ONE CREW MEMBER DEVELOPING A HEADACHE. CORRECTIVE ACTION: ARRIVSDR DXTA2025051903504Engine · fodMOLD ODER IN COCKPIT, BOTH CREW MEMBERS EXPERIENCING SORE THROAT. FOUND UNKNOWN DEBRIS IN LH ENGINE DURING BOROSCOPE. ACCOMPLISHED COMPRESSOR WASH ·PERFORMANCE RECOVERY IAW PHENOM 300 AMM 71-00-00-160·806, NO ODOR PRESENT AT THIS TIME. (ORIGINAL SUBMISSION SDR DXTA2023112710144Battery · defectiveCABIN EMERG LIGHT: AFTER 1 HOUR IN CRUISE, CABIN EMERGENCY LIGHTS BEGAN TO FLASH AND EVENTUALLY REMAINED ON WITH SWITCH IN ARM POSITION///REMOVED AND REPLACED #1 & #2 EMERGENCY BATTERIES. IAW PHENOM 300 AMM 33-52-01. OPS CHECK GOOD.SDR DXTA2023102598720Control Unit · faultedANTI SKID: AFTER LANDING WHEN BRAKE PRESSURE APPLIED THE RH BRAKES WOULD GRAB HARD THEN QUICKLY RELEASE WHENEVER BRAKES APPLIED.THIS CONTINUED ALL THE WAY ON TAXI IN //SIGNOFF//SDR DXTA2023091194870Unknown · unknownRIGHT MLG BRAKE: UPON LANDING, EXCESSIVE GRABBING AND GRINDING FELT ON BOTH BRAKES. SAME PROBLEM WAS PRESENT DURING TAXI. NOT SURE IF IT WAS LEFT OR RIGHT BRAKE BECAUSE PROBLEM WAS FELT WHEN APPLYING EITHER SIDE. SUSPECT RIGHT BRAKE BECAUSE TIRE WAS CHANGEDSDR DXTA2021110851470None · noneBRK FAIL YELLOW CAS: PARKING BRAKE RELEASED ......NO PEDAL PRESSURE OR BRAKES LEFT SIDE, RIGHT SIDE HAD PEDAL PRESSURE BUT NO BRAKES. EMERGENCY BRAKING EMPLOYED TO A SUCCESSFUL STOP. BRAKE FAIL CAS ILLUMINATED SHORTLY AFTER PARKING BRAKE RELEASED.SDR DXTA2021081847130Drive Assy · leakingLIGHT HAZE AND ELECTRICAL ODOR FILLED CABIN. VCS SYSTEM CUTOFF. VCS SYNOPSIS PAGE DISPLAYS YELLOW X ON VCS. RECOVERED REFRIGERANT FLUID OF VCS. REMOVED OLD COMPRESSOR DRLVE MODULE P/N 11336-10-8 S/N 700 AND OLD RECEIVER DRYER ASSY P/N 1134175-12. INSTALLED OVSDR JGVR20201116001Balance Weight · damagedDURING APPLICATION OF EMBRAER SB 505-55-0004 FOUND THE FOLLOWING FLIGHT CONTROL BALANCE WEIGHTS NOT ACCEPTABLE AND REQUIRING REPLACEMENT. INSTALLED 3 LT ELEVATOR ADJUSTABLE BALANCE WEIGHTS P/N: PE915109-L33, IAW SB505-55-0004 R1 PART 1: ELEVATOR MASS BALANCE
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