- Registered owner
- Flexjet LLC
- Location
- Cleveland, OH
- Owner type
- LLC
- Serial number
- 50500384
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- November 3, 2016
- Certificate issued
- November 30, 2021
- Expires
- November 30, 2028
- Mode S code
- A4345E
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 N370FXMatched 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 N370FXMatched 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 J7SA2025090400455Seat · brokenON TAKEOFF ROLL, THE LEAD PASSENGERS SEAT BROKE CAUSING PASSENGER TO FALL BACKWARD. SHORTLY AFTER THE CREW WAS NOTIFIED THAT THE FORWARD-FACING MIDDLE SEAT WOULD NOT REMAIN UPRIGHT. THE SEAT DID NOT RESTRICT ANY EMERGENCY EXIT, EGRESS ROUTE, OR MAIN AISLE. AIRSDR J7SA2025082600451Fce · faultedGND SPLR FAIL CAS ILLUMINATED ON TOUCHDOWN. REPLACED FCE 2. RIGGING AND OPS CHECK GOOD. ALL WORK COMPLETED IAW EMBRAER PHENOM 300 AMM 27-03-01.SDR J7SA2022012400307None · nonePRIOR TO DEPARTURE, CREW DISCOVERED THAT ELEVATOR FEELS THE ELEVATOR FEELS ABNORMALLY HEAVY WITH INTERFERENCE ON THE PILOT SIDE YOKE. REPLACED BEARING ON PILOT SIDE ELEVATOR TORQUE TUBE IN FORWARD FUSELAGE. PILOT YOKE NOW OPERATES SMOOTHLY. WORK COMPLETED IAW SDR J7SA2020072300209Battery · not reportedDISCOVERED EMERGENCY LIGHTS REMAIN ON WITH SWITCH IN THE ARM POSITION. REMOVED AND REPLACED FORWARD AND AFT EMERGENCY BATTERIES IAW AMM 33-52-01. OPS CHECK GOOD.SDR J7SA202006175001Landing Gear · malfunctionedAFTER TAKEOFF CREW RECEIVED LANDING GEAR DISAGREE CAS MESSAGE. GEAR DID NOT RETRACT INTO THE WELL. CREW DECLARED AN EMERGENCY AND RETURNED SAFELY TO DEPARTURE. THIS IS A REPEAT ISSUE, THE SAME GEAR ISSUE PRESENTED ITSELF ON TAKEOFF ON 13 JUNE 2020. INSPECTED SDR DJFA2019041726001Control Unit · defectiveAT CRUISE ALTITUDE (FL450) HAD YELLOW X FOR BOTH SPOILER AND PITCH TRIM INDICATIONS. ALSO THE PRIMARY PITCH TRIM WAS INOPERATIVE. WE HAD NO CAS MESSAGES UNTIL AFTER LANDING (SPWS FAULT). TROUBLESHOT SYSTEM. FOUND # 2 FCE TO BE DEFECTIVE. REMOVED AND REPLACESDR DJFA201904171001Control Unit · malfunctionedAT CRUISE ALTITUDE (FL430) HAD YELLOW X FOR BOTH SPOILER AND PITCH INDICATIONS. ALSO SPWS FAULT CAS MESSAGE, AND MAIN TRIM WAS NOT WORKING. TROUBLESHOT, COMPLIED WITH CMC DOWNLOAD, IASP AND ADS OPS - CHECK OK REMOVED AND REPLACED FCE 2 PER MCC IAW AMM 27-03-SDR DJFA20181225001Starter Gen · malfunctionedLEFT ENGINE HAS A RUMBLING VIBRATION WHEN RUNNING. STARTER GENERATOR LUGS AND SURGES DURING START CYCLE. REMOVED AND REPLACED STARTER GENERATOR. WORK WAS DONE IRT 24-81-01. OPS AND LEAK CHECK GOOD. COMPLIED WITH CMM TASK 05-50-00 FOR UNSCHEDULED GENERATOR CHA
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