# N116QS: 2016 Bombardier BD-700-1A11

- Status: Valid registration
- Airframe: [Bombardier BD-700-1A11](https://openairdocs.org/model/bombardier-bd-700-1a11) (registry code 1390022, 8 seats)
- Engine: [Rolls-Royce BR-700 series](https://openairdocs.org/engine/rolls-royce-br-700-series) (registry code 54565)
- Data sheets: [TCDS T00003NY](https://openairdocs.org/tcds/T00003NY) (Bombardier Inc.) (OpenAirDocs)
- Serial number: 9768
- Year built: 2016
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: March 30, 2017
- Certificate issued: June 12, 2026
- Expires: June 30, 2033
- Mode S code: A043EC
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=116QS
- Page: https://openairdocs.org/aircraft/N116QS

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination. The registry lists only the engine series, so ADs for every Rolls-Royce BR-700 model are included.

## ADs that may apply (OpenAirDocs): 84 in force

### Matched by airframe (Bombardier BD-700-1A11)

- [AD 2026-15-09](https://openairdocs.org/ad/2026-15-09): Landing Gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 3, 2026
- [AD 2026-11-07](https://openairdocs.org/ad/2026-11-07): Equipment/furnishings · Bombardier BD-700-1A10, BD-700-1A11 and BD-700-2A12. Effective Jul 20, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2026-09-18](https://openairdocs.org/ad/2026-09-18): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 26, 2026
- [AD 2026-08-04](https://openairdocs.org/ad/2026-08-04): Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 29, 2026
- [AD 2025-14-51](https://openairdocs.org/ad/2025-14-51): Indicating/Recording System · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 4, 2026
- [AD 2025-12-01](https://openairdocs.org/ad/2025-12-01): Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 17, 2025
- [AD 2025-07-11](https://openairdocs.org/ad/2025-07-11): Hydraulic Power · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 2, 2025
- [AD 2025-09-04](https://openairdocs.org/ad/2025-09-04): Time Limits/Maintenance Checks · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 6, 2025
- [AD 2024-26-09](https://openairdocs.org/ad/2024-26-09): Time Limits/Maintenance Checks; Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 11, 2025
- [AD 2024-23-02](https://openairdocs.org/ad/2024-23-02): Landing Gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 15, 2025
- [AD 2024-23-08](https://openairdocs.org/ad/2024-23-08): Wings · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 6, 2025
- [AD 2024-07-09](https://openairdocs.org/ad/2024-07-09): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 17, 2024
- [AD 2024-03-08](https://openairdocs.org/ad/2024-03-08): Pneumatic · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 3, 2024
- [AD 2024-02-05](https://openairdocs.org/ad/2024-02-05): Wings · Bombardier BD-700-1A10 and BD-700-1A11. Effective Apr 9, 2024
- [AD 2023-24-08](https://openairdocs.org/ad/2023-24-08): Landing gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Feb 6, 2024
- [AD 2023-12-02](https://openairdocs.org/ad/2023-12-02): Time Limits/Maintenance Checks · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 7, 2023
- [AD 2023-13-15](https://openairdocs.org/ad/2023-13-15): Navigation · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 27, 2023
- [AD 2023-08-01](https://openairdocs.org/ad/2023-08-01): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 20, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2023-05-11](https://openairdocs.org/ad/2023-05-11): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 12, 2023
- [AD 2022-24-01](https://openairdocs.org/ad/2022-24-01): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 9, 2023
