- Registered owner
- Flexjet LLC
- Location
- Cleveland, OH
- Owner type
- LLC
- Serial number
- 55010033
- Year built
- 2017
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 8, 2017
- Certificate issued
- December 17, 2021
- Expires
- December 31, 2028
- Mode S code
- A4EAFD
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 N416FXMatched 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 N416FXMatched 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 J7SA2025022100434Shaft · shearedDIVERTED DUE TO GEN 2 BUS OFF CAS AND RELATED MESSAGES WHILE CLIMBING THROUGH FL430. THE SIC RAN THE CHECKLIST AND ATTEMPTED TO RESET THE GENERATOR, BUT THE ISSUE PERSISTED. THE CREW DESCENDED TO FL310, DECLARED AN EMERGENCY, AND DIVERTED TO KRDU. AIRCRAFT LANSDR J7SA2022082600328None · noneDURING DESCENT, LEFT SIDE COCKPIT WINDOW CRACKED. CREW DECLARED EMERGENCY AND LANDED SAFELY AT KAUS. NO LOSS OF PRESSURIZATION, NO INJURIES, ONE PASSENGER ON BOARD. REPLACED LEFT SIDE COCKPIT WINDOW IAW EMB 550 AMM 56-12-00. LEAK AND OPS CHECK GOOD. THIS IS THSDR J7SA2021022500278Power Supply · inoperativeDISCOVERED EMERGENCY LIGHTS FAILED. REMOVED AND REPLACED BOTH FWD AND AFT EMERGENCY POWER SUPPLIES IAW EMB 550 AMM 33-51-01. OPS CHECK GOOD. PN 6450LS-00; SN FWD 001166; SN AFT 001878.SDR J7SA2021012600267Battery Pack · faultedEMERGENCY LIGHT BATTERY FAULT CAS MESSAGE DISPLAYED. REMOVED AND REPLACED FWD AND AFT EMERGENCY LIGHT BATTERY PACKS, IAW EMB 550 AMM 33-51-01. OPERATIONS CHECK GOOD. LEFT RACK P/N OFF/ON: 6450LS-00; S/N OFF: 000675, S/N ON: 002273. C FLOOR P/N OFF/ON: 6450SDR J7SA2020112400243Battery Pack · inoperativeDISCOVERED EMERGENCY LIGHTS REMAIN ON IN ARMED POSITION. REMOVED AND REPLACED FWD AND AFT EMERGENCY BATTERIES, IAW LEGACY 450/500 AMM 33-51-01. OPERATIONS CHECK GOOD AT THIS TIME. FWD P/N OFF/ON: 6450LS-00, S/N OFF: 000897, S/N ON: 000832. AFT P/N OFF/ON:
Reports on N416FX not matched to an aircraft · 2
They name N416FX, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 4511302132005Clamp · looseCREW ADVISED, THE RIGHT PYLON OVERHEAT ILLUMINATED IN CLIMB AT FL 17.0 WITH NAC AND ANTI-ICE SELECTED TO THE OFF POSITION. CREW REDUCED RIGHT ENGINE N1 TO 75 PERCENT FOR 1 MINUTE THEN TO IDLE FOR 2 MINUTES. CAS MESSAGE WOULD NOT EXTINGUISH. CREW FOLLOWED ACSDR WVE2004F00023Cable · maladjustmentLT AND RT GEAR IN TRANSIT LIGHTS REMAINED ILLUMINATED AFTER GEAR EXTENSION. THE FREEFALL CONTROL LEVER WAS BUMPED OUT OF ITS NORMAL (UP) POSITION AND WHEN THE GEAR WAS SELECTED DOWN AND IT COMPLETED ITS CYCLE THE MAIN LANDING GEAR INBOARD DOOR FREEFALL CABLE
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)