- Owner type
- Co-owned, fractional ownership
- Serial number
- 20638
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- July 28, 2016
- Certificate issued
- March 17, 2026
- Expires
- March 31, 2033
- Mode S code
- AAC850
Bombardier BD-100-1A10TCDS T00005NYAirframe · Bombardier BD-100-1A10TCDS E00010LAEngine · Honeywell AS907-2-1A
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 55
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 2006 | 1 |
|---|---|
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 2 |
| 2012 | 2 |
| 2013 | 1 |
| 2014 | 1 |
| 2015 | 2 |
| 2016 | 2 |
| 2017 | 5 |
| 2018 | 4 |
| 2019 | 3 |
| 2020 | 3 |
| 2021 | 6 |
| 2022 | 5 |
| 2023 | 9 |
| 2024 | 8 |
| 2025 | 1 |
| 2026 | 3 |
Airframe · Bombardier BD-100-1A10
AD 2026-13-02NavigationAD 2026-02-06Flight controlsAD 2026-01-07Time Limits/Maintenance ChecksInformation bulletins that may apply · 2
Advisory, not mandatory.
Airframe · Bombardier BD-100-1A10
SAIB AIR-22-02R1Pitot/Static Anti-Ice SystemSAIB NM-18-32R1Electrical Power - Direct Current Power CenterNTSB investigations
No NTSB investigations matched to N794QSMatched 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 Bombardier BD-100-1A10 aircraft
FAA incident reports
No FAA accident or incident reports matched to N794QSMatched 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 Bombardier BD-100-1A10 aircraft
Service difficulty reports · 10
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026031307220Warning Message · false activationINFLIGHT CYAN EICAS 'FIRE SYS FAULT' DISPLAYED. B3-008147 CANNOT DUPLICATE ISSUE. DISCONNECTED CONNECTOR A91P2 AT THE FIREX CONTROL UNIT AND PERFORMED A RESISTANCE CHECK FROM PIN 17 TO PIN 18. TOTAL RESISTANCE SHOULD BE AROUND 11.67 OHMS AND THE MULTIMETER WSDR DXTA2025120105885Trim Tab · excess playIN CLIMB THROUGH APPROX 15,000 FT , WAS HAND FLYING AUTO PILOT OFF, EXPERIENCED WHAT WOULD BE CALLED A MODERATE OR HIGHER FLUTTER IN CONTROL COLUMN, WITH A MILD ROLL BACK IN FORTH, LT TO RT IN ROLL AXIS. CLIMBING ON PROFILE OF 280 KNOTS. CONDITION WAS EXPESDR DXTA2025070204099Shutoff Valve · defectiveOUTBOARD BREAKS FAIL CAS DURING PARKING AT THE RAMP WITH ENGINES RUNNING AND HYDRAULIC SYSTEM ON AND NORMAL PRESSURE. REPLACED OB BRAKE SHUT OFF VALVE IAW CL350 AMM 32-43-25. OPERATIONAL TEST CARRIED OUT SERVICEABLE.SDR DXTA2025011501953Unknown · vibrationINFLIGHT VIBRATION (EXCEPT ENGINE): DURING DESCENT WITH AUTOPILOT ON WHILE PASSING THROUGH 25000FT AND 310KIAS, WE OBSERVED A NOTICEABLE VIBRATION THROUGH BOTH YOKES. THIS VIBRATION CONTINUED THROUGHOUT THE REST OF THE DESCENT AND WAS MOST PRONOUNCED ABOVE 25SDR DXTA2024011510609Unknown · unknownMAIN DOOR WILL NOT CLOSE. BOTH POWER ASSIST AND MANUAL ATTEMPTS FAILED. DOOR IS BINDING AT THE TOP OF THE CLOSING, STOPS, THEN FALLS OPEN. DOOR NOT COMPLETELY IN THE FULL OPEN POSITION. ONCE AIRCRAFT WAS PLACED IN HANGER, TECHS CAREFULLY OPENED AND SUPPORT MESDR DXTA2023112010092Switch · defectiveON INITIAL CLIMB OUT WITH THE AUTO PILOT OFF THE RUDDER TRIM WENT HARD RIGHT. IT WAS SO VIOLENT WE THOUGHT WE HAD AN ENGINE FAILURE. WE GOT THE TRIM RE-CENTERED, ENGAGED THE AUTO PILOT, AND THE RUDDER TRIM WENT HARD, RIGHT A SECOND TIME. WE DISENGAGED THE AUTSDR DXTA2023032783180Acm · defectiveCABIN SMOKE: AFTER CLEARING THE RUNWAY AND SWITCHING FROM ENGINE BLEED AIR TO APU BLEED AIR, A BURNING SMELL STARTED COMING FROM THE A/C VENTS FOLLOWED BY A HAZE IN THE CABIN. WE THEN SWITCHED OFF THE APU AIR AND THE SMELL AND HAZE DISSAPPATED AFTER A COUPLE OSDR DXTA2022082969070None · noneIMMEDIATELY FOLLOWING ROTATION, WEIGHT OFF WHEELS, THE PASSENGER DOOR, AMBER CAS MESSAGE DISPLAYED. WE RETURNED TO LAND, AND AS SOON AS THE AIRCRAFT WAS WEIGHT ON WHEELS, THE MESSAGE EXTINGUISHED. TWO B3 CODES WERE CAPTURED IN FAULT HISTORY; B3-007469 FOR A DOSDR DXTA2021061743840Wire Harness · defectiveENGINE OIL STORAGE: ONE HOUR INTO THE FLIGHT AT FL400 A CYAN L ENGINE OIL BYPASS MESSAGE ILLUMINATED. NO FAULT CODES AIRBORN OR POSTFLIGHT WERE AVAILABLE. //SIGN OFF// REMOVED LH ENGINE WIRING HARNESS INSTALLED NEW LH ENGINE WIRE HARNESS IAW HONEYWELL AS907-ZSDR DXTA2018021300584Oil System · out of adjustCLIMBING THROUGH 11000, EXPERIENCED LT ENGINE OIL PRESSURE HIGH. FOLLOWED BY A RT ENG OIL PRESSURE HIGH. STOPPED THE CLIMB IAW QRH TO EXTINGUISH THE LIGHTS WAS TO ALMOST PULL POWER TO IDLE. DECLARED AN EMERGENCY. PERFORMED OIL PRESSURE ADJUSTMENT IAW MM
Reports on N794QS not matched to an aircraft · 4
They name N794QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA200500837Oil System · overservicedAFTER STARTING APU AND BLEED AIR ON, COULD NOT CONTROL COCKPIT HEAT AUTO OR MANUAL. BLUE SMOKE FILLED COCKPIT. DUCT TEMPERATURE WAS 210 AND RISING WHEN BLEED AIR WAS TURNED OFF. SMOKE THEN DISAPPEARED. INVESTIGATED AND FOUND APU OVER SERVICED WITH OIL. SERVICSDR DXTA200500631Quick Disconnect · dirtyON LANDING BRAKE PEDALS FELT NORMAL, HOWEVER AIRCRAFT HAD DIFFICULTY COMING TO A STOP WITH HARD BRAKING ACTION PERFORMED. TROUBLESHOT SYSTEM, FOUND RT MAIN GEAR STRUT SQUAT SWITCH ELECTRICAL CONNECTOR VERY DIRTY. CLEANED CONNECTOR, OPS CHECK GOOD, REF CITATISDR 99ZZZX2552Oxygen Mask · defectiveINSPECTED AIRCRAFT FOR COMPLIANCE OF AD 99-08-21 PURITAN BENNETT PASSENGER OXYGEN MASKS. OXYGEN MASK INSTALLED IN AIRCRAFT WERE NOT FULLED LISTED.
STCs that may be installed · 141
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 141 STCs