- [AD 2022-25-13](https://openairdocs.org/ad/2022-25-13): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 13, 2023
- [AD 2022-14-07](https://openairdocs.org/ad/2022-14-07): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 19, 2022
- [AD 2022-13-05](https://openairdocs.org/ad/2022-13-05): Navigation · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 11, 2022
- [AD 2022-11-17](https://openairdocs.org/ad/2022-11-17): Time Limits/Maintenance Checks · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 22, 2022
- [AD 2022-12-01](https://openairdocs.org/ad/2022-12-01): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 19, 2022
- [AD 2021-21-04](https://openairdocs.org/ad/2021-21-04): Powerplant · Bombardier BD-700-1A10 and BD-700-1A11. Effective Dec 8, 2021
- [AD 2021-08-11](https://openairdocs.org/ad/2021-08-11): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Apr 27, 2021
- [AD 2020-12-14](https://openairdocs.org/ad/2020-12-14): Electrical power · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 8, 2020
- [AD 2020-12-15](https://openairdocs.org/ad/2020-12-15): Pneumatic · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 24, 2020
- [AD 2020-05-27](https://openairdocs.org/ad/2020-05-27): Fuselage · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 7, 2020
- [AD 2020-03-21](https://openairdocs.org/ad/2020-03-21): Landing gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 12, 2020
- [AD 2020-02-15](https://openairdocs.org/ad/2020-02-15): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 12, 2020
- [AD 2019-12-02](https://openairdocs.org/ad/2019-12-02): Electrical Power · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 12, 2019
- [AD 2019-03-22](https://openairdocs.org/ad/2019-03-22): Landing gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Apr 15, 2019
- [AD 2018-25-07](https://openairdocs.org/ad/2018-25-07): Fuselage · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 15, 2019
- [AD 2018-22-08](https://openairdocs.org/ad/2018-22-08): Fire protection · Bombardier BD-700-1A10 and BD-700-1A11. Effective Dec 10, 2018
- [AD 2018-20-20](https://openairdocs.org/ad/2018-20-20): Flilght Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Nov 20, 2018
- [AD 2018-21-03](https://openairdocs.org/ad/2018-21-03): Fuselage · Bombardier BD-700-1A10 and BD-700-1A11. Effective Nov 19, 2018
- [AD 2018-09-15](https://openairdocs.org/ad/2018-09-15): Engine · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 15, 2018
- [AD 2017-22-14](https://openairdocs.org/ad/2017-22-14): Navigation · Bombardier BD-100-1A10 (Challenger 300), BD-500-1A10, BD-500-1A11 and 13 more. Effective Dec 20, 2017
- [AD 2017-19-11](https://openairdocs.org/ad/2017-19-11): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Oct 23, 2017
- [AD 2017-14-15](https://openairdocs.org/ad/2017-14-15): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 31, 2017
- [AD 2016-17-16](https://openairdocs.org/ad/2016-17-16): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Oct 5, 2016
- [AD 2016-15-06](https://openairdocs.org/ad/2016-15-06): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 8, 2016
- [AD 2016-15-03](https://openairdocs.org/ad/2016-15-03): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 31, 2016
- [AD 2016-10-06](https://openairdocs.org/ad/2016-10-06): Navigation · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 23, 2016
- [AD 2016-01-12](https://openairdocs.org/ad/2016-01-12): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Feb 25, 2016
- [AD 2015-17-05](https://openairdocs.org/ad/2015-17-05): Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 29, 2015

