- Owner type
- Co-owned, fractional ownership
- Serial number
- 9615
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 16, 2014
- Certificate issued
- June 11, 2026
- Expires
- June 30, 2033
- Mode S code
- A0BA69
Bombardier BD-700-1A10TCDS T00003NYAirframe · Bombardier BD-700-1A10TCDS E00057ENEngine · Rolls-Royce Deutschland BR700-710A220
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 75
Matched by this aircraft’s airframe and engine models. Each AD’s applicability may narrow it by serial number, part number or equipment.
| 1999 | 1 |
|---|---|
| 2001 | 2 |
| 2003 | 1 |
| 2005 | 1 |
| 2006 | 3 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 2 |
| 2011 | 4 |
| 2012 | 1 |
| 2013 | 2 |
| 2014 | 2 |
| 2015 | 2 |
| 2016 | 6 |
| 2017 | 4 |
| 2018 | 5 |
| 2019 | 3 |
| 2020 | 5 |
| 2021 | 7 |
| 2022 | 4 |
| 2023 | 10 |
| 2024 | 4 |
| 2025 | 8 |
| 2026 | 6 |
Airframe · Bombardier BD-700-1A10
AD 2026-15-09Landing GearAD 2026-11-07Equipment/furnishingsAD 2026-13-02NavigationInformation bulletins that may apply · 3
Advisory, not mandatory.
Historical bulletins · 1
NTSB investigations
No NTSB investigations matched to N146QSMatched 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-700-1A10 aircraft
FAA incident reports
No FAA accident or incident reports matched to N146QSMatched 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-700-1A10 aircraft
Service difficulty reports · 3
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026031107170Receptacle · brokenAFTER TAKEOFF GEAR WOULD NOT RETRACT. CYCLED ONCE STILL WOULD NOT RETRACT. WHEN GEAR HANDLE WAS UP WE GOT AN AMBER CAS GEAR DISAGREE. PUT GEAR HANDLE DOWN AND CONTINUED SHORT FLIGHT. REVIEWED PREVIOUS STEPS AND PROCEEDED WITH THE FOLLOWING; GAINED ACCESS TOSDR DXTA2024121101446Hand Rail · failedENTRANCE STAIR HAND RAIL: HAND RAIL HAS COME APART AT TOP OF THE STAIR. LEFT HAND SIDE ENTERING AIRCRAFT. THERE IS A SCREW MISSING EXTRACTED BROKEN SCREW FROM CABIN DOOR HANDLE EXTENSION. INSTALLED SCREW AS REQUIRED. P/N: MS24693-C23. OPS CHECKED GOOD. REF GSDR DXTA2018020700560Control Unit · failedAFTER GEAR SELECTED DOWN, A BRAKE FAULT CAS MESSAGE AND AUTOBRAKE FAIL CAS MESSAGE ILLUMINATED. ON TOUCHDOWN THE LEFT BRAKE DRAGGED AND SHIMMIED. RIGHT BRAKE WAS USED TO STOP PLANE. REMOVED AND REPLACED THE LT OTBD BRAKE CONTROL VALVE AND BCU. OPS AND LEAKS
STCs that may be installed · 432
Approved for this aircraft’s airframe or engine model. The registry doesn’t record which STCs an aircraft has; its records do.
See all 432 STCs