- Owner type
- Co-owned, fractional ownership
- Serial number
- 20732
- Year built
- 2018
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- April 26, 2018
- Certificate issued
- July 31, 2026
- Expires
- July 31, 2033
- Mode S code
- AA2A54
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 N754QSMatched 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 N754QSMatched 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 · 4
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026101610172Nut · looseEVERYTHING WAS NORMAL IN ALL PHASES OF FLT, EXCEPT TAKEOFF WHEN GEAR WAS RETRACTED, A GRINDING, OR THUMPING SOUND HAS HEARD, FOLLOWED BY A VIOLENT SHAKING VIBRATION THROUGH PLANE, CONTINUES AFTER TRACTION FOR A FEW SECS & THEN STOPPED. EVERYTHING NORMAL DURSDR DXTA2026072108896Adc · defectiveDURING SHORT FLIGHT, JUST AFTER LEVELING OFF AT 12,000', AMBER EFIS MISCOMPARE AND ALT FLAG (ON PFD2) DISPLAYED. THE RIGHT, PFD2 DISPLAYED A 140' LOW DIFFERENCE COMPARED TO THE LEFT PFD1. BOTH MESSAGES DISAPPEARED ONCE WE STARTED OUR DESCENT. QRH PROCEDURESDR DXTA2024101500835Sensing Element · defectiveBLEED AIR: 13 MINUTES AFTER TAKE OFF APOX 32000 FT RED LEFT BLEED LEAK MASTER WARNING ILLUMINATED ALONG WITH RED EICAS. RAN QRH PROCEDURE WARNING WENT AWAY. RETURED TO KLAS B3-007016 CORRECTIVE ACTION: COMPLIED WITH REMOVAL OF LH BLEED LOOP SENSING ELEMENT DSDR DXTA2024091800568Transducer · failedOUTBD BRAKES FAIL AMBER CAS: ON TAXI OUT NOTICED OUTBD BRAKES FAIL AMBER CAUTION MESSAGE. RAN THROUGH OUR CHECKLIST AND THEN TAXI BACK TO THE RAMP. MESSAGE STILL REMAINS AFTER SHUTDOWN. B3 007836 IS THE B3 CODE. CORRECTIVE ACTION: BRAKE FAIL CAS. REPLACED R
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