- Location
- Cleveland, OH
- Owner type
- Co-owned, fractional ownership
- Serial number
- 50500233
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, commuter
- Airworthiness date
- November 3, 2014
- Certificate issued
- March 31, 2025
- Expires
- March 31, 2032
- Mode S code
- A40CDF
Embraer Executive EMB-505TCDS A60CEAirframe · Embraer Executive 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 Executive 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 Executive 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 N360FXMatched 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 Executive EMB-505 aircraft
FAA incident reports · 1
FAA accident and incident reports matched to this aircraft by N-number and event date, checked against the reported make and model.
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR J7SA2025111000461Fce · faultedPTRIM BKP FAIL CAUTION CAS ILLUMINATED ON ROTATION; REMAINED ON AFTER POWER CYCLE AT DESTINATION. REPLACED FCE IAW AMM 27-03-01. PERFORMED FLAP SYSTEM ELECTRONIC RIGGING. OPERATIONAL TESTS SATISFACTORY.SDR J7SA2025070300450Fce · faultedFCE 1 REPLACED DUE TO MULTIPLE INCIDENTS OF SPURIOUS FLIGHT CONTROL CAS MESSAGES. WORK COMPLETED IAW EMB-505 AMM 27-03-01. COMPLETED RIGGING PROCEDURE OF THE FLAP SYSTEM. ALL OPS CHECKS GOOD.SDR J7SA2025040200443Fce · faultedPITCH TRIM BACKUP FAIL CAS MESSAGE DURING SYSTEM TEST. REPLACED FCE1 IAW AMM 27-03-01. RIGGING AND OPS CHECK GOOD.SDR J7SA2021062400286Electronic Unit · faultedFLAP FAIL CAS MESSAGE AFTER INITIAL POWER UP. TWO RESETS WERE PERFORMED, BOTH UNSUCCESSFUL. REMOVED AND INSTALLED SERVICEABLE FCE UNIT IAW EMBRAER P300 AMM 27-03-01. OPS CHECK GOOD. P/N 462900-1017; S/N 0057.SDR DJFA20190417001Sensor · faultyTROUBLESHOOT SPOILER FAULT & GRND SPOILER FAIL CAS MESSAGE. ACCOMPLISHED CMC DOWNLOAD AND DONWLOADED CMC INTERFACE FILES TO ACCESS TO MED OEM PAGE AND SENT SCREENSHOTS OF SPOILER SYSTEM SENSORS TO CONTACT CENTER FOR ANALYSIS. DURING TROUBLESHOOTING PER SL505-2SDR DJFA20170422001Windshield · crackedAIR TURNBACK DUE TO WINDSHIELD SHATTERING ON CAPTAINS SIDE DURING CLIMB. CREW DECLARE AN EMERGENCY AND LANDED WITHOUT INCIDENT. REPLACED CAPT SIDE NR 1 WINDSCREEN. LEAK AND OPS CHECK GOOD.
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