- Registered owner
- Flexjet LLC
- Location
- Cleveland, OH
- Owner type
- LLC
- Serial number
- 50500105
- Year built
- 2012
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- February 22, 2013
- Certificate issued
- March 21, 2022
- Expires
- March 31, 2029
- Mode S code
- A3E917
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 N351FXMatched 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 N351FXMatched 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 · 11
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR J7SA2020120800253Battery Pack · inoperativeDISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REMOVED THE NR 1 AND NR 2 EMERGENCY BATTERIES AND INSTALLED INSPECTED UNITS. OPERATIONS TEST GOOD. WORK PERFORMED IAW EMB-505 AMM 33-52-01.SDR J7SA2020062600200Starter Gen · failedDIVERTED DUE TO ELECTRICAL EMERGENCY CAS WHILE FLYING AT FL430 IN CRUISE. CREW LOST POWER, UNDERTOOK AN EMERGENCY DESCENT, AND OXYGEN MASKS DEPLOYED. GENERATORS WERE RESET UPON REACHING 10,000 FEET; #2 GEN AND AHARS DID NOT RESET (ALL OTHER SYSTEMS OPERATIONALSDR DJFA201908094001Tube · brokenAIR TURN BACK DUE TO FUEL 1 FEED FAULT. MOTIVE FLOW PUMP 1 RED X DISPLAY. AIRCRAFT LANDED WITHOUT INCIDENT.REPLACED LH WING ENGINE FEED CHECK VALVE. REPLACED LH FUEL TANK VENT TUBE DRAIN VALVE FOUND BROKEN OFF IN FUEL TANK. PERFORMED HIGH POWER ENGINE RUN AND SDR DJFA20190403001Unknown · malfunctionedFLAP FAIL, SPWS FAULT, SPOILER FAULT. PERFORMED CMC DOWNLOAD FINDING FAULT CODE27522041 AND 27020141. COMPLIED WITH FIM TASK 27-53-00-810-808 FINDING CONDITION TO BE TRANSITORY. PER CUSTOMER REQUEST SWAPPED FCE 1 AND FCE 2 IAW AMM 27-03-01. PERFORMED FLAP SYSSDR DJFA2019041722001Control Unit · failedBACKUP PITCH TRIM FAIL CAS MESSAGE ON PDFS. POWERED AIRCRAFT DOWN AND BACKUP, MESSAGE STILL THERE ON PDFS. REMOVED AND REPLACED #1 FCE AND ACCOMPLISHED ELECTRONIC RIGGING PROCEDURE. ACCOMPLISHED IAW PHENOM 300 AMM 27-03-00. OPS CHECKS GOOD IAW PHENOM 300 AMM 2SDR DJFA2019041705001Control Unit · failedGND SPLR FAIL CAS MESSAGE IN FLIGHT. REMOVED AND REPLACED FCE 2 UNIT AND PERFORMED SATISFACTORY RIGGING/OPERATIONAL TEST OF THE SPOILER SYSTEM PER EMB 505 AMM 27-03-01 P/N 462900-1017 S/N 0938SDR DJFA20181119001Starter Gen · failedDIVERTED DUE TO VIBRATION GEN NR 1 FAIL CAS MSG APPEARED SHORTLY AFTER. CREW RAN CHECKLIST. VIBRATION WENT AWAY WITH REDUCED POWER BUT GEN WOULD NOT RESET. AIRCRAFT LANDED WITHOUT INCIDENT. R&R NR 1 GEN, STARTER PAD SEAL MAGNETIC SEAL, ACCESSORY DRIVE GEARSHIFSDR DJFA20180216001Actuator · failedPITCH TRIM NORMAL FAIL CAS MESSAGE AT HIGH ALTITUDE. WHEN BACKUP TRIM ENGAGED PTRM BKP FAIL CAS MESSAGE. TRIM FULL DOWN AT 14.1. REPLACED THE PITCH TRIM ACTUATOR. OPS CHECKED GOOD. R & R TELESCOPING DUCT O-RING SEALS. LEAK CHECKED GOOD.SDR DJFA20180125002Actuator · malfunctionedPITCH TRIM NORMAL FAIL, CAS MESSAGE ILLUMINATED ON CLIMB PASSING 16,000FT. REPLACED THE STAB TRIM ACTUATOR WITH REPAIRED UNIT. REPLACED FCE NR 2 WITH MODIFIED UNIT. OPS CHECKED GOOD AND NO DEFECTS NOTED.SDR DJFA20180125001Warning Message · false activationPASSING FLIGHT LEVEL 390, PTRIM NML FAIL, CAS MESSAGE ILLUMINATED AND REMAINED ON FOR REMAINDER OF FLIGHT. OPS CHECK GOOD AT THIS TIME.SDR DJFA2018104267001Actuator · failedPITCH TRIM NEUTRAL FAIL CASS MESSAGE COMES ON IN DESCENTS (BETWEEN SETTINGS OF 13.5 -13,9 ). REMOVED AND REPLACED PITCH TRIM ACTUATOR ON 467500-1003. REMOVED SN 0141 AND INSTALLED SN 0058. ACCOMPLISHED HORIZONTAL STABILIZER ELECTRICAL STOP-FUNCTIONAL CHECK, CH
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