- Owner type
- Co-owned, fractional ownership
- Serial number
- 9732
- Year built
- 2015
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- June 14, 2016
- Certificate issued
- October 11, 2025
- Expires
- October 31, 2032
- Mode S code
- A03C7E
Bombardier BD-700-1A11TCDS T00003NYAirframe · Bombardier BD-700-1A11TCDS E00057ENEngine · Rolls-Royce Deutschland BR700-710A220
From the FAA registry file of October 24, 2026.
On this page
Airworthiness directives that may apply · 71
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 | 2 |
| 2008 | 1 |
| 2009 | 1 |
| 2010 | 1 |
| 2011 | 4 |
| 2012 | 1 |
| 2013 | 2 |
| 2014 | 2 |
| 2015 | 1 |
| 2016 | 6 |
| 2017 | 4 |
| 2018 | 5 |
| 2019 | 3 |
| 2020 | 5 |
| 2021 | 5 |
| 2022 | 4 |
| 2023 | 10 |
| 2024 | 4 |
| 2025 | 7 |
| 2026 | 6 |
Airframe · Bombardier BD-700-1A11
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 N114QSMatched 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-700-1A11 aircraft
FAA incident reports
No FAA accident or incident reports matched to N114QSMatched 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-700-1A11 aircraft
Reports on N114QS not matched to an aircraft · 1
They name N114QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another 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 DXTA2025092905092Contactor · faultedDURING POWER UP CHECKS ON PREFLIGHT, RED SMOKE AVIONICS BAY CAS MESSAGE AND AUDIO CAME ON. AFTER PERFORMING THE SMART OPS PROCEDURE FOR AN ASSOCIATED ELEC SYS FAULT MESSAGE THE CAS MESSAGE CLEARED. AFTER ENGINE START THE SAME RED SMOKE AVIONICS BAY CAS MESSAGESDR DXTA2021112252340Autobrake Sys · faultedAUTOBRAKE FAIL AMBER CAS: ON FINAL ON INITIAL APPROACH, AMBER AUTOBRAKE FAIL AND CYAN BRAKE FAIL CAME ON. A GO-AROUND WAS INITIATED. ON THE SECOND APPROACH R INBOARD BRAKE FAIL CAME ON AFTER GEAR EXT. // SIGNOFF // ACCOMPLISHED LEAK CHECK OF RIGHT INBOARD BRAK
Reports on N114QS not matched to an aircraft · 18
They name N114QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2012061104995Landing Gear · unknownLANDING GEAR HANDLE PLACED DOWN, GEAR DID NOT EXTEND SLOW TO EXTEND. REMOVED CONNECTOR PLUG AND CHECKED PINS AND PLUG WITH NO DISCREPANCIES NOTED. CLEANED AND LUBRICATED SELECTOR HANDLE, SECURED CONNECTOR PLUG, AND PERFORMED MLG FUNCTIONAL CHECK. OPS CHECKESDR DXTA2011061704618Control Cable · out of rigINITIATED A 15 DEGREES LEFT TURN & HAD A BINDING IN SPOILER SYS. NO PROBLEMS ROLLING RT. AT 0-10 NORMAL 10-15 DEGREES BINDING BEGINS & AROUND 15, PRESSURE POPS OFF TO LESS THAN NORMAL. AT 18, NORMAL PRESSURE & CONTROL. OBSERVED ON BOTH CONTROL COLUMNS AT MUSDR DXTA2011040104536Control Valve · inoperativeON LANDING ROLLOUT, BRAKES ARE HARD AND NON-RESPONSIVE ON INITAL APPLICATION. BRAKES ARE THEN SOFT AND GRAB AS IF ANTI SKID HAS FAILED. R & R BRAKE VALVE ASSY. OPS AND LEAK CHECKED GOOD. WORK DONE IAW MM: 32-40-00.
See all 18 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