- Registered owner
- Flexjet LLC
- Location
- Cleveland, OH
- Owner type
- LLC
- Serial number
- 50500208
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- April 15, 2014
- Certificate issued
- March 24, 2022
- Expires
- March 31, 2029
- Mode S code
- A406CF
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 N359FXMatched 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 N359FXMatched 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 · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR J7SA2026072200487Flt Controls · multiple failDIVERTED DUE TO SWPS FAULT, FLAP FAIL, PTRIM BKP FAIL, AND SPOILER FAULT MESSAGES AT FL410. THE CREW RAN THE QRH AND DIVERTED TO KSFB. AIRCRAFT LANDED WITHOUT INCIDENT AT KSFB. REPLACED FCE #1 IAW AMM 27-03-01.SDR J7SA201911220001Warning Message · false activationON TAXI OUT, BRK FAIL CAS MESSAGE APPEARED. NO BRAKE ACTION AVAILABLE FROM MAIN BRAKES. USED EMERGENCY/PARKING BRAKE TO SAFELY POSITION AND STOP THE AIRPLANE.PERFORMED MAIN BRAKE SYSTEM FUNCTIONAL TEST I.A.W PHENOM 300 A.M.M 32-41-00-720-801-A. NO DEFECTS NOTSDR DJFA201811128001Controller · malfunctionedDIVERTED DUE TO SWPS FAULT, PITRIM BKP FAIL, FLAP FAIL, SPOILER FAULT, RED XS IN FLAP INDICATOR BOX AND RED XS IN PITCH INDICATOR BOX AT ALTITUDE. R & R #1 FCE. PERFORMED RIGGING AND OPS CHECKS WITH NO DEFECTS NOTED AT THIS TIME.SDR DJFA20170312001Starter Gen · failedDIVERTED DUE TO A BANG AND VIBRATION IN FLIGHT, FOLLOWED BY LT GENERATOR GOING OFFLINE. LANDED WITHOUT INCIDENT. REMOVED AND REPLACED THE LT ENGINE STARTER/GENERATOR WITH NEW. OPS CHECKS NORMAL PER AMM 24-31-01. PERFORMED FIM 24-31-00-810-829-A NO DEFECTS NOTESDR DJFA2018062606001Actuator · failedDURING CLIMB OUT, CAS MESSAGE NML PITCH TRIM FAIL CAME ON. NORMAL PITCH TRIM HAD FAILED CONTINUED TO 450FL USED BACKUP TRIM. REMOVED THE PITCH TRIM ACTUATOR AND REPLACED WITH A REPAIRED ACTUATOR IAW P-300 AMM 27-41-01. PERFORMED HORIZONTAL STABILIZER ELECTRIC
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