- Owner type
- Co-owned, fractional ownership
- Serial number
- 9632
- Year built
- 2014
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 27, 2015
- Certificate issued
- July 8, 2026
- Expires
- July 31, 2033
- Mode S code
- A0BE20
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 N147QSMatched 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 N147QSMatched 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 · 5
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2024112001189Chain · corrodedMAIN DOOR: AS THE AIRCRAFT REACHED CRUISE ALTITUDE, A LOUD BANGING SOUND CAME FROM THE MAIN CABIN DOOR. THE CABIN DIFFERENTIAL WAS AT 9.7. NO FLUCTUATION IN CABIN PRESSURIZATION WAS NOTED. CABIN ALTITUDE REMAINED AT 4500. WAITED FOR LINE SERVICE TO BRING THE ASDR DXTA2023040383540Unknown · unknownMAIN DOOR UPPER HANDLE DISCONNECTED FROM LOWER ASSEMBLY. NEEDS MISSING FASTER. OTHER SIDE ALSO LOOSE. RESECURED AFT UPPER MAIN DOOR HANDRAIL. REPLACED MISSING SCREW FROM FORWARD LOWER HANDRAIL EXTENSION ATTACH POINT. PERFORMED SEVERAL OPS CHECKS WITH NO DEFSDR DXTA2023031382460Tube · damagedDURING CLIMB OUT GOT A HYD 1 LO PRESS CAS MSG. LOOKING AT THE HYD SYNOPTIC #1 QTY SHOWS 0 & HYD 1 PRESSURE WAS 0. AFTER GAINING ACCESS TO AFT ACCESSORY COMP NOTED HYD FLUID SATURATING AREA. ON FURTHER INSP NOTED #1 ENG HYD RETURN LINE LOOSE & CHAFING BRACKET SDR DXTA2022052362460None · noneMAIN DOOR: WHEN HOLDING THE DOOR CLOSE BUTTON, YOU HAVE TO HOLD THE BUTTON, UNTIL THE DOOR IS COMPLETLY UP. IF YOU LET GO AT ANYTIME BEFORE THE DOOR FREE FALLS TO THE OPEN POSITION.SDR DXTA2015083106070Brake Sys · malfunctionedTHE BRAKES ARE VERY GRABBY DURING ALL PHASES OF GND OPERATION. LT BRAKE TEMPS ARE MUCH HIGHER THAN THE RT SIDE. STRONG PULSING WITH LIGHT BRAKE APPLICATION. PERFORMED OPS CHECKS WITH NO DEFECTS NOTED. PERFORMED PRESSURE CHECKS VIS OMS WITH NO DEFECTS NOTE
Reports on N147QS not matched to an aircraft · 7
They name N147QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2012030204897Brake · smokeAFTER LANDING, SMOKE WAS NOTICED FROM LT MLG. R & R BRAKE ASSY. OPS AND LEAK CHECKED GOOD. ALL WORK PERFORMED IAW MM 32-40-00.SDR DXTA2009110503846Transducer · inoperativeBRAKE PEDALS REQUIRE EXCESSIVE AMOUNT OF FORCE TO ENGAGE BRAKES. BRAKES CATCH UNEVENLY. REMOVED LT WHEEL TRANSDUCER. INSTALLED OVERHAULED TRANSDUCER. OPS CHECKED GOOD. IAW MM 32-40-00-201. REMOVED RT WHEEL TRANSDUCER. BENCHED CHECKED GOOD. INSTALLED TRANSDR DXTA2009102903829Filter · dirtyBRAKE PEDALS REQUIRE EXCESSIVE AMOUNT OF FOURCE TO ENGAGE BRAKES, BRAKES CATCH UNEVENLY. REMOVED AND CLEANED BRAKE CONTROL VALVE FILTERS, REINSTALLED, LEAK CHECKED GOOD. INSPECTED WHEEL TRANSDUCERS, AND BRAKES WITH SATISFACTORY RESULTS. BLEED BRAKE SYSTEM, TA
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