- Owner type
- Co-owned
- Serial number
- 20617
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- April 21, 2016
- Certificate issued
- October 16, 2026
- Expires
- October 31, 2033
- Mode S code
- AAB364
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 N789QSMatched 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 N789QSMatched 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 · 6
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026080609135Control Valve · defectiveON TAKEOFF WE RECEIVED A LT OTBD BRAKE FAIL MESSAGE. THIS WAS FOLLOWED SHORTLY BY A R OTBD BRAKE FAIL MESSAGE. ABORTED. THE MESSAGES CAME ON AND OFF INTERMITTANTLY AFTER THAT. B3 CODES ARE AS FOLLOWS: B3-007830 AND B3-007107. REPLACED BRAKE CONTROL VALVE. OPSSDR DXTA2026020906810I/O Module · defectiveSHORTLY AFTER TAKE OFF WE STARTED EXPERIENCING A SERIES OF CAS MSGS. AT FIRST A FEW. THEN MANY. AT THE HEIGHT 2 PAGES FULL OF CAS MSGS. AT THE LAST 1/3 OF THE FLIGHT MOST HAD RESOLVED THEM SELVES AND WERE REDUCED TO A FEW. THESE ARE SOME OF THE CAS MSGS WE EXPSDR DXTA2025080704467Seal · faultedCLIMBING THROUGH 9000FT WE STARTED HEARING A LOUD WHISTLING WIND NOISE ALL THE WAY UP TO FL210. FIRST OFFICER WENT BACK AROUND 12,000FT AND SAID HE COULD SEE LIGHT THROUGH THE DOOR ON THE TOP LEFT HAND CORNER. THIS WAS FOLLOWED BY A FEW POPPING SOUNDS BELIEVEDSDR DXTA2025071504253Warning Message · false activationEMERGENCY EXIT YELLOW CAS MESAGE CAME ON WHILE CLIMBING THROUGH 10,000 FEET. RAN APPROPRIATE CHECKLIST AND RETURNED BACK TO ICT. ATTEMPTED TO VERIFY FAULT BUT COULD NOT RECREATE ON THE GROUND. PERFORMED OPERATIONAL TEST OF THE DOOR SENSORS, OPS TEST OF THE ESDR DXTA2025062503999Engine · failedON THE FINAL DESCENT AND TRANSITION TO THE APPROACH PHASE OF FLIGHT, CREW RECOGNIZED ENG VIBRATION & ISOLATED VIBRATION TO THE RT ENG. RT ENGINE VIBRATION AMBER CAS ILLUMINATED. CREW RAN QRH FOR CAS & ELECTED TO REMAIN MONITORING VIBRATION. CREW NOTICED RTSDR DXTA2021061743790Acm · odorCOCKPIT ODOR: IMMEDIATELY AFTER ROTATION AIRCRAFT ENCOUNTERED EXCESSIVE NOISE ASSOCIATED WITH AIRFLOW TO THE CABIN, AN ACRID SMELL, AND EXCESSIVE TEMPERATURE OF AIRFLOW FROM THE ENVIRONMENTAL SYSTEM. THE AIRFLOW NOISE WAS EXCESSIVE AND ABNORMAL AND INCREASED
Reports on N789QS not matched to an aircraft · 10
They name N789QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA200500652Smoke Detector · failedSMOKE DETECTION MASTER WARNING LIGHTS ILLUMINATED. REMOVED SMOKE DETECTOR CONTROL UNIT. REPLACED WITH REPAIRED UNIT IAW CHAP 26-12-00 OF THE CESSNA 650 MM. OPS CHECKED GOOD.SDR DXTA200500515Line · unknownON LANDING ROLL OUT,THE LEFT BRAKE PEDAL WENT TO THE STOP WITHOUT ANY BRAKING OCCURRING ON THE LEFT MAINS. TAXI CHECK A/C COULD NOT DUPLICATE. HOOKED UP PRESS GAUGES TO LT BRAKE ASSY APPLY HYD PRESS + GET 2000 PSI OUT OF BOTH BRAKE ASSY. BLED BRAKES. TAXI SDR DXTA200400400Converter · defectiveFLAPS INOPERATIVE ANNUNCIATOR ILLUMINATED AFTER TAKEOFF WITH FLAPS INDICATING UP, FLAP WOULD NOT RESET. DURING LANDING APPROACH FLAPS WOULD RESET AND OPERATE BUT FLAPS INOP ANNUNCIATOR REMAINS ILLUMINATED ON THE GROUND. TROUBLESHOT SYSTEM TO DEFECTIVE FLAP RE
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