- Owner type
- Co-owned, fractional ownership
- Serial number
- 9768
- Year built
- 2016
- Type
- Fixed wing multi engine
- Engine
- Turbo-fan
- Airworthiness
- Standard, transport
- Airworthiness date
- March 30, 2017
- Certificate issued
- June 12, 2026
- Expires
- June 30, 2033
- Mode S code
- A043EC
Bombardier BD-700-1A11TCDS T00003NYAirframe · Bombardier BD-700-1A11Engine modelRolls-Royce BR-700 series
From the FAA registry file of October 24, 2026. The registry lists only the engine series, so ADs for every Rolls-Royce BR-700 model are included below.
On this page
Airworthiness directives that may apply · 84
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 | 3 |
| 2003 | 1 |
| 2005 | 2 |
| 2006 | 2 |
| 2008 | 1 |
| 2009 | 4 |
| 2010 | 1 |
| 2011 | 4 |
| 2012 | 3 |
| 2013 | 4 |
| 2014 | 5 |
| 2015 | 1 |
| 2016 | 6 |
| 2017 | 4 |
| 2018 | 5 |
| 2019 | 3 |
| 2020 | 5 |
| 2021 | 6 |
| 2022 | 4 |
| 2023 | 11 |
| 2024 | 4 |
| 2025 | 7 |
| 2026 | 7 |
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 N116QSMatched 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 N116QSMatched 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
Service difficulty reports · 9
Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.
SDR DXTA2026101510145Aileron Sys · jammedAILERON JAMMED IN CRUISE FLIGHT. BOTH SIDES AFFECTED. WAS ABLE TO SLOWLY TURN THE AIRCRAFT. POURING RAIN FOR HOURS BEFORE OUR DEPARTURE. PICTURES ARE OF WATER DRAINING FROM AILERON AT DESTINATION.SDR DXTA2026022006937Microwave Oven · faultedIN FLIGHT OUR FA ATTEMPTED TO USE THE MICROWAVE TO WARM PASSENGER FOOD. WITHIN 5 SECONDS OF USE, THE MICROWAVE BEGAN TO ARC INSIDE ON THE TOP, MADE A HIGH PITCH SQUEELING SOUND, AND GAVE OFF AN ACRID SMELL. WE STOPPED THE PROCESS AND ISOLATED THE CIRCUIT VIA TSDR DXTA2025122906287Seat · faultedDURING CRUISE, AN ELECTRICAL/PLASTIC INSULATION BURNING ODOR IN CABIN, AND A VERY LIGHT HAZE OF SMOKE NOTICEABLE AGAINST INCOMING SUNLIGHT, CREW WAS ABLE TO LOCATE THE SOURCE AREA, LOWER SIDEWALL ADJACENT TO SEAT NR 4, LOCATION THAT ALSO PRESENTS AN AREA OF DSDR DXTA2025111705694Battery Pack · intermittentCABIN EMERGENCY LIGHTS ARE TURNING OFF AND ON UNCOMMANDED WHEN EMERGENCY LIGHT SWITCH IS IN ON POSITION. CABIN EMERGENCY LIGHTS ARE TURNING OFF AND ON UNCOMMANDED WHEN EMER LIGHT SWITCH IS IN ON POSITION: REMOVED #4 EMERGENCY LIGHT POWER SUPPLY P/N 8ES40980SDR DXTA2025021202310Actuator · failedMAIN DOOR: THE MAIN CABIN DOOR CAN NOT BE CLOSED BY THE NORMAL PROCESS WITH THE MOTOR AND CABLES. WHEN THE MOTOR SWITCH ON THE EXTERIOR OF THE PLANE OR THE BUTTON IS ACTIVATED IN THE INTERIOR OF THE PLANE THE MOTOR RUNS BUT THE DOOR WILL NOT RAISE. CORRECTIVE SDR DXTA2023101698060Unknown · unknownUPON LANDING THE AC BEGUN TO PULL LEFT AND THEN THE CAS CAUTION ILLUMINATED. NOSE WHEEL STEERING WAS LOST. COMPLIED WITH APPROPRIATE CHECKLIST WITHOUT RESOLUTION. PERFORMED THE OPERATIONAL CHECK OF THE NOSE WHEEL STEERING (NWS) SYSTEM WITH TORQUE LINKS DISCONSDR DXTA2023092596230Actuator · defectiveMAIN DOOR: THE MAIN CABIN DOOR WILL NOT CLOSE WITH THE INTERIOR OR EXTERIOR PUSH BUTTONS. //SIGNOFF// REMOVED FAULTY ACTUATOR PN:GS321-0591-9, SN: 60776 AND INSTALLED REPAIRED UNIT, SAME PART NUMBER WITH SN MENTIONED ABOVE. WORK DONE IAW GLOBAL 5000 MM 52-11-2SDR DXTA2023011778720Pressure Switch · failedAFTER TAKE OFF THE LEFT MAIN LANDING GEAR STAYED DOWN WHILE THE NLG AND RT MLG RETRACTED. RECEIVED A AMBER GEAR DISAGREE MESSAGE. COULD HEAR LTMG WHEEL STILL SPINNING. SEEMED LIKE THE WHEEL STOPPED SPINNING, THE LT MLG RETRACTED. IT TOOK APPROXIMATELY 25-30 SSDR DXTA2022121676280Ecu · faultedAFTER TAKEOFF LT MLG AND MLG DOOR FAILED RETRACTION, AMBER INDICATION ON MLG DISPLAY. VIBRATION & NOISE UNTIL GEAR RETRACTED APPROX 25 SECS. INSPECTED AND FOUND LGECU A FAULT 1. MLG WOW TO SPC & LGECU B FAULT 1. WOW TO SFOJ 2. BOTH FAUL TS ARE ACTIVE IN THE F
Reports on N116QS not matched to an aircraft · 10
They name N116QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.
SDR DXTA2013061805419Brake Assy · misinstalledBRAKES MAKE LOUD SQEAULING NOISE WHEN APPLIED WHILE TURNING AND OCCAISIONALLY WHEN STOPPING STRAIGHT AHEAD. TROUBLESHOT BRAKE SYS AND FOUND THAT THE RT BRAKE ASSY SHUTTLE VALVE IS BAD AND IS ALLOWING HYDRAULIC FLUID TO GO THROUGH TO THE EMERGENCY AIR LINE, THSDR DXTA2012112905197Control Unit · malfunctionedAFTER LANDING, THE BRAKES APPEARED TO WORK NORMALLY. PILOT APPLIED THE BRAKES BUT THE PEDALS WERE STIFF. IT FELT LIKE THE ANTI-SKID CHECK DURING TAXI OUT. A SECOND ATTEMPT WAS MADE AND THE BRAKES WERE STILL STIFF AND THE AIRPLANE WAS NOT SLOWING DOWN. COPSDR DXTA2012112105188Control Valve · failedAFTER LANDING, BRAKES APPLIED AND WORKED FINE. ACFT WAS TAXIING TO PARKING, PILOT APPLIED BRAKES AND NO RESULT. PEDALS WERE STIFF. SECOND ATTEMPT PROVIDED SAME RESULT. BRAKE PEDALS RELEASED AND BRAKES RETURNED TO NORMAL. R & R POWER BRAKE CONTROL VALVE IA
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