### Matched by engine (Rolls-Royce BR-700 series)

- [AD 2026-21-04](https://openairdocs.org/ad/2026-21-04): Engine (Turbine/Turboprop) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Nov 23, 2026
- [AD 2025-06-03](https://openairdocs.org/ad/2025-06-03): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 23, 2025
- [AD 2023-17-11](https://openairdocs.org/ad/2023-17-11): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Sep 20, 2023
- [AD 2022-26-02](https://openairdocs.org/ad/2022-26-02): Accessory Gearboxes · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20, BR700-710C4-11 and 1 more. Effective Jan 27, 2023
- [AD 2021-21-12](https://openairdocs.org/ad/2021-21-12): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A2-20. Effective Dec 13, 2021
- [AD 2021-14-03](https://openairdocs.org/ad/2021-14-03): Turbine Section · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 19, 2021
- [AD 2021-12-07](https://openairdocs.org/ad/2021-12-07): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 12, 2021
- [AD 2018-18-14](https://openairdocs.org/ad/2018-18-14): Engine Controls · Rolls-Royce Deutschland BR700-710A2-20 and BR700-710C4-11. Effective Oct 12, 2018
- [AD 2016-13-12](https://openairdocs.org/ad/2016-13-12): Pawl carrier pivot pins · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Aug 5, 2016
- [AD 2014-12-03](https://openairdocs.org/ad/2014-12-03): Fuel metering units (FMUs) · Rolls-Royce Deutschland BR700-725A1-12. Effective Jul 17, 2014
- [AD 2014-08-05](https://openairdocs.org/ad/2014-08-05): Low-pressure compressor (LPC) case ice impact panels · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 23, 2014
- [AD 2014-07-02](https://openairdocs.org/ad/2014-07-02): High-pressure (HP) compressor stages 1 to 6 rotor disc assemblies · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective May 8, 2014
- [AD 2013-12-03](https://openairdocs.org/ad/2013-12-03): Fuel pump tube · Rolls-Royce Deutschland BR700-725A1-12. Effective Jun 14, 2013
- [AD 2013-03-17](https://openairdocs.org/ad/2013-03-17): High-pressure turbine (HPT) stage 1 and stage 2 discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Mar 21, 2013
- [AD 2012-14-01](https://openairdocs.org/ad/2012-14-01): LP compressor booster rotor · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Oct 19, 2012
- [AD 2009-07-01 R1](https://openairdocs.org/ad/2009-07-01-R1): High-pressure (HP) turbine stage 1 discs, and HP turbine stage 2 discs · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 6, 2012
- [AD 2011-22-01](https://openairdocs.org/ad/2011-22-01): Touch-and-go and overshoot on life cycle counting · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Nov 23, 2011
- [AD 2010-25-05](https://openairdocs.org/ad/2010-25-05): Turbine Discs · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 13, 2011
- [AD 2009-21-04](https://openairdocs.org/ad/2009-21-04): Engine Failure · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Dec 3, 2009
- [AD 2009-04-13](https://openairdocs.org/ad/2009-04-13): Low pressure (LP) compressor (fan) · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Mar 26, 2009
- [AD 2005-21-05](https://openairdocs.org/ad/2005-21-05): Fan discs and fan blades · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Nov 25, 2005
- [AD 2005-16-12](https://openairdocs.org/ad/2005-16-12): Independent Overspeed Protection (IOP) unit. · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Aug 26, 2005
- [AD 2000-25-51](https://openairdocs.org/ad/2000-25-51): High Pressure Turbine Disks · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Feb 20, 2001
- [AD 2001-01-01](https://openairdocs.org/ad/2001-01-01): Oil Filter · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Jan 31, 2001
- [AD 98-24-03 R1](https://openairdocs.org/ad/98-24-03-R1): Combustion Core Fairings · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Dec 27, 1999

### Historical (superseded or no longer in force)

- [AD 2023-03-06](https://openairdocs.org/ad/2023-03-06) (historical): Navigation · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 13, 2023
- [AD 2021-10-02](https://openairdocs.org/ad/2021-10-02) (historical): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 29, 2021
- [AD 2016-25-18](https://openairdocs.org/ad/2016-25-18) (historical): Engine · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 3, 2017
- [AD 2008-24-12](https://openairdocs.org/ad/2008-24-12) (historical): Bolt which connects the PCU (power control unit) to the elevator surface · Bombardier BD-700-1A10 and BD-700-1A11. Effective Dec 15, 2008
- [AD 2022-24-06](https://openairdocs.org/ad/2022-24-06) (historical): Turbine Engine Compressor Section · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Jan 6, 2023
- [AD 2013-05-13](https://openairdocs.org/ad/2013-05-13) (historical): Fuel pump splined couplings · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20 and BR700-710C4-11. Effective Apr 24, 2013
- [AD 2012-26-14](https://openairdocs.org/ad/2012-26-14) (historical): High-pressure (HP) compressor stages 1 to 6 rotor disc assembly · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Jan 10, 2013
- [AD 2009-07-01](https://openairdocs.org/ad/2009-07-01) (historical): High Pressure (HP) Turbine · Rolls-Royce Deutschland BR700-715A1-30, BR700-715B1-30 and BR700-715C1-30. Effective Apr 27, 2009
- [AD 2003-07-11](https://openairdocs.org/ad/2003-07-11) (historical): Fan discs · Rolls-Royce Deutschland BR700-710A1-10 and BR700-710A2-20. Effective Apr 28, 2003
- [AD 2001-05-06](https://openairdocs.org/ad/2001-05-06) (historical): Fan Disk · BMW Rolls-Royce BR700-710A1-10 and BR700-710A2-20. Effective Mar 29, 2001

