- Registered owner
- Flexjet LLC
- Location
- Cleveland, OH
- Owner type
- LLC
- Serial number
- 50500115
- Year built
- 2012
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- November 6, 2012
- Certificate issued
- March 14, 2023
- Expires
- March 31, 2030
- Mode S code
- A3F085
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 N353FXMatched 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 N353FXMatched 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 · 12
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR J7SA2024100300418Fce · unserviceableCREW RECEIVED GND SPOILER FAIL CAS MESSAGE IN FLIGHT. REPLACED FAULTY FCE #2 IAW EMB 505 AMM 27-03-01. OPS CHECK GOOD, NO FURTHER FAULTS NOTED.SDR J7SA2024051300398Generator · failedON DESCENT INTO KPHX AT AROUND 10,000FT, CREW NOTICED A LIGHT WHINING NOISE & FELT VIBRATION IN FLOOR & RUDDER PEDALS. RECEIVED E2 FIRE DET FAIL CAS, BEGAN RUNNING QRH, & 10-15 SECONDS LATER E2 FAIL ILLUMINATED & RT ENGINE FAILED. AN EMERGENCY WAS DECLARED, SDR J7SA2023122700379Electronic Unit · unserviceableWHILE IN CRUISE FLIGHT PTRIM NML FAIL CAS. MESSAGE STAYED ON UNTIL POWER DOWN. REPLACED #2 FCE. COMPLIED W/ RIGGING AND OPS CHECKS, NO DEFECTS NOTED. WORK COMPLETED IAW EMB 505 AMM 27-03-01.SDR J7SA2022080400327Elevator · fault messageREPLACED #2 FCE DUE TO REPEAT PITCH TRIM AND SPOILER FAULT CAS MESSAGES IAW PHENOM 300 27-03-01.SDR J7SA2022060200321Spoiler · fault messageREPLACED FCE #2 DUE TO GND SPLR FAIL AND SPOILER FAULT ON LANDING. OPS CHECK GOOD. WORK COMPLETED IAW EMB 505 AMM 27-03-01.SDR J7SA2022050200316Fcu · fault messageREPLACED #2 FCE DUE TO SWPS FAULT, GND SPL FAIL, PTRIM NML FAIL, SPOILER FAULT AND RED X'S ON SPOILER INDICATOR AND PITCH INDICATOR WHILE TAXING INTO POSITION FOR TAKEOFF AT KMDW. WORK COMPLETED IAW PHENOM 300 AMM 27-30-01.SDR J7SA2020110200233Power Supply · malfunctionedDISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REMOVED AND INSTALLED FWD AND AFT EMERGENCY LIGHT POWER SUPPLIES WITH SERVICEABLE, IAW AMM 33-52-01. FUNCTIONAL CHECK GOOD.SDR J7SA202002064001Warning Message · false activationNOSE LANDING GEAR DISAGREE ON GEAR EXTENTION. RECEIVED THREE GREEN INDICATIONS AFTER RECYCLING THE GEAR AS PER EMERGENCY PROCEDURE. VISUALLY INSPECTED THE NOSE GEAR FOR CONDITION AND SECURITY, NO DEFECTS OR LEAKS NOTED. PERFORMED LUBRICATION OF THE NOSE LANDINSDR J7SA201912195001Autopilot Sys · failedPTRIM NML FAIL CAS MESSAGE ILLUMINATED AT CRUISE. AUTOPILOT THEN FAILED - NO CAS SWAPPED FCE 1 AND FCE 2 FOR TROUBLESHOOTING PURPOSES. REPLACED FCE 1 WITH REPAIRED UNIT. ALL WORK PERFORMED IAW EMB 505 AMM 27-03-01 PN 462900-1017 S/N 1038 PN 462900-1017 S/NSDR J7SA20191016001Electronic Unit · failed#1 FCE FAILED PTRIM BACK UP OPS TEST. REMOVED AND REPLACED #1 FCE, OPERATIONAL CHECK SATISFACTORY.SDR DJFA20180709001Modulating Valve · defectiveON DESCENT PASSING 1200 (H STAB AND ENGINE HEATS ON) IMC, "DUCT 2 OVERTEMP" CAS MESSAGE ILLUMINATED. AIR CONDITION TO MANUAL - NO EFFECT, ECS KNOB - 1 NO EFFECT, ECS KNOB OFF - VENT CAS MESSAGE WENT OUT. LANDING UNEVENTFUL AFTER SHUT DOWN STRONG BURNING SMELSDR DJFA20171113001Warning Message · false activationDUCT NR 2 OVERTEMP CAS MESSAGE DURING CLIMB OUT. DECLARED EMERGENCY AND DIVERTED. LANDED WITHOUT INCIDENT. RESET THE CIRCUIT BREAKER AND COMPLIED WITH AN ELECTRICAL CHECK. NO FAULTS FOUND..
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