- Owner type
- Co-owned, fractional ownership
- Serial number
- 9479
- Year built
- 2012
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- December 26, 2012
- Certificate issued
- December 16, 2024
- Expires
- December 31, 2031
- Mode S code
- A0A7D6
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 N141QSMatched 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 N141QSMatched 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 · 7
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2024121601503Hand Rail · detachedMAIN ENTRANCE HAND RAIL DETACHES AND INTERFERES WITH MAIN ENTRY DOOR OPERATION WHEN DOOR IS RAISED FOR CLOSING. CORRECTIVE ACTION; INSPECT THE AREA AND FOUND THE MISSING SCREW ON THE RANDRAIL EXTENSION LOWER ATTACHING PIVOT FITTING REINSTALLED THE SCREW OPERATSDR DXTA2024120501358Unknown · odorCABIN POWER (60 HZ): ON TAXI IN AND AFTER ENGINE SHUTDOWN A BURNING ELECTRICAL SMELL CAME FROM THE CABIN. THE SMELL WAS STRONGEST IN THE AFT LAV AREA WITH VISABLE SMOKE. THE SMELL AND SMOKE DISSIPATED ONCE CABIN POWER WAS TURNED OFF AND EVEN MORE AFTER THE APSDR DXTA2023092696470Unknown · unknownMAIN EXIT SIGN/LIGHT: EMERGENCY LIGHTS ABOVE THE MAIN ENTRANCE, DOOR, FLICKERING LIKE A SHORT IN THE SYSTEM AND THE EMERGENCY LIGHT ABOVE THE EMERGENCY EXIT OR NOT ILLUMINATING AT ALL DURING TEST. SOME OF THE OTHER EMERGENCY LIGHTS WERE NOT WORKING THROUGHOUT SDR DXTA2023020780050Actuator · defectiveMAIN DOOR: WHILE CLOSING THE MAIN CABIN DOOR, IT CAME CRASHING DOWN VERY FAST. BOTH HOLLOW SIDE BARS BROKE IN DIFFERENT AREAS. DOOR WILL NOT CLOSE ELECTRONICALLY // SIGNOFF// GAINED ACCESS TO MED STAIR ACTUATOR VIA STAIR LIGHT PANELS. REMOVED AND REPLACED SDR DXTA2022060863510None · noneMAIN HYDRAULICS: DURING CRUISE FLIGHT AT FL 430, HYD SYSTEM 2 QUANTITY WENT TO 0%. COMPLETED HYD 2 LO QTY QRH CHECKLIST. SYSTEM PRESSURE WAS HOLDING AT 3000 PSI SO WE CONTINUED ON TO DESTINATION. AFTER APPROXIMATLEY 1 HOUR, HYD SYSTEM PRESSURE BEGAN TO DROPSDR DXTA2020103104297Acm · failedSMOKE IN CABIN AND COCKPIT. NO CAS MESSAGES SHOWN. LOUD UNDULATING GRINDING NOISE FROM LEFT PACK. GAINED ACCESS AND REMOVED DEFECTIVE ACM P/N GG431-2010-3 S/N 01089 AND INSTALLED CUSTOMER SUPPLIED REPAIRED ACM P/N GG431-2010-3 S/N 00201. REINSTALLED ALL ACSDR DXTR2015010701Battery · failedLEFT AND RIGHT CLASS 3 ELECTRONIC FLIGHT BAG, EFB, WILL NOT DISPLAY IMAGE. APPEARS TO BE RECEIVING POWER. R & R LT AND RT ELECTRONIC FLIGHT BAG DISPLAYS AND RELOADED EFB SOFTWARE IAW SOFTWARE LOAD PROCEDURE FOR L3 EFB DOC 945-6731-001. EFB DISPLAYS GROUND C
Reports on N141QS not matched to an aircraft · 13
They name N141QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2011031604510Switch · intermittentHORIZONTAL STAB FAIL LIGHT ILLUMINATED IN FLIGHT. INSTALLED A NEW SWITCH. ACCOMPLISHED HORIZONTAL STAB PITOT STATIC TEST, NO DEFECTS NOTED. ACCOMPLISHED HORIZONTAL STAB SELF TEST. NO DEFECTS NOTED. ACCOMPLISHED HORIZONTAL STAB HEAT OPS TEST, NO DEFECTS NOTSDR DXTA2011030904499Uplock · intermittentUPON GEAR RETRACTION, 3 GREEN LIGHTS EXTINQUISHED BUT RED LIGHT IN GEAR HANDLE REMAIN ILLUMINATED RED. REPLACED THE NLG UPLOCK ASSY WITH A NEW ASSY IAW MM 32-20-00. PERFORMED A NCG AND MCG FUNCTIONAL CHECK WITH NO DEFECTS AT THIS TIME IAW MM 32-20-00.SDR DXTA2011030304485Uplock Switch · malfunctionedAFTER TAKEOFF AND GEAR RETRACTION SELECTED, THE 3 GREEN LIGHT EXTINGUSHED, BUT THE RED LIGHT REMAINED ILLUMINATED. CLIMBED TO 6000FT ON THE AUTOPILOT. AFTER 3, 90 DEGREE TURNS ON THE AUTOPILOT WE FELT A HARD BUMP FROM THE UNDERSIDE OF THE AIRPLANE AND THEN THE
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