- Registered owner
- Flexjet LLC
- Location
- Cleveland, OH
- Owner type
- LLC
- Serial number
- 50500094
- Year built
- 2012
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- October 31, 2012
- Certificate issued
- January 7, 2022
- Expires
- January 31, 2029
- Mode S code
- A3D7E2
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 N347FXMatched 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 N347FXMatched 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 J7SA2026050400480Fce · faultedDURING CRUISE, CREW RECEIVED GND SPLR FAIL CAS. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED AND RIGGED FCE2. OPS CHECK GOOD. WORK PERFORMED IAW AMM 27-03-01.SDR J7SA2025040200441Fce · faultedCREW RECEIVED GND SPOILER FAIL CAS MESSAGE DURING DESCENT. ATC INSTRUCTED THE CREW TO REDUCE SPEED TO 190 KNOTS; THE CREW ATTEMPTED TO DEPLOY SPEED BRAKES AT APPROXIMATELY 225 KNOTS. A GND SPOILER FAIL CAS MESSAGE APPEARED, AND THE SPOILER BOX INDICATED A FAILSDR J7SA2024121200422Fce · faultedAIR TURN BACK DUE TO PTRIM NML FAIL CAS MESSAGE AFTER MANUAL PITCH TRIM ACTIVATION RESULTED IN NO TRIM INPUT NEAR THE INITIAL LEVEL-OFF ALTITUDE. BACKUP MODE PITCH TRIM WAS USED FOR THE REMAINDER OF THE FLIGHT. AIRCRAFT LANDED WITHOUT INCIDENT AT KMDW. REPLACESDR J7SA2024120300421Controller · failedTHE #2 FCE FAILED DURING ENGINE RUNS. UNIT WAS SWAPPED AND FAULT FOLLOWED UNIT. REPLACED #2 FCE IAW PHENOM 300 AMM 27-03-01.SDR J7SA2024090300415Controller · unserviceableCREW RECEIVED SWPS FAULT, FLAP FAIL AND PTRIM BKP FAIL CAS IN FLIGHT. EXECUTED NO FLAP LANDING. REPLACED FCE #1 IAW PHENOM AMM 27-03-01. ALL FOLLOW-ON CHECK PASSED AND NO FURTHER CAS MESSAGES PRESENT.SDR J7SA2021083100294Mount · faultedABNORMAL SOUND COMING FROM UNDER RH COCKPIT SEAT. ELEVATOR CONTROL FEELS LIKE SOMETHING IS DRAGGING WHEN ACTUATED BY THE CONTROL YOKE. REPLACED ELEVATOR SERVO ACTUATOR. REPLACED ELEVATOR SERVO MOUNT. ACCOMPLISHED ELEVATOR MOVEMENT. ACCOMPLISHED ELEVATOR SERVO SDR J7SA2021010400260Flt Controls · malfunctionedDURING DESCENT, SPOILER FAIL CAS MESSAGE. AIRCRAFT LANDED WITHOUT INCIDENT. REMOVED AND REPLACED NR 2 FCE, IAW PHENOM 300 AMM 27-03-01-400-801. PERFORMED ALL ASSOCIATED RIGGING AND OPERATIONS CHECKS, PER TASK 37-03-01-400-801. ALL OPERATIONS CHECKS GOOD. SDR DJFA2018042612001Actuator · failedNORMAL PITCH TRIM FAIL CAS MESSAGE, FAILED HALF HOUR INTO FLIGHT. REMOVED AND REPLACED REPAIRED PITCH TRIM ACTUATOR. OPS CHECKED GOOD.SDR DJFA20160813001Thermal Switch · defectiveDIVERTED DUE TO "BLEED 2 LEAK" CAS MESSAGE. COMPLETED QRH PROCEDURE AND CAS MESSAGE CLEAR. DURING DECENT CAS MESSAGE CAME BACK. COMPLETED QRH PROCEDURES TO SECOND END POINT AND CAS MESSAGE CLEARED AND REMAINED OFF FOR REMAINDER OF FLIGHT. CREW DECLARED AN EMSDR DJFA20160124001Connector · looseON DESCENT CREW RECEIVED HYD HIGH TEMP CASS MSG. EXECUTED CHECKLIST & RESULTED IN LOSS OF HYD SYS. DECLARED EMER. UPON LANDING, UTILIZED EMER BRAKES & BLEW BOTH MAIN TIRES ON RUNWAY. FOUND LOOSE CONNECTOR P0589 AT HYD TEMP SWITCH. THE CONNECTOR WAS ADJUST
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