# N700QS: Bombardier BD-100-1A10

- Status: Valid registration
- Airframe: [Bombardier BD-100-1A10](https://openairdocs.org/model/bombardier-bd-100-1a10) (registry code 1390044, 8 seats)
- Data sheets: [TCDS T00005NY](https://openairdocs.org/tcds/T00005NY) (Bombardier Inc.) (OpenAirDocs)
- Serial number: 20792
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: September 26, 2025
- Expires: September 30, 2032
- Mode S code: A955FD
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=700QS
- Page: https://openairdocs.org/aircraft/N700QS

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): 54 in force

### Matched by airframe (Bombardier BD-100-1A10)

- [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 2026-02-06](https://openairdocs.org/ad/2026-02-06): Flight controls · Bombardier BD-100-1A10. Effective Feb 25, 2026
- [AD 2026-01-07](https://openairdocs.org/ad/2026-01-07): Time Limits/Maintenance Checks · Bombardier BD-100-1A10. Effective Feb 20, 2026
- [AD 2025-02-01](https://openairdocs.org/ad/2025-02-01): Flight controls · Bombardier BD-100-1A10. Effective Mar 17, 2025
- [AD 2024-21-04](https://openairdocs.org/ad/2024-21-04): Electrical Power · Bombardier BD-100-1A10. Effective Dec 17, 2024
- [AD 2024-18-03](https://openairdocs.org/ad/2024-18-03): Electrical Power · Bombardier BD-100-1A10. Effective Nov 12, 2024
- [AD 2024-16-18](https://openairdocs.org/ad/2024-16-18): Nacelles/Pylons · Bombardier BD-100-1A10. Effective Oct 30, 2024
- [AD 2024-16-13](https://openairdocs.org/ad/2024-16-13): Ice and Rain Protection · Bombardier BD-100-1A10. Effective Oct 29, 2024
- [AD 2024-16-04](https://openairdocs.org/ad/2024-16-04): Equipment/Furnishings · Bombardier BD-100-1A10. Effective Oct 23, 2024
- [AD 2024-11-02](https://openairdocs.org/ad/2024-11-02): Stabilizer · Bombardier BD-100-1A10. Effective Aug 26, 2024
- [AD 2024-01-09](https://openairdocs.org/ad/2024-01-09): Landing gear · Bombardier BD-100-1A10. Effective Mar 21, 2024
- [AD 2023-26-02](https://openairdocs.org/ad/2023-26-02): Pneumatic · Bombardier BD-100-1A10 (Challenger 300). Effective Feb 27, 2024
- [AD 2023-23-05](https://openairdocs.org/ad/2023-23-05): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Dec 14, 2023
- [AD 2023-13-06](https://openairdocs.org/ad/2023-13-06): Time limits/maintenance checks, Landing Gear · Bombardier BD-100-1A10 (Challenger 300). Effective Sep 1, 2023
- [AD 2023-14-11](https://openairdocs.org/ad/2023-14-11): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 10, 2023
- [AD 2023-12-06](https://openairdocs.org/ad/2023-12-06): Auto flight · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 7, 2023
- [AD 2023-11-04](https://openairdocs.org/ad/2023-11-04): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 21, 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 2023-03-18](https://openairdocs.org/ad/2023-03-18): Fuselage · Bombardier BD-100-1A10 (Challenger 300). Effective Apr 4, 2023
- [AD 2023-02-01](https://openairdocs.org/ad/2023-02-01): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Mar 14, 2023
- [AD 2022-12-02](https://openairdocs.org/ad/2022-12-02): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 21, 2022
- [AD 2022-09-02](https://openairdocs.org/ad/2022-09-02): Landing gear · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 16, 2022
- [AD 2022-03-11](https://openairdocs.org/ad/2022-03-11): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Mar 17, 2022
- [AD 2021-25-07](https://openairdocs.org/ad/2021-25-07): Landing gear · Bombardier BD-100-1A10 (Challenger 300). Effective Feb 15, 2022
- [AD 2021-23-14](https://openairdocs.org/ad/2021-23-14): Electrical power · Bombardier BD-100-1A10 (Challenger 300). Effective Jan 10, 2022
- [AD 2021-14-01](https://openairdocs.org/ad/2021-14-01): Navigation · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 24, 2021
- [AD 2021-10-26](https://openairdocs.org/ad/2021-10-26): Hydraulic power · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 6, 2021
- [AD 2021-09-17](https://openairdocs.org/ad/2021-09-17): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 23, 2021
- [AD 2021-09-16](https://openairdocs.org/ad/2021-09-16): Pneumatic; Engine Fuel and Control · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 1, 2021
- [AD 2021-03-10](https://openairdocs.org/ad/2021-03-10): Fire protection · Bombardier BD-100-1A10 (Challenger 300). Effective Mar 31, 2021
- [AD 2020-25-06](https://openairdocs.org/ad/2020-25-06): Landing gear · Bombardier BD-100-1A10 (Challenger 300). Effective Jan 27, 2021
- [AD 2020-11-14](https://openairdocs.org/ad/2020-11-14): Navigation · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 21, 2020
- [AD 2020-11-10](https://openairdocs.org/ad/2020-11-10): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 14, 2020
- [AD 2019-15-04](https://openairdocs.org/ad/2019-15-04): Flight controls · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 23, 2019
- [AD 2019-03-29](https://openairdocs.org/ad/2019-03-29): Landing Gear · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 6, 2019
- [AD 2019-07-06](https://openairdocs.org/ad/2019-07-06): Landing Gear · Bombardier BD-100-1A10 (Challenger 300). Effective May 28, 2019
- [AD 2018-20-16](https://openairdocs.org/ad/2018-20-16): Hydraulic Power · Bombardier BD-100-1A10 (Challenger 300). Effective Nov 23, 2018
- [AD 2018-14-05](https://openairdocs.org/ad/2018-14-05): SUMMARY: We are adopting a new airworthiness directive (AD) for certain  
 Bombardier, Inc., Model BD-100-1A10 airplanes. This AD was prompted by reports  
 of fire incidents of the auxiliary power unit (APU) inlet, which caused tail  
 cone damage after an initial failed APU start followed by two or more in-flight  
 APU start attempts. This AD requires modification of the APU electronic control  
 unit (ECU) wiring harness. We are issuing this AD to address the unsafe · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 13, 2018
- [AD 2018-13-04](https://openairdocs.org/ad/2018-13-04): Oxygen · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 25, 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 2017-17-13](https://openairdocs.org/ad/2017-17-13): Electrical power · Bombardier BD-100-1A10 (Challenger 300). Effective Oct 2, 2017
- [AD 2017-14-16](https://openairdocs.org/ad/2017-14-16): Fuselage · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 1, 2017
- [AD 2017-12-11](https://openairdocs.org/ad/2017-12-11): Equipment/ Furnishings · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 20, 2017
- [AD 2017-11-12](https://openairdocs.org/ad/2017-11-12): Landing gear · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 11, 2017
- [AD 2016-02-05](https://openairdocs.org/ad/2016-02-05): Navigation · Bombardier BD-100-1A10 (Challenger 300). Effective Mar 8, 2016
- [AD 2015-26-03](https://openairdocs.org/ad/2015-26-03): Equipment/Furnishings · Bombardier BD-100-1A10 (Challenger 300). Effective Feb 2, 2016
- [AD 2015-23-07](https://openairdocs.org/ad/2015-23-07): Electrical Power · Bombardier BD-100-1A10 (Challenger 300). Effective Dec 22, 2015
- [AD 2015-15-08](https://openairdocs.org/ad/2015-15-08): Flight Controls · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 28, 2015
- [AD 2014-05-23](https://openairdocs.org/ad/2014-05-23): Electrical power · Bombardier BD-100-1A10 (Challenger 300). Effective Apr 15, 2014
- [AD 2012-12-17](https://openairdocs.org/ad/2012-12-17): Oxygen · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 30, 2012

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

- [AD 2023-11-01](https://openairdocs.org/ad/2023-11-01) (historical): Electrical Power · Bombardier BD-100-1A10 (Challenger 300). Effective Aug 15, 2023
- [AD 2020-07-13](https://openairdocs.org/ad/2020-07-13) (historical): Auto flight · Bombardier BD-100-1A10 (Challenger 300). Effective May 18, 2020
- [AD 2013-11-12](https://openairdocs.org/ad/2013-11-12) (historical): Hydraulic Power · Bombardier BD-100-1A10 (Challenger 300). Effective Jul 9, 2013
- [AD 2011-07-10](https://openairdocs.org/ad/2011-07-10) (historical): Air conditioning · Bombardier BD-100-1A10 (Challenger 300). Effective May 5, 2011
- [AD 2010-10-18](https://openairdocs.org/ad/2010-10-18) (historical): Air conditioning and Equipment/Furnishings · Bombardier BD-100-1A10 (Challenger 300). Effective Jun 1, 2010
- [AD 2009-25-13](https://openairdocs.org/ad/2009-25-13) (historical): Equipment/Furnishings · Bombardier BD-100-1A10 (Challenger 300). Effective Dec 28, 2009

All 60: https://openairdocs.org/aircraft/N700QS/ads.md

## Information bulletins (advisory) (2 in force)

- [SAIB AIR-22-02R1](https://openairdocs.org/saib/AIR-22-02R1): PITOT/STATIC ANTI-ICE SYSTEM. Issued May 17, 2022
- [SAIB NM-18-32R1](https://openairdocs.org/saib/NM-18-32R1): Electrical Power - Direct Current Power Center. Issued Mar 22, 2021
- [SAIB AIR-22-02](https://openairdocs.org/saib/AIR-22-02) (historical): PITOT/STATIC ANTI-ICE SYSTEM. Issued Feb 25, 2022
- [SAIB NM-18-32](https://openairdocs.org/saib/NM-18-32) (historical): Electrical Power - Direct Current Power Center. Issued Dec 3, 2018

## NTSB investigations

None matched to N700QS.

## FAA accident and incident reports

None matched to N700QS.

## Reports on N700QS not matched to an aircraft (1)

They name N700QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20070502008529I](https://openairdocs.org/incident/20070502008529I), May 2, 2007: Israel GALAXY (N700QS), Las Vegas, NV, Minor damage. (-23) On 05/03/2007 inspectors from the las FSDO were contacted by mccarran international airport that a Galaxy G-200, N700QS, may have scraped a wing tip…

## Service difficulty reports (4)

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 DXTA2026082109351](