- Registered owners
- Arcflight LLCMatos AaronMatos OliviaAutodesk IncBruno Aviation LLCStimac Gary A Trustee
- Location
- Oklahoma City, OK
- Owner type
- Co-owned, fractional ownership
- Serial number
- 55010199
- Year built
- 2026
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 19, 2026
- Certificate issued
- April 13, 2026
- Expires
- April 30, 2033
- Mode S code
- A2ED22
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 N288QSMatched 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 N288QSMatched 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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026062208490Transducer · shearedDURING INITIAL CLIMB AT APPX. 400 FT. AGL, CREW RECEIVED A BRAKE LT FAULT CYAN CAS ACCOMPIANIED BY AN AMBER FLT CTRL NO DISPATCH CAS. LT INBOARD WHEEL SPEED TRANSDUCER LOST ROTATION. FAULT CODE: 32410. ARRIVED AND ACCESSED THE ACFT. PERFORMED POWER CHECKS ANDSDR DXTA2026041407640Sensor · out of alignmentTHROUGH FL210 DOOR PAX OPEN WARNING MESSAGE. CHECKLIST ACCOMPLISHED. CABIN PRESSURIZATION INDICATIONS NORMAL. C/W MAIN DOOR CLOSED SENSOR ALIGNMENT IAW EMB-545-MOD AMM 52-71-20. OPS CHECK GOOD. NO DEFECTS NOTED. THIS CLEARS MEL 52-71-00 AND RETURNS AIRCRAF
Reports on N288QS not matched to an aircraft · 3
They name N288QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR 99ZZZX3321Oxygen Mask · tornDURING ROUTINE INSPECTION OF THE PASSENGER OXYGEN MASKS, A TEAR WAS FOUND AROUND THE COLLAR OF THE BAG WHERE THE OXYGEN FEED TUE ENTERS IT.SDR CWQR061DBolt · seizedRUST ON SUPPORT ASSY FROM FLAP BELLCRNK ASSY. UPON REMOVAL FOUND BOLT (PIVOT) SEIZED TO BEARINGS, SPACER. BEARINGS ARE FACTORY LUBED AND NOT FIELD LUBED. ALSO, BOLT IS INSTALLED DRY (NO LUBE). ALSO, NO INSPECTION CALLED OUT TO CHECK ON LUBE OF THESE COMPONSDR 96ZZZX398Seal · defectiveDURING INSPECTION, FOUND TKS ANTI-ICE FLUID LEAKING FROM RIGHT SIDE OF NOSE WHEELWELL. TRACED LEAK TO AFT SIDE OF FORWARD PRESSURE BULKHEAD. FOUND O-RINGS ON FORWARD PRESSURE BULKHEAD FITTINGS DEFECTIVE AND PUDDLE OF TKS FLUID IN FLOOR BOARDS. REPLACED O-RI
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)