- Registered owner
- Flexjet LLC
- Location
- Cleveland, OH
- Owner type
- LLC
- Serial number
- 50500050
- Year built
- 2011
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- July 3, 2011
- Certificate issued
- March 24, 2022
- Expires
- March 31, 2029
- Mode S code
- A3CCBD
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 N344FXMatched 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 N344FXMatched 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 · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR J7SA2025112400463Torque Tube · damagedBINDING NOTED ON TWO SEPARATE FULL RIGHT RUDDER FULL RIGHT BRAKE APPLICATIONS. ACCOMPLISHED A GIV OF THE CONTROL PEDALS IAW AMM 27-01-02 AND THE RUDDER FORWARD TORQUE TUBE IAW AMM 27-21-06. FOUND THE TOP BRACKET HOLDING THE CENTER RUDDER FORWARD TORQUE TUBE FLSDR J7SA2025010600424Flt Controls · unserviceablePTRM NML FAIL CAS MESSAGE RECEIVED DURING AIRCRAFT SETUP. RESET ATTEMPTED WITH NO SUCCESS. REPLACED #2 FLIGHT CONTROL ELECTRONIC IAW EMBRAER 505 AMM 27-03-01. PERFORMED OPS AND RIGGING CHECKS; ALL CHECKS GOOD WITH NO DEFECTS NOTED.SDR J7SA2024070100407Control Unit · unserviceableCREW RECEIVED PTRIM NML FAIL, GND SPLR FAIL, SWPS FAULT, AND SPOILER FAULT AFTER STARTUP. REPLACED FCE # 1. REPLACED FCE # 2. RIG COMPLETED WITH NO DEFECTS NOTED. OPS CHECK GOOD. WORK COMPLETED IAW EMB 505 AMM 27-03-01/SB505-27-0022.SDR J7SA2024050700397Wire Harness · faultedDURING CLIMB, THE RED LIGHT ON #2 FIRE SHUTOFF BUTTON WAS ILLUMINATED. CREW CONSULTED QRH AND INSPECTED FOR ANY OTHER INDICATIONS BUT FOUND NO EVIDENCE OTHERWISE THAT THERE WAS ANY FIRE. AIRCRAFT LANDED AT KLUK WITHOUT INCIDENT. REPLACED #2 ENGINE HARNESS IAW SDR J7SA2022052400320Landing Gear · false indicationAT CRUISE ALTITUDE, 43,000FT, LG LEVER DISAG, ADS 2 SLIP FAIL AND ADS 1 SLIP FAIL CAS MESSAGES ILLUMINATED. DURING DESCENT, CREW LEVELED AT 16,000FT, ENTERED A HOLD, AND PERFORMED LG LEVER DISAG QRH CHECKLIST. GEAR WAS CYCLED DOWN-UP-DOWN. NO CHANGE IN THE CASSDR DJFA201804265001Actuator · failedBACKUP PITCH TRIM FAIL CAS MESSAGE IN FLIGHT. INSTALLED A REPAIRED PITCH TRIM ACTUATOR.
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