- Owner type
- Co-owned
- Serial number
- 20641
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- September 25, 2016
- Certificate issued
- September 29, 2026
- Expires
- September 30, 2033
- Mode S code
- AACC07
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 N795QSMatched 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 N795QSMatched 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 DXTA2025060203707Guide Fitting · faultedWHILE OPENING MAIN DOOR AFTER A FLT, FO NOTED MAIN DOOR DIFFICULT TO OPEN. ATTEMPT TO CLOSE & OPEN DOOR & NO ISSUES. ON 2ND FLT, DIFFICULT TO OPEN. ONCE DOOR CYCLED 1 TIME, EASY TO CLOSE & OPEN. OPENED & CLOSED MED WITH NO DEFECTS NOTED. PRESSURIZED ACFTSDR DXTA2025050403348Door Frame · damagedFUSELAGE DOOR FRAME: WHEN OPENING THE MAIN CABIN DOOR THERE WAS A POPOING NOISE AND THE DOOR WAS EXTREMELY DIFFICULT TO OPEN. CORRECTIVE ACTION: BEGAN TROUBLESHOOTING. POWERED UP AIRCRAFT AND PERFORMED OPS CHECKS OF MED MULTIPLE TIMES WITH NO DEFECTS. GAINED ASDR DXTA2025043003280Pin · lack of lubeMAIN CABIN DOOR JAMMED WHILE TRYING TO OPEN IT FROM THE INSIDE. THE HANDLE WOULDN'T MOVE FAR ENOUGH TO MOVE THE ROLLERS OUT OF THEIR TRACKS. WE RESEATED THE DOOR FULLY INTO THE SECURE POSITION, TRIED AGAIN AND HAD THE SAME RESULT 3 TIMES. ON THE FOURTH TRY THESDR DXTA2025013102146Handle · faultedMAIN DOOR HANDLE: MAIN DOOR UNLOCK AND RELEASE IS INTERMITTENT WHEN USING INTERIOR HANDLE.SDR DXTA2023090694720Acm · faultedDEPARTED, SHUT DOWN APU, TURNED OFF BLEEDS, THEN SMOKE APPEARED IN THE COCKPIT. ALSO SMELL OF BURNT OIL. RETURNED FOR LANDING. REMOVED FAILED ACM PN:3471A020000 SN 00734 AND INSTALLED CUSTOMER SUPPLIED MODIFIED ACM PN: 3471A020000 SN: 00430. PERFORMED SATISFSDR DXTA2023063089880Rod · damagedENTRANCE STAIR EXTENSION: AIR STAIR DOOR OPENS NORMALLY BUT WHEN I STEPPED ON THE STAIRS THE HANDLE JUMPS FROM ITS'S OVER-CENTER POSITION TO AN UNSECURED POSITION AND THE DOOR DROPS TO A POSITION ABOUT 1/2 INCH FROM THE GROUND AND BINDS AGAINST THE FUSELAGE. SDR DXTA2023042184680Engine · defectiveR ENGINE VIBRATION AMBER CAS: ON DECENT IN KAFW THRU FL340, GOT A VIBRATION BROUGHT THROTTLES BACK, ONE AT A TIME & FELT RT ENG VIBRATING. THE AMBER RT ENG VIBE CAS ILLUM. RAN CHKLIST & LT IT AT IDLE ROUGHLY 10 MINS, LATER RT ENG FLAMED OUT MESSAGE ILLUM. SDR DXTA2022101071830Door · unknownMAIN DOOR: HEARD A LOUD POP AS A CREW MEMBER WALKED UP THE STAIRS. IT LOOKS LIKE IT IS HANGING LOWER NOW AND CONTACTS THE FUSELAGE WITH WEIGHT ON THE DOOR. WE ATTEMPTED TO CLOSE DOOR AND IT REMAINS APPROX 4" OPEN AND WILL NOT SECURE. PERFORMED EXTERNAL GVI OFSDR DXTA2016102608323Bleed Valve · unstableAFTER TAKEOFF WITH ENGINES AT CLIMB POWER, THE L PYLON BLEED LEAK RED CAS MESSAGE ILLUMINATED. THRUST LEVER WAS REDUCED TO IDLE IAW CHECKLIST. AFTER APPROX 1 MINUTE THE MESSAGE CLEARED. ENGINE WAS LEFT AT IDLE WHILE WE RETURNED FOR LANDING. REMOVED AND REPLACESDR DXTA2016102606323Warning Message · false activationAFTER TAKEOFF WITH ENGINES AT CLIMB POWER, THE LT PYLON BLEED LEAK RED CAS MESSAGE CAME ON. THRUST LEVER WAS REDUCED TO IDLE PER CHECKLIST. AFTER APPROX 1 MINUTE THE MESSAGE CLEARED. ENGINE WAS LEFT AT IDLE WHILE WE RETURNED FOR LANDING.
Reports on N795QS not matched to an aircraft · 5
They name N795QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA200701975Unknown · smokeDISTINCT SMELL OF ELECTRICAL SMOKE IN CABIN AND COCKPIT AND A NOTICEABLE HAZE OF SMOKE VISIBLE. OPERATED GROUND TEST APU TWICE FOR APPROX 20-25 MIN IAW 650 MM 49-10-00. NO NOTICEABLE SIGNS OF SMOKE IN CABIN. RAN CABIN TEMP TO FULL HOT AND COLD. BITE CHECKED SDR DXTA200601472Acm · leakingDURING FLIGHT FROM GSO TO LUK, REAR ACM LEAKING OIL WITH STRONG ODOR IN CABIN. AIRCRAFT CONTINUED AND LANDED AT LUK. REMOVED AND REPLACED REAR ACM, INSTALLED AN OVHD UNIT OF THE SAME P/N WORK DONE IAW HAMILTON STANDARD MM 21-50-03. SERVICED TO PROPER LIMITS.SDR DXTA200500988Smoke Detector · faultyDURING THE TAKEOFF ROLL, THE RED "SMOKE DETECT" LIGHT CAME ON TRIGGING THE MASTER WARNING, DURING THE TAXI BACK TO THE FBO THE LIGHT AND MASTER WARNING KEPT ON ILLUMINATING AND FLASHING. TROUBLESHOT SYSTEM AND FOUND SMOKE DETECTOR BOX FAULTY. REMOVED DEFECTI
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