- Owner type
- Co-owned, fractional ownership
- Serial number
- 20629
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 28, 2016
- Certificate issued
- August 6, 2025
- Expires
- August 31, 2032
- Mode S code
- AABD2B
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 N791QSMatched 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 N791QSMatched 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 · 8
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026042307719Bearing · faultedDOOR OPENS NORMALLY, BUT AS YOU WALK DOWN THE STAIRS, IT THUDS LOWER AND SUPPORT MECHANISM FAILS AND DOOR PRESSES AGAINST FUSELAGE. DOOR HANDLE ALSO RAISES UP SLIGHTLY FROM NORMAL POSITION. REMOVED AND REPLACED OPEN LOCK SHAFT OUTER BEARING IAW AMM 52-11-05 SDR DXTA2025121806150Acm · seizedDURING FLIGHT, CREW NOTICED A WHISTLING SOUND AND ODOR ENROUTE. AS FLIGHT PROGRESSED, CREW AND PAX NOTICED SMOKE. WE SWITCHED FROM ENGINES TO APU BLEED AND IT IMPROVED TO NORMAL. AS WE CONTINUED ON APPROACH, THE WHISTLING STARTED AGAIN ON APU AIR. ECS SYSTEM DSDR DXTA2025090304776Door · faultedAS PASSENGER WAS DESCENDING DOWN THE MAIN STEPS THE PASSENGER DOOR MADE A VERY LOUD POP AND DROPPED ABOUT 1-2 INCHES. WHEN YOU STEP ON THE STAIRS THEY SAG/DROP AND THE PART OF THE STAIRS FUSELAGE NEAR THE PLANE (UNDERNEATH THE TOP OF THE STAIRS) MOVES UP AND HSDR DXTA2024091100492Control Valve · defectiveINBD BRAKES FAIL AMBER CAS: INBOARD BRAKE FAIL. B3-007102 CORRECTIVE ACTION: REMOVED FAULTY LH BRAKE CONTROL VALVE ASSY AND INSTALLED AN OVERHAULED LH BRAKE CONTROL VALVE ASSY !AW CL 350 AMM 32-43-09-400-801. NO DEFECTS NOTED. OPS CHECK GOOD.SDR DXTA2023020679900Control Unit · defectiveOUTBD BRAKES FAIL AMBER CAS: ON THE GROUND, WE RECEIVED THE CAS MESSAGE. ALL HYDRAULIC PRESSURES WERE NORMAL. DIAGNOSTIC CODE IS B3-006383. // SIGNOFF// YCRILICD BRAKE ACCUMULATOR PRESSURE. APPLIED POWER TO THE AIRCRAFT. STARTED APU.
NO CURRENT OUTBD DRAKES FSDR DXTA2022082969230None · noneLEFT ENGINE ENGINE HARDWARE: ON CLIMB OUT PASSING 13000 FEET AIRCRAFT SHOOK WITH A LOUD BANG. AFTER A FEW SECONDS THE AMBER L ENGINE VIBRATION MESSAGE CAME ON. IMMEDIATELY RETARDED LEFT THROTTLE TO IDLE. NO ADVERSE INDICATIONS FROM ENGINE INSTRUMENTS. AT ISDR DXTA2021072845910Acm · defectiveON SHORT FINAL TO BCT NOTICED SLIGHT ODOR IN COCKPIT WITH ENGINE BLEEDS ON. AFTER LANDING & SWITCHING TO APU BLEED, LIGHT SMOKE OBSERVED IN COCKPIT & CABIN. RAPID TEMPERATURE INCREASE, THEN PACK TEMP HIGH AMBER CAS MESSAGE ILLUMINATED. PERFORMED QRH PACK TEMP SDR DXTA2017112200001Engine · power lossDURING TAKEOFF AT ABOUT 1000', RT ENGINE STARTED BANGING AND POPPING. AIRPLANE BEGAN TO YAW LIKE AN ENGINE FAILURE. ITT WAS RED AT ABOUT 1120. RED CASS MESSAGE SAID "ENGINE EXCEEDANCE". WE BROUGHT THROTTLE TO IDLE AND THEN ALL WAS NORMAL. FLEW WITH ENGINE AT
Reports on N791QS not matched to an aircraft · 10
They name N791QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA200701933Wire · brokenRT ENGINE FIRE DETECT ANUNCIATOR ILLUMINATED AFTER COCKPIT PREP WAS COMPLETED. T/S TO BROKEN RT FIRE LOOP ON ENG. REMOVED & REPLACED FIRE LOOP. BLEED T/R'S, SYSTEM OP'S CHECKS SATISFACTORY AT THIS TIME. ALL WORK DONE IAW CE 650 M/M 26-10-01SDR DXTA200500969Line · brokenHYDRAULIC LINE IN RIGHT MAIN GEAR WELL BROKE AFTER T/O HAD TO BLOW GEAR DOWN AND USE ALL BACKUP SYSTEMS HAD RIGHT AND LEFT HYD LOW VOLUME AND PRESSURE LIGHTS. ITEM IS UNDER INVESTIGATION.SDR DXTA200500883Smoke · detectedON THE GROUND WITH APU RUNNING THE COCKPIT FILLED WITH BLUE SMOKE AND THE COCKPIT SUPPLY AIR TEMPERATURE WAS 170 DEGREES AND CLIMBING WITH THE TEMPERATURE CONTROL IN FULL COLD.
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