- Owner type
- Co-owned, fractional ownership
- Serial number
- 20792
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Certificate issued
- September 26, 2025
- Expires
- September 30, 2032
- Mode S code
- A955FD
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 54
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 | 3 |
| 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 N700QSMatched 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 N700QSMatched 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
Reports on N700QS not matched to an aircraft · 1
They name N700QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
Service difficulty reports · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026082109351Proximity Sensor · faultedON APPROACH TO LANDING WITH GEAR SELECTED DOWN, CAS MESSAGE PROX SYS FAULT APPEARED B3-224420. REPEAT WRITE UP. ON LANDING ROLLOUT, AFTER SIGNIFICANT SHUDDERING (LIKE A FLAT SPOT ON ALL TIRES) CAS MESSAGE BREAK FAULT APPEARED B3-007414. REMOVED INTERMITTENTSDR DXTA2025081504618Transducer · out of adjustAIRCRAFT PULLS TO THE LEFT WHILE TAXING. CONSTANT RIGHT TILLER OR RUDDER IS REQUIRED. AIRCRAFT PULLS HARDER TO THE LEFT WHEN MODERATE BRAKING IS APPLIED. PERFORMED RIGGING CHECK OF ROTARY VARIABLE TRANSDUCER & FOUND RVT OUT OF LIMITS, PERFORMED RIGGING OFSDR DXTA2024031311184Transducer · defectiveAFTER TAKEOFF WE RECEIVED A R HYD TEMP HIGH AMBER CAS. RAN QRH. HYDRAULIC TEMP ON RIGHT SIDE EXCEEDED 155° (APPROXIMATELY 209°) AND PROCEEDED TO SHUTDOWN RT ENGINE IAW QRH. RECEIVED WHILE SETTING UP FOR LANDING: R HYD PRESS LOW FLAPS NORM PRESS LOW FLAPS FSDR DXTA2020100504171Dcu · faultedDCU B B3-006531 DCU "A" B3-006494 BRAKE FAULT B3-22442 UPON SELECTING GEAR DOWN WE GOT A MAGENTA BOX WITH DASHES ON THE RIGHT MAIN GEAR. WE ALSO GOT THE FOLLOWING CAS MESSAGES: GEAR DISAGREE, LEFT AND RIGHT THRUST REVERSER FAIL, BRAKE FAUL AND LEFT HYD TEMP H
Reports on N700QS not matched to an aircraft · 22
They name N700QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2013112005574Engine · damagedCLIMBING THROUGH 38000' IN MAX CLIMB DETENT 290KTS TWO DISTINCT BANGS, SIMILAR TO COMPRESSOR STALLS, WERE FELT THROUGH FLOOR, RUDDERS & CONTROLS. ALL INSTRUMENT READINGS WERE NORMAL EXCEPT 1/4 SCALE ON RT VIB METER. DISCONNECTED A/P DES TO 24000 SLOWED 250KTSSDR DXTA2012051104974Warning Light · illuminatedON APPROACH, AT 170KIAS THE LANDING GEAR WAS LOWERED. THE NOSE AND LT MAIN GEAR INDICATIONS WERE NORMAL. THE RT MAIN GEAR SHOWED AMBER FOR ABOUT 10 SECONDS FOLLOWED BY A RED INDICATION. THE ANTI-SKID FOR THE RT BRAKE INDICATED OFF. AFTER ABOUT 45 SECONDS THSDR DXTA2012030704907Selector Valve · leakingON GEAR EXTENSION, RECEIVED GREEN LIGHTS FOR LT MAIN AND NOSE GEAR BUT THE RT MAIN INDICATED YELLOW FOR APPROX 20 SECONDS FOLLOWED BY A RED "UNSAFE" INDICATION FOR ABOUT 30 SECONDS. ALSO SHOWED THE RT ANTISKID SYS INOPERATIVE. THE RT MAIN GEAR LIGHT THEN T
See all 22 unmatched reportsSTCs 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