# N114QS: 2015 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 Deutschland BR700-710A220](https://openairdocs.org/engine/rolls-royce-deutschland-br700-710a220) (registry code 54004) - Data sheets: [TCDS T00003NY](https://openairdocs.org/tcds/T00003NY) (Bombardier Inc.), [TCDS E00057EN](https://openairdocs.org/tcds/E00057EN) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs) - Serial number: 9732 - Year built: 2015 - Type: Fixed wing multi engine - Engine type: Turbo-fan - Airworthiness: Standard, transport - Airworthiness date: June 14, 2016 - Certificate issued: October 11, 2025 - Expires: October 31, 2032 - Mode S code: A03C7E - Owner type: Co-owned, fractional ownership - FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=114QS - Page: https://openairdocs.org/aircraft/N114QS 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. ## ADs that may apply (OpenAirDocs): 71 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 Deutschland BR700-710A220) - [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 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 2021-12-07](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 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 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 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 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 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 79: https://openairdocs.org/aircraft/N114QS/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 N114QS. ## FAA accident and incident reports None matched to N114QS. ## 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. - [Incident 20110728014369I](https://openairdocs.org/incident/20110728014369I), Jul 28, 2011: Raytheon Aircraft Company 400A (N114QS), Miami, FL, No damage. During climb out of 16000 feet, a large amp split was notice. The left amp gauge read 25 amps and the right gauge read 225 amps. Also, noted at the time, the… ## Service difficulty reports (2) 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 DXTA2025092905092](https://openairdocs.org/sdr/DXTA2025092905092), Sep 25, 2025: CONTACTOR. FAULTED. DURING 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 F - [SDR DXTA2021112252340](https://openairdocs.org/sdr/DXTA2021112252340), Nov 22, 2021: AUTOBRAKE SYS. FAULTED. AUTOBRAKE 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 IN ## Service difficulty 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 DXTA2012061104995](https://openairdocs.org/sdr/DXTA2012061104995), Jun 9, 2012: LANDING GEAR. UNKNOWN. LANDING 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 L - [SDR DXTA2011061704618](https://openairdocs.org/sdr/DXTA2011061704618), Jun 16, 2011: CONTROL CABLE. OUT OF RIG. INITIATED 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 - [SDR DXTA2011040104536](https://openairdocs.org/sdr/DXTA2011040104536), Apr 1, 2011: CONTROL VALVE. INOPERATIVE. ON 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. - [SDR DXTA2011040404536](https://openairdocs.org/sdr/DXTA2011040404536), Apr 1, 2011: BRAKE SYS. MALFUNCTIONED. ON LANDING ROLLOUT, BRAKES ARE HARD AND NON-RESPONSIVE ON INITAL APPLICATION. BRAKES ARE THEN SOFT AND GRAB AS IF ANTI SKID HAS FAILED. - [SDR DXTA2011030704492](https://openairdocs.org/sdr/DXTA2011030704492), Mar 6, 2011: BRAKE ASSY. MALFUNCTIONED. BRAKES DURING TAXI AND ROLLOUT ARE HARD AND NON- RESPOSIVE ON INITIAL APPLICATION ONCE PRESSURE IS PRESSED HARD THEN BRAKES GRAB AS IF ANTI SKID IS OFF LEFT BRA - [SDR E81RJW304203](https://openairdocs.org/sdr/E81RJW304203), Feb 11, 2011: PCB. INTERMITTENT. INVESTIGATED FLIGHT CREW REPORT OF ROLL TRIM NOT RESPONDING TO SELECTED INPUTS AFTER 10 DEGRESS FLAPS SELECTED ON APPROACH. ROLL TRIM OPERATING NORMAL AFTER LAN - [SDR E81RJW304162](https://openairdocs.org/sdr/E81RJW304162), Feb 7, 2011: TRANSMITTER. OUT OF ADJUST. FLIGHT CREW REPORTED FLAP ASSYMETRY ANNUNCIATOR LIGHT INDICATION AND SLIGHT RT ROLL ON APPROACH, WHEN FLAPS EXTENDED TO 20 DEGREE POSITION. FOUND LT FLAP FOLLOW - [SDR DXTA2011010304394](https://openairdocs.org/sdr/DXTA2011010304394), Dec 31, 2010: INDICATOR. INOPERATIVE. LANDING GEAR, DOWN LIGHTS DID NOT ILLUMINATE WHEN GEAR WAS SELECTED DOWN OR WHEN LIGHTS WERE TESTED VIA ROTARY TEST. THE GEAR WAS NOT BLOWN DOWN. INSTALLED & SA - [SDR DXTA2010090704220](https://openairdocs.org/sdr/DXTA2010090704220), Sep 5, 2010: BRAKE. WEAK. ON LANDING AND TAXI IN, BRAKES ON LT AND RT SIDES APPLY WHAT FEELS LIKE MINIMAL BRAKING ON INITIAL APPLICATION. UPON INCREASE IN TOE PEDAL PRESSURE, BRAKES WILL - [SDR DXTA2010083004215](https://openairdocs.org/sdr/DXTA2010083004215), Aug 26, 2010: BRAKE SYS. MALFUNCTIONED. AFTER GEAR RETRACTION THE RED GEAR UNSAFE LIGHT REMAINED ON AS WELL AS THE HYD PRESS CAUTION LIGHT. AFTER LOWERING THE GEAR ALL THREE GREEN LIGHTS ILLUMINATED A - [SDR DXTA2010060404114](https://openairdocs.org/sdr/DXTA2010060404114), May 25, 2010: BULB. INOPERATIVE. RT GREEN GEAR DOWN LIGHT INOP. R & R BULBS AS NEEDED, REF MM 33-11-00-201. OPS CHECK NORMAL. - [SDR DXTA2010032404051](https://openairdocs.org/sdr/DXTA2010032404051), Mar 23, 2010: BRAKE. MALFUNCTIONED. CO PILOTS LT BRAKE PEDAL OPERATES AND FEELS NORMAL, RT BRAKE PEDAL TRAVELS APPROX HALF THE DISTANCE OF THE LT WHEN BRAKING OCCURS. CAPTAINS LT PEDAL FEELS NORMA - [SDR DXTA2010032304050](https://openairdocs.org/sdr/DXTA2010032304050), Mar 19, 2010: BRAKE. WEAK. BRAKES ARE DIFFICULT TO MODULATE & PERFORMANCE IS LESS THAN NORMAL. BRAKE PEDAL DEFLECTION ON BOTH SIDES IS MUCH MORE THAN NORMAL OPS. APPLIED & HELD STEADY BRA - [SDR DXTA2008123003449](https://openairdocs.org/sdr/DXTA2008123003449), Dec 29, 2008: LANDING GEAR. INOPERATIVE. LANDING GEAR WOULD NOT EXTEND. PERFORMED ALTERNATE GEAR EXTENSION PROCEDURE. - [SDR DXTA2008110603340](https://openairdocs.org/sdr/DXTA2008110603340), Nov 5, 2008: MASTER CYLINDER. LEAKING. UPON LANDING RT BRAKE PEDAL IN BOTH PILOT & COPILOTS POSITION WAS APPLIED TO FULLY DEPRESSED POSITION & RESPONDED WITH NEGATIVE BRAKING EFFECT ON BOTH POSITIONS - [SDR DXTA200809073268](https://openairdocs.org/sdr/DXTA200809073268), Sep 7, 2008: BRAKE ASSY. WEAK. RT BRAKE PEDAL DROPPED TO THE FLOOR ON BOTH SIDES UPON USAGE DURING LANDING ROLL. PIC IN LT SEAT PUMPED RT BRAKE PEDAL 3 TIMES AND RT BRAKE STARTED TO WORK AGAI - [SDR DXTA200702458](https://openairdocs.org/sdr/DXTA200702458), Sep 9, 2007: ANTI-SKID SYS. INOPERATIVE. ANTI SKID INOP ON LANDING IN SDF (HARD PEDALS AND WHEEL BRAKES LOCKING). RAN & TAXIED AIRCRAFT TO PERFORM OPERATIONAL CHECK AND TO VERIFY SQUAWK. COULD NOT DUPL - [SDR DXTA200601553](https://openairdocs.org/sdr/DXTA200601553), Aug 13, 2006: AIR DUCT. ODOR. DURING FLIGHT FROM SLC TO COS, HAD A BURNING SMELL IN COCKPIT AND CABIN WHEN ENG AND WING ANTI-ICE WAS TURNED ON, SMELL WAS STRONGER IN CABIN. FELT SIDE PANEL I ## 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/N114QS/stcs.md ## Related - Other Bombardier BD-700-1A11 aircraft: https://openairdocs.org/model/bombardier-bd-700-1a11/aircraft.md - The Rolls-Royce Deutschland BR700-710A220 engine: https://openairdocs.org/engine/rolls-royce-deutschland-br700-710a220.md --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.