- Registered owner
- Flexjet LLC
- Location
- Cleveland, OH
- Owner type
- LLC
- Serial number
- 55010055
- Year built
- 2019
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 9, 2019
- Certificate issued
- December 28, 2021
- Expires
- December 31, 2028
- Mode S code
- A50757
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 N423FXMatched 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 N423FXMatched 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 · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR J7SA2023073100366Unknown · unknownDIVERTED DUE TO CREW HEARD A LOUD BANG AT FL450. AFTER FURTHER INSPECTION THEY NOTED THE PILOT SIDE WINDOW HAD CRACKED AND WAS BEGINNING TO DELAMINATE. CREW DID NOT DECLARE EMERGENCY. ATC TREATED IT AS ONE AND FIRE TRUCKS MET THE AIRCRAFT ON LANDING AT KSGF. RSDR J7SA2022061300323Window · crackedRH WINDOW CRACKED DURING FLIGHT AT FL450. NO LOSS OF PRESSURIZATION. AIRCRAFT LANDED WITHOUT INCIDENT AT MMPR. REPLACED RH COCKPIT SIDE WINDOW AND IAW EMBRAER LEGACY 450/500 AMM 56-12-00. LEAK CHECK GOOD. NO DEFECTS NOTED.SDR J7SA2021022500277Power Supply · faultedDISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REMOVED AND REPLACED FWD EMERGENCY LIGHT POWER SUPPLY IAW AMM 33-51-01. OPS CHECK GOOD. PN 6450LS-00; SN 000675.SDR JGVR20200915001Wire · shortedON TAXI IN, CYAN FLT CNTRL FAULT ILLUMINATED ALONG WITH CYAN REMOTE C/B TRIP. WE WERE ABLE TO RESET THE TRIPPED C/B REU5 AND MESSAGES CLEARED. ON TAXI OUT, CYAN FLT CNTRL FAULT AND REMOTE C/B TRIP MESSAGE RETURNED. THE REU5 C/B IS TRIPPED FOR A 2ND TIME. FSDR J7SA2020072300210Battery Pack · failedDISCOVERED EMERGENCY LIGHTS NOT ARMED CAS MESSAGE WILL NOT GO OFF. REMOVED AND REPLACED THE NR 1 EMERGENCY BATTERY PACK WITH AN INSPECTED UNIT AND THE NR 2 EMERGENCY BATTERY PACK WITH A TESTED UNIT IAW AMM 33-51-00. ACCOMPLISHED THE OPERATIONAL TEST OF THE E
Reports on N423FX not matched to an aircraft · 4
They name N423FX, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 4513412032005Actuator · malfunctionedRIGHT MAIN LANDING GEAR DOOR WILL NOT RETRACT. MX ADVISED THAT THE RT DOOR SWITCH ON THE RT INBOARD GEAR DOOR ACTUATOR IS NOT OPENING WITH POWER ON. THE SWITCH COMES AS PART OF THE ACTUATOR ASSEMBLY. THE ACTUATOR HAS BEEN PLACED ON ORDER AT THIS TIME.SDR 2006FA0000024Cable · damagedDURING THE INITIAL 5,000 HOUR CABLE INSPECTIONON THIS AIRCRAFT NOTED EXTENSIVE DAMAGE TO THE LOWER LEFT AFT ELEVATOR CONTROL CABLE AND PRESSURIZATION SYSTEM VACUUM LINE WAS FOUND MISROUTED CAUSING DAMAGE TO THE ELEVATOR CONTROL CABLE AND VACCUM LINE. ENGINEERSDR 2006FA0000027Torque Tube · corrodedDURING 5,000 HR INSPECTION, THE RUDDER WAS REMOVED FOR SB, REPAIR OF (RUDDER TORQUE TUBE ASSY BONDING JUMPERS) FOUND CORROSION ON TORQUE TUBE INTERNAL AND EXTERNAL. MOISTURE INGRESSION THROUGH WIRE BUNDLE HOLE. ENGINEERING EVALUATE FOR POSSIBLE INTERNAL INSP
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)