- Registered owner
- Flexjet LLC
- Location
- Cleveland, OH
- Owner type
- LLC
- Serial number
- 50500090
- Year built
- 2012
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- July 2, 2012
- Certificate issued
- March 21, 2022
- Expires
- March 31, 2029
- Mode S code
- A3D42B
Embraer S A EMB-505TCDS A60CEAirframe · Embraer S A 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 S A 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 S A 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 N346FXMatched 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 S A EMB-505 aircraft
FAA incident reports
No FAA accident or incident reports matched to N346FXMatched 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 S A 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 J7SA2026041300478Glare Shield · smokeDIVERTED TO KMRY DUE TO AN ELECTRICAL BURNING SMELL IN THE CABIN. DURING CRUISE, THE PIC NOTED A RED X APPEAR OVER COM2 WHICH THEN EXTINGUISHED AND REAPPEARED MULTIPLE TIMES SHORTLY THEREAFTER. THE CREW OBSERVED SMOKE EMANATING FROM THE GLARESHIELD PROMPTING TSDR J7SA2024070300408Electronic Unit · abnormalDIVERTED DUE TO FLAP FAIL CAS DURING APPROACH WITH GEAR DOWN AT 1500FT AGL. CREW PERFORMED GO AROUND, RAN QRH, AND LANDED WITHOUT INCIDENT AT KAUS. REPLACED THE FCE 1 IAW EMB 505 AMM 27-03-01. RIG AND OPS CHECKS GOOD.SDR J7SA2024070100406Control Unit · failedCREW RECEIVED FLAP FAIL, SWPS FAULT, PTRIM BKP FAIL, AND SPOILER FAULT ON POWER UP AND PERFORMED TWO UNSUCCESSFUL RESETS. REPLACED # 1 FCE IAW PH300 AMM 27-03-01. RIGGED AND OPS TESTED WITH NO DEFECTS FOUND.SDR J7SA2023081000369Electronic Unit · unserviceableON DESCENT, SWPS FAIL AND PTRIM BKP FAIL CAS ILLUMINATED. CREW RAN QRH, DETERMINED THIS WAS A TRUE FLAP FAILURE, DECLARED EMERGENCY WITH ATC, NOTIFIED PAX, AND LANDED WITHOUT INCIDENT AT KRAP. TROUBLESHOT ISSUE TO FCE # 1. REPLACED FCE #1 IAW EMB P300 AMM 27-5SDR J7SA2022012600308None · noneAIR TURN BACK DUE TO BLEED 1 OFF AND BLEED 1 FAIL CAS. RAN QRH, TURNED BLEED 1 SWITCH OFF FOR 60 SECONDS. DURING 60 SECOND PERIOD, BLEED 2 OFF AND BLEED 2 FAIL CAS ILLUMINATED. PERFORMED EMERGENCY DESCENT; DECLARED EMERGENCY; MANUAL PAX MASK DEPLOYMENT. CABIN SDR 2021FA0000327None · noneDIVERTED DUE TO CABIN ALTITUDE PRESSURIZATION INCREASING AT A RATE OF 800FT PER MINUTE. THE CREW IMMEDIATELY INSTRUCTED ATC THEY NEEDED TO DESCEND. THE PRESSURIZATION RATE WAS NOT DECREASING DURING DESCENT, CAUSING THE CREW TO DECLARE AN EMERGENCY. THE CABIN ASDR J7SA2021102600299Rudder Control · malfunctionedVENTRAL RUDDER FAIL CAS ON SHORT FINAL IN HEAVY CROSS WIND CONDITIONS. DURING POST FLIGHT, FOUND VENTRAL RUDDER FULLY DEFLECTED AND FROZE TO THE LEFT. PERFORMED VISUAL INSPECTION OF AIRCRAFT, NO DAMAGE NOTED. TROUBLESHOT IAW FIM 22-11-00. PERFORMED VENTRAL RUSDR DJFA20171226001Control Unit · failedBRAKES FAILED CAS MESSAGE ON LANDING. MAIN BRAKES DID NOT WORK. BOTH MAIN TIRES HAD FLAT SPOTTED. R & R THE BRAKE CONTROL UNIT AND BOTH MAIN WHEEL AND TIRE ASSYS. OPS CHECKED GOOD.SDR DJFA20140928001Actuator · failedPITCH TRIM NORMAL FAIL CAS (MSG) COMES ON IN FLIGHT. REMOVED PITCH TRIM ACTUATOR P/N 467500-1003 S/N 0038 AND INSTALLED REPAIRED ACTUATOR P/N 467500-1003 S/N 0047. OPS CHECKED GOOD.SDR DJFA201042600001Actuator · failedPTRIM BKP FAIL CAS MESSAGE. REMOVED AND REPLACED THE PITCH TRIM ACTUATOR WITH REPAIRED UNIT. REMOVED SN 0047 AND INSTALLED SN 0038.
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