- Registered owner
- Flexjet LLC
- Location
- Cleveland, OH
- Owner type
- LLC
- Serial number
- 50500032
- Year built
- 2011
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- April 15, 2011
- Certificate issued
- March 22, 2022
- Expires
- March 31, 2029
- Mode S code
- A39A19
Embraer-Empresa Brasileira De EMB-505TCDS A60CEAirframe · Embraer-Empresa Brasileira De EMB-505TCDS E00053ENEngine · Pratt & Whitney Canada PW535E
From the FAA registry file of October 21, 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-Empresa Brasileira De 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-Empresa Brasileira De 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 N331FXMatched by N-number and event date. Investigations from before this aircraft carried the mark are under Earlier aircraft. Investigations on Embraer-Empresa Brasileira De EMB-505 aircraft
FAA incident reports
No FAA accident or incident reports matched to N331FXMatched by N-number and event date. Reports from before this aircraft carried the mark are under Earlier aircraft. Reports on Embraer-Empresa Brasileira De EMB-505 aircraft
Service difficulty reports · 7
SDR J7SA2026090100514Fce · faultedFLAP FAIL CAS ILLUMINATED AFTER MOVING FLAP LEVER TO NR 1 POSITION. REPLACED FCE NR 1 IAW AMM 27-03-01. REPLACED FLAP SELECTED LEVER AND FLAP POWER DRIVE UNIT IAW AMM 27-53-01 AND 27-51-07. COMPLIED WITH FLAP RIGGING IAW 27-50-00. OPS CHECKS GOOD.SDR J7SA2026010600468Fce · faultedON START UP, FLAP FAIL CAS ILLUMINATED AND FLAP INDICATOR ON MFD SHOWED YELLOW. CYCLED FLAPS AND MESSAGE REMAINED. REPLACED FCE 1 IAW EMB 505 AMM 27-03-01. RIGGING/OPS CHECK GOOD.SDR J7SA2026010600466Fce · faultedDURING CRUISE, CREW RECEIVED SWPS FAULT, FLAPS FAIL, PTRIM BKP FAIL AND SPOILER FAULT. AIRCRAFT LANDED WITHOUT INCIDENT. REPLACED FCE 1 IAW EMB 505 AMM 27-03-01. FCE 1 RIGGING / OPS CHECK GOOD AND NO CAS MESSAGE ILLUMINATED.SDR J7SA2024070100405Control Unit · failedCREW RECEIVED GROUND SPOILER FAIL ON LANDING. REPLACED # 2 FCE IAW PH300 AMM 27-03-01.SDR J7SA2024060300402Controller · unserviceableCREW RECEIVED GROUND SPOILER FAULT, SPOILER FAIL, AND PRIMARY TRIM FAIL (PTRIM NML FAIL). REPLACED FAILED # 2 FCE. PERFORMED SPOILER ELECTRONIC RIGGING. OPS CHECK GOOD. ALL WORK COMPLETED IAW PHENOM 300 AMM 27-03-01.SDR DJFA201908238001Wire · burnedELECTRICAL BURN SMELL. FOUND BURNT WIRE HARNESS (W311) AT LH PDU CONNECTING TO THE GPU POWER RECEPTACLE. REMOVED AND REPLACED THE LPDU EXTERNAL POWER RECEPTACLE, AND HARNESS W311 REF PHENOM 300 AMM 24-65-01 AND 24-41-00 PERFORMED OPS CHECKS OPS CHECKED GOODSDR 6045491052106Engine · overtempLEFT ENGINE ITT WENT INTO THE RED. ENGINE ICON POSTED ABOVE THE ITT GAUGE. THE PILOT OBSERVED THE LEFT ITT WAS ABOVE 900. DURING TAKEOFF ROLL THE LEFT ENGINE ITT WENT INTO THE RED. THE ENGINE ICON POSTED ABOVE THE ITT GAUGE. THE PILOT OBSERVED THE LEFT IT