- Registered owner
- Sale Reported
- Location
- Cleveland, OH
- Owner type
- Individual, fractional ownership
- Serial number
- 55010011
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 23, 2016
- Mode S code
- A4C37E
- Registry status
- Sale reported
Embraer S A EMB-545TCDS TC00062IBAirframe · Embraer S A EMB-545TCDS E00010LAEngine · Honeywell AS907-3-1E
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.
| 2017 | 1 |
|---|---|
| 2018 | 1 |
| 2021 | 1 |
| 2022 | 1 |
| 2023 | 2 |
| 2024 | 4 |
| 2025 | 1 |
| 2026 | 2 |
Airframe · Embraer S A EMB-545
AD 2026-13-02NavigationAD 2026-08-52Flight controlsEmergency ADAD 2025-13-02DoorsAD 2024-23-07Landing gearAD 2024-16-16WindowsAD 2024-15-13WindowsAD 2024-05-13Auto FlightAD 2023-10-02Indicating/Recording System, NavigationAD 2022-19-14Equipment/furnishingsAD 2022-21-08Flight ControlsAD 2020-25-07WindowsAD 2017-22-14NavigationEngine · Honeywell AS907-3-1E
AD 2018-04-13Engine Controls SectionInformation bulletins that may apply
Advisory, not mandatory.
No bulletins matched this aircraft’s models
NTSB investigations
No NTSB investigations matched to N406FXMatched 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-545 aircraft
FAA incident reports
No FAA accident or incident reports matched to N406FXMatched 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-545 aircraft
Service difficulty reports · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR J7SA2022091200331Generator · faultedDIVERTED DUE TO AMBER BATT 1 DISCHARGING CAS FOLLOWED BY A GEN 1 OFF BUS. ELECTRICAL SYNOPTIC PAGE SHOWED GEN 1 OFF AND BOTH SHED BUSSES OFF, WITH GEN 2 POWERING THE SYSTEM. AIRCRAFT LANDED WITHOUT INCIDENT AT KCHS. WHILE TAXIING IN, ENG 1 OIL CHIP DETECT CAS SDR J7SA2020102700232Power Supply · malfunctionedDISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REMOVED AND REPLACED AFT NR 2 EMERGENCY LIGHT POWER SUPPLY. OPERATIONS CHECK GOOD, IAW AMM 33-51-00. P/N 6450LS-00 S/N 001360.SDR J7SA2020093000223Power Supply · failedDISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REPLACED NR 2 EMERGENCY LIGHT POWER SUPPLY WITH TESTED UNIT. OPS CHECK GOOD, IAW LEGACY 450 AMM 33-51-01. P/N 6450LS-00; S/N 001734.SDR J7SA2020052715001Power Supply · inoperativeDURING ROUTINE MAINTENANCE, DISCOVERED EMERGENCY LIGHT NOT ARMED AMBER CAS DISPLAYS WHEN EMERGENCY LIGHT SWITCH IS IN THE ARMED POSITION. REPLACED BOTH EMERGENCY LIGHT POWER SUPPLIES WITH INSPECTED UNITS. OPS CHECK GOOD. NR 1 PN ON: 6450LS-00; SN ON: 001040. NSDR J7SA20181114001Fairing · erodedV-STAB TOP FAIRING PAINT AND HONEYCOMB STRUCTURE IS PEELING AND ERODING, THIS SDR TO BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION. REMOVED AND REPLACED VERT STAB AFT UPPER FAIRING REF AMM 55-32-31. DUE TO WATER INTRUSION. AFT RED BEACON WAS ALSO REPLACESDR J7SA2018112014001Fairing · damagedV-STAB TOP FAIRING PAINT AND HONEYCOMB STRUCTURE IS PEELING AND ERODING, THIS SDR TO BE UPDATED UPON COMPLETION OF THE CORRECTIVE ACTION.
Reports on N406FX not matched to an aircraft · 3
They name N406FX, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 4508909252005Relay · failedRED CAS STAB OVERHEAT, BURNING SMELL IN CABIN. CREW ADVISED THE RED (STAB OVHT) CAS MESSAGE ILLUMINATED WITH CWP AND TRIPLE CHIME DURING CLIMB THROUGH FL 30.0. THE THRUST LEVERS WERE JUST BELOW MCR, 82% N1 AND -29 TEMP. CREW SELECTED ANTIICE *OFF* AND PULLESDR 4508912172004Valve · faultyNOSE GEAR REMAINED UP ON FIRST 4 CYCLES OF THE GEAR HANDLE THEN LOWERED NORMALLY ON 5TH ATTEMPT. MAINTENANCE REPLACED THE LANDING GEAR CONTROL VALVE. OPS CHECK NORMAL. NO DEFECTS NOTED AND NO RE-OCCURRENCESDR WVE2002F00002Squat Switch · missingDURING OUT GOING INSPECTION FOUND ONE SET SCREW MISSING AND ONE SET SCREW LOOSE ON RIGHT MAIN LANDING GER OUT BOARD SQUAT SWITCH SWING ARM. PROBABLE CAUSE: THE SCREWS VIBRATED LOOSE. RECOMMEND THAT AN INSPECTION FOR LANDING GEAR SQUAT SWITCH BE ADDED TO THE
STCs that may be installed · 15
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
Airframe · Embraer S A EMB-545
STC ST04764NYTrue Blue Power TS56 Emergency Battery Power Supply ReplacementSTC ST03885ATInstallation of an Avionica, Inc. avCM Cellular ModuleSTC ST11982CHInstallation of SpaceX Starlink Aviation System iSTC ST04560ATReplacement of the existing Honeywell HTF7000 engine upper and lower thrust reverser door assemblies with Quiet Technology Aerospace modified upper and lower thrust reverser door assembliesSTC ST02534SEInstallation and maintenance of a Crane Aerospace & Electronics Tire Pressure Sensor AssemblySTC ST02472ATInstallation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIIISTC ST11934IBInstallation of Gogo AVANCE L5/LX5 SystemSTC ST11863CHInstallation of Gogo Dual Directional AntennasSTC ST00079IBIntegration of Halon-free Portable Fire Extinguisher HAFEXSTC ST04665CHInstallation of a Galley 115VAC/60Hz inverter and USB Charging Ports in accordance with Premier Air
Center Master Data List Document No. A23377L-755, Revision C, dated June 7, 2024, or later FAA
approved revision.STC ST04650CHInstallation of a Gogo Avance L5 Broadband SystemSTC ST04575ATInstallation of the Rockwell Collins ALT-1000+/ -4000+ with 5G FilteringSTC ST00098IBIntroduction of ADS-B OutSTC ST04464ATReplacement of the inner aluminum barrel of the engine inlet cowlSTC ST03776NYModification to upgrade existing Rockwell Collins TCAS (Model: TTR-920, TTR-921, and TTR-4000) at VERSION 7.0 to Rockwell Collins TCAS (Model: TTR-921, TTR-4000, and TTR-4100) at VERSION 7.1 (ACAS II)