All 94: https://openairdocs.org/aircraft/N116QS/ads.md

## Information bulletins (advisory) (3 in force)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB NM-15-02](https://openairdocs.org/saib/NM-15-02): Cabin Equipment/Furnishings. Issued Nov 6, 2014
- [SAIB NM-11-34](https://openairdocs.org/saib/NM-11-34): Doors: Passenger/Crew Doors, Tensator Springs of the Door Actuator. Issued May 17, 2011
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021

## NTSB investigations

None matched to N116QS.

## FAA accident and incident reports

None matched to N116QS.

## Service difficulty reports (9)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DXTA2026101510145](https://openairdocs.org/sdr/DXTA2026101510145), Oct 11, 2026: AILERON SYS. JAMMED. AILERON 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 D
- [SDR DXTA2026022006937](https://openairdocs.org/sdr/DXTA2026022006937), Feb 17, 2026: MICROWAVE OVEN. FAULTED. IN 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
- [SDR DXTA2025122906287](https://openairdocs.org/sdr/DXTA2025122906287), Dec 24, 2025: SEAT. FAULTED. DURING CRUISE, AN ELECTRICAL/PLASTIC INSULATION BURNING ODOR IN CABIN, AND A VERY LIGHT HAZE OF SMOKE NOTICEABLE AGAINST INCOMING SUNLIGHT, CREW WAS ABLE TO LOC
- [SDR DXTA2025111705694](https://openairdocs.org/sdr/DXTA2025111705694), Nov 14, 2025: BATTERY PACK. INTERMITTENT. CABIN EMERGENCY LIGHTS ARE TURNING OFF AND ON UNCOMMANDED WHEN EMERGENCY LIGHT SWITCH IS IN ON POSITION. CABIN EMERGENCY LIGHTS ARE TURNING OFF AND ON UNCOMMAND
- [SDR DXTA2025021202310](https://openairdocs.org/sdr/DXTA2025021202310), Feb 9, 2025: ACTUATOR. FAILED. MAIN 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 BUTT
- [SDR DXTA2023101698060](https://openairdocs.org/sdr/DXTA2023101698060), Oct 15, 2023: UNKNOWN. UNKNOWN. UPON LANDING THE AC BEGUN TO PULL LEFT AND THEN THE CAS CAUTION ILLUMINATED. NOSE WHEEL STEERING WAS LOST. COMPLIED WITH APPROPRIATE CHECKLIST WITHOUT RESOLUTIO
- [SDR DXTA2023092596230](https://openairdocs.org/sdr/DXTA2023092596230), Sep 23, 2023: ACTUATOR. DEFECTIVE. MAIN 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 INS
- [SDR DXTA2023011778720](https://openairdocs.org/sdr/DXTA2023011778720), Jan 16, 2023: PRESSURE SWITCH. FAILED. AFTER 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 SP
- [SDR DXTA2022121676280](https://openairdocs.org/sdr/DXTA2022121676280), Dec 15, 2022: ECU. FAULTED. AFTER TAKEOFF LT MLG AND MLG DOOR FAILED RETRACTION, AMBER INDICATION ON MLG DISPLAY. VIBRATION & NOISE UNTIL GEAR RETRACTED APPROX 25 SECS. INSPECTED AND FOUND

