- Owner type
- Co-owned, fractional ownership
- Serial number
- 21100
- Year built
- 2025
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 23, 2025
- Certificate issued
- December 31, 2025
- Expires
- December 31, 2032
- Mode S code
- A973B5
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 N708QSMatched 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 N708QSMatched 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 · 2
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026042907824Selector Valve · faultyON APPROACH WHEN SELECTING FLAPS 30 R HYD PRESS LOW ILLUMINATED AND R FLUID WAS LOST. FLAPS AND SPOILERS BOTH FAILED. REMOVED FAULTY SWITCHING VALVE P/N 975290-3, S/N PN1114 AND INSTALLED A CUSTOMER SUPPLY OVERHAULED VALVE P/N 975290-3, S/N 0267. TORQUED HYDSDR DXTA2026032307291Actuator · defectiveDEPARTED AIRPORT, AT 3000 FEET CLIMBING TO 5000 FT NOTED EXCESSIVE NOISE FROM MAIN DOOR. PRESSURE WAS ZERO & UPON DESCENT WAS OVER DESCENDING TO KEEP UP. UPON LANDING OUR LINEMAN MENTIONED THE CABLE VISIBLE AT MAIN CABIN DOOR/ WAS NOT THERE @ DEPARTURE REP
Reports on N708QS not matched to an aircraft · 14
They name N708QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2013053105408Outflow Valve · malfunctioned15 MINUTES INTO FLIGHT AT 31,000 FT, CABIN ALTITUDE REACHED 8500 & DISPLAY TURNED YELLOW. KEPT SLOWLY CLIMBING. RAN CHECKLIST & PUT IN MANUAL MODE, BUT STILL UNABLE TO CONTROL. CABIN ALTITUDE REACHED 10,000 FT, DESCENDED TO 15,000 FT. REACHING THAT ALTITUSDR DXTA2012012304851Unknown · odorFUEL ODOR IN CABIN. IT IS MOST NOTICABLE NEAR THE FORWARD COUCH SEAT. INSPECTED ENGINES, MLG WW, AND LAVATORY, NO LEAKS NOTED IAW 28-10-00.SDR DXTA2008122303430Brake · lockedLEFT BRAKE LOCKED ON LANDING BOTH LEFT MAIN TIRES BLOWN, WHEELS AND RIMS DESTROYED.
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