- Owner type
- Co-owned, fractional ownership
- Serial number
- 20704
- Year built
- 2017
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 7, 2017
- Certificate issued
- July 24, 2024
- Expires
- July 31, 2031
- Mode S code
- AA02D5
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 N744QSMatched 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 N744QSMatched 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 DXTA2026070608657Switch · failedINTERIOR EMERGENCY LIGHTS ABOVE SEAT 2L AND 3R DO NOT ILLUMINATE WHEN EMER LIGHT SWITCH IS PLACED TO ON. LIGHTS ILLUMINATE NORMALLY WITH CABIN LIGHT SWITCH TO ON.SDR DXTA2026032407360Seal · failedON TAKEOFF, A STRONG, DISTINCT ODOR WAS NOTICED AND LASTED THROUGHOUT THE FLIGHT. IT SMELLED LIKE BURNING WET LOCKER ROOM SOX AND NOW OUR CLOTHES HAVE THAT SAME ODOR. IN MY PAST, THIS WAS FOUND TO BE A BAD ACM SHAFT SEAL. CORRECTIVE ACTION: PERFORMED SERVICE SDR DXTA20240110726Acm · defectiveAPU (EXCEPT GENERATOR): AFTER LANDING AND SWITCHING THE BLEEDS OVER TO THE APU A FOUL ODOR WAS OBSERVED FOLLOWED BY A LOUD WHINING SOUND. THE FIRST OFFICER ALSO OBSERVED THAT HOT AIR WAS COMING OUT OF THE WEMAC LOCATED BELOW THE RIGHT COMM PANEL. WE TOOK THESDR DXTA2024072212428Pump · failedDURING FLIGHT AT FL240 WE FELT A STRONG VIBRATION, FOLLOWED BY A AMBER L HYD TEMP HIGH AND SHORTLY AFTER CYAN L HYD ENG PUMP FAIL. HYD SYS INDICATED 0% AND 109°. AN EMERGENCY GEAR EXTENSION WAS PERFORMED & ACFT WAS PINNED & TOWED TO RAMP. LARGE PUDDLES OF HYDSDR DXTA2024061212023Door · handler errorAFTER OPENING & STEPPING ON MAIN DOOR, IT MADE A NOISE & SEEM TO DROP A FEW MORE INCHES THAN NORMAL. APPEARED TO BE SLIGHTLY LOWER TO GROUND THAN NORMAL, COULD NOT SEE ANY DEFECTS. CLOSING DOOR FROM EXTERIOR WITH ELECTRONIC ASSIST, DOOR WOULD NOT GO UP FAR ENSDR DXTA2019110803041Hose · failedHYDRAULIC PUMP - UPON LOWERING LANDING GEAR, GEAR DISAGREE CAS ILUMINATED FOLLOWED QUICKLY BY L HYD PRESS LOW, BRAKE FAULT AND PROX SYS FAULT CAS MESSAGES. EXECUTED GEAR DISAGREE CHECKLIST AND LANDED ASAP. AFTER SHUTDOWN, OBSERVED EXCESSIVE LEAKING OF HYD FLUI
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