## Service difficulty 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 DXTA2013061805419](https://openairdocs.org/sdr/DXTA2013061805419), Jun 17, 2013: BRAKE ASSY. MISINSTALLED. BRAKES MAKE LOUD SQEAULING NOISE WHEN APPLIED WHILE TURNING AND OCCAISIONALLY WHEN STOPPING STRAIGHT AHEAD. TROUBLESHOT BRAKE SYS AND FOUND THAT THE RT BRAKE AS
- [SDR DXTA2012112905197](https://openairdocs.org/sdr/DXTA2012112905197), Nov 28, 2012: CONTROL UNIT. MALFUNCTIONED. AFTER 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 SEC
- [SDR DXTA2012112105188](https://openairdocs.org/sdr/DXTA2012112105188), Nov 20, 2012: CONTROL VALVE. FAILED. AFTER LANDING, BRAKES APPLIED AND WORKED FINE. ACFT WAS TAXIING TO PARKING, PILOT APPLIED BRAKES AND NO RESULT. PEDALS WERE STIFF. SECOND ATTEMPT PROVIDED SAME 
- [SDR DXTA2012111605183](https://openairdocs.org/sdr/DXTA2012111605183), Nov 15, 2012: BRAKE SYS. CONTAMINATED. PEDALS WERE STIFF WITH NO RESISTANCE AND PLANE WAS NOT SLOWING. UPON EMERGENCY BRAKE APPLICATION, THE BRAKE PEDALS REENGAGED. FOUND AIR IN BRAKE SYSTEM. PERFORM
- [SDR DXTA2010111704311](https://openairdocs.org/sdr/DXTA2010111704311), Nov 17, 2010: BULB. INOPERATIVE. LEFT MAIN GEAR INDICATOR LIGHT IS INOPERATIVE. R & R LT GEAR INDICATION LAMP IAW MM 33-10-00. OPS CHECK GOOD.
- [SDR DXTA2009081703762](https://openairdocs.org/sdr/DXTA2009081703762), Aug 14, 2009: CONTROL CABLE. LOOSE. CONTROL YOKE SLOPPY IN FIRST 2-3 INCHES OF TRAVEL, MORE PRONOUNCED IN LT TURNS. AT LOW SPEED (200 KIAS WITH FLAPS UP) THE FIRST 3 " OF TRAVEL HAS NO EFFECT. WIT
- [SDR DXTA200808073219](https://openairdocs.org/sdr/DXTA200808073219), Aug 7, 2008: WARNING SYSTEM. MALFUNCTIONED. AFTER SELECTING GEAR UP, GEAR RET NORMALLY BUT RED GEAR UNSAFE LT. REMAINED ILLUMINATED + DID NOT EXTINGUISH. GEAR EXTENSION WAS ALSO NORMAL AND RED UNSAFE LT E
- [SDR DXTA200601495](https://openairdocs.org/sdr/DXTA200601495), Jul 12, 2006: PROXIMITY SWITCH. MALFUNCTIONED. GREEN RIGHT MAIN GEAR LANDING LT DID NOT ILLUMINATE. LIGHT BULB WAS OPERATIVE. RAN CHECKLIST AND MADE NORMAL LANDING. REPLACED RT MLG DOWNLOCK SWITCH WITH NEW. 
- [SDR DXTA200500908](https://openairdocs.org/sdr/DXTA200500908), Aug 19, 2005: PCB. DEFECTIVE. AFTER T/O RED LIGHT IN HANDLE ILLUMINATED. CYCLED GEAR, GOT 3 GR AND 1 RD. RAN ALT GEAR EXT PROCEDURE. JACKED THE AIRCRAFT, SWUNG THE GEAR FOUND THAT THE MAIN G
- [SDR DXTA200500768](https://openairdocs.org/sdr/DXTA200500768), Jun 12, 2005: WARNING LIGHT. INTERMITTENT. DURING T/O ROLL & TAXI BACK TO FBO THE RIGHT WINDSHIELD OVERHEAT & MASTER WARNING LIGHTS ILLUMINATED ON & OFF INTERMITTENTLY. ITEM IS UNDER INVESTIGATION.

## STCs that may be installed (OpenAirDocs) (141, first 50)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Bombardier BD-700-1A11)

- [STC ST04612CH](https://openairdocs.org/stc/ST04612CH): Installation of a SpaceX Starlink Aviation System. Nextant Aerospace
- [STC ST12507IB](https://openairdocs.org/stc/ST12507IB): Iridium Antenna relocation. Q.C.M. DESIGN GmbH
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST12362IB](https://openairdocs.org/stc/ST12362IB): Ferry Kit Lift Raft installation equipment must be installed in accordance with Transport Canada Civil Aviation (TCCA) approved Bombardier Inc. Modification Data Summary RAZ-BM700-323 Rev--, dated July 16, 2024, or later TCCA approved revision. Bombardier Inc
- [STC ST03199NY](https://openairdocs.org/stc/ST03199NY): Installation of ABC Completions Electronic Flight Bag Display Mounts and DAC International GDC-64. Delta Engineering Corporation
- [STC ST12270IB](https://openairdocs.org/stc/ST12270IB): Installation of Gogo Galileo Satcom System. Q.C.M. DESIGN GmbH
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST04754NY](https://openairdocs.org/stc/ST04754NY): Installation of LAI Windshields. Lee Aerospace Inc
- [STC ST12078IB](https://openairdocs.org/stc/ST12078IB): Installation of wiring provisions for a subsequent interior completion. Bombardier Inc
- [STC ST12029CH](https://openairdocs.org/stc/ST12029CH): Installation of Gogo MB13 antennas. Premier Air Center, LLC d/b/a West Star Aviation
- [STC ST02472AT](https://openairdocs.org/stc/ST02472AT): Installation of a mini Quick Access Recorder (QAR) model MKI, MKII, or MKIII. Aircraft Systems and Manufacturing Inc
- [STC ST04677NY](https://openairdocs.org/stc/ST04677NY): Installation of Demonstration of Transmitting Personal Electronic Device (TPED) Tolerance. Bombardier Inc
- [STC ST09931AC](https://openairdocs.org/stc/ST09931AC): Installation of an Aspire 400 Satcom System. L2 Aviation
- [STC ST03759NY](https://openairdocs.org/stc/ST03759NY): Installation of INGENIO Cockpit Tripod Electronic Flight Bag (EFB) Mount. INGENIO Aerospace Inc
- [STC ST04591NY](https://openairdocs.org/stc/ST04591NY): Structural integration and installation of Iridium Satcom Antenna. ALAMO Engineering GmbH
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST04561CH](https://openairdocs.org/stc/ST04561CH): Installation of a Latitude Technologies Corporation DL-150 Satellite Data Unit (SDU) and Iridium Antenna. West Star Aviation
- [STC ST00215IB](https://openairdocs.org/stc/ST00215IB): Installation of saf-Tglo ECO Photoluminescent Aisle Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST04159CH](https://openairdocs.org/stc/ST04159CH): Upgrade of Honeywell Primus II Communications Units RCZ-8XX Transponders to support Certification of Automatic Dependent Surveillance -Broadcast (ADS-B) Out. CMD Flight Solutions LLC
- [STC ST01057WI](https://openairdocs.org/stc/ST01057WI): Installation of a Vision Safe Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST00190IB](https://openairdocs.org/stc/ST00190IB): Installation of a Satcom Iridium Datalink Unit with FANS 1/A+ capability and removal of the installed Inmarsat Swift 64 satcom system. ALAMO ENGINEERING GmbH
- [STC ST04268NY](https://openairdocs.org/stc/ST04268NY): Replacement of Honeywell DU-870 display units with DU-875 Elite display units with basic functions. ALAMO ENGINEERING GmbH
- [STC ST00167IB](https://openairdocs.org/stc/ST00167IB): Installation of Ku-Band Satcom with TMA. ALAMO ENGINEERING GmbH
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST00126IB](https://openairdocs.org/stc/ST00126IB): Replacement of Halon agent with alternate Halon-free Portable Fire Extinguisher agent. AMAC Aerospace Switzerland AG
- [STC ST02302CH](https://openairdocs.org/stc/ST02302CH): Install ERDA model 7004 HI-LO table with slide top. Collins Aerospace
- [STC ST01970WI](https://openairdocs.org/stc/ST01970WI): Installation of an Aircraft Health Management System (AHMS). Learjet Inc
- [STC ST02012WI](https://openairdocs.org/stc/ST02012WI): Upgrade of Gogo Business Aviation AVANCE L5 to AVANCE L5/X3 System with MB13 Antennas. Duncan Aviation Inc
- [STC ST04396CH](https://openairdocs.org/stc/ST04396CH): Installation of SATCOM system and associated KuKa Radome. Envoy Aerospace LLC
- [STC ST04562NY](https://openairdocs.org/stc/ST04562NY): Installation of saf-Tglo® SuperSeal UltraLite-X (SSUL-X) Photoluminescent Floor Proximity Emergency Escape Path Marking Systems. STG AEROSPACE GERMANY GmbH
- [STC ST00105IB](https://openairdocs.org/stc/ST00105IB): Introduction of Activation of Wireless Charging Systems for Portable Electronic Devices. AMAC AEROSPACE SWITZERLAND AG
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST00064IB](https://openairdocs.org/stc/ST00064IB): Installation of the KU Band Satcom System. Sky Service F.B.O. Inc
- [STC ST00051IB](https://openairdocs.org/stc/ST00051IB): Installation of the Interior Refurbishment. Skyservice Business Aviation Inc
- [STC ST02293SE](https://openairdocs.org/stc/ST02293SE): Installation of a Crane Aerospace & Electronics Tire Sensor Assembly. ELDEC Aerospace Corp
- [STC ST02140NY](https://openairdocs.org/stc/ST02140NY): Complete Custom Aircraft Interior Installation. Bombardier Completion Center Inc
- [STC ST04678NY](https://openairdocs.org/stc/ST04678NY): Installation of Provisions for Custom Furnishing in the Cockpit and Tow Bar and Toolbox Installation in the Aft Equipment Bay. Bombardier Inc
- [STC ST04673NY](https://openairdocs.org/stc/ST04673NY): Installation of Rockwell Collins Venue Retrofit. Q.C.M. DESIGN GmbH
- [STC ST00818DE](https://openairdocs.org/stc/ST00818DE): Installation of Honeywell Control Display Unit (CDU) model CD-830. Premier Air Center LLC d/b/a West Star Aviation
- [STC ST02167NY](https://openairdocs.org/stc/ST02167NY): Installation of Insulation Blankets for BD-700-1A11, BD-700-1A10 aircraft models. MTI-Polyfab Inc
- [STC ST02280NY](https://openairdocs.org/stc/ST02280NY): The installation of structural provisions for the D & M Part Number 444-DMC57-1 Securaplane Antenna. Bombardier Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST03228NY](https://openairdocs.org/stc/ST03228NY): Installation of aircraft completion. B/E Aerospace Limited
- [STC ST03088NY](https://openairdocs.org/stc/ST03088NY): Installation of Aircraft Completion Modifications. Bombardier Inc
- [STC ST03267NY](https://openairdocs.org/stc/ST03267NY): Aircraft completion modifications. Innotech Aviation a Division of IMP Group Limited
- [STC ST03595NY](https://openairdocs.org/stc/ST03595NY): Installation of Honeywell Laseref IV Upgrade. Dassault Aircraft Services (DAS)
- [STC ST04538NY](https://openairdocs.org/stc/ST04538NY): Installation of Ku Band Satellite System with a Gimbal Antenna and WiFi Hotspots. Q.C.M. DESIGN GmbH
- [STC ST00299BO](https://openairdocs.org/stc/ST00299BO): Installation of a Honeywell DU-875 or DU-875AF Liquid Crystal Display (LCD) based Display System including two Cursor Control Devices (CCDs). Learjet Inc
- [STC ST01949WI](https://openairdocs.org/stc/ST01949WI): Installation of Aviation Clean Air Bi-Polar Ionization System. Duncan Aviation Inc

All 141: https://openairdocs.org/aircraft/N116QS/stcs.md

## Related

- Other Bombardier BD-700-1A11 aircraft: https://openairdocs.org/model/bombardier-bd-700-1a11/aircraft.md
- The Rolls-Royce BR-700 series engine: https://openairdocs.org/engine/rolls-royce-br-700-series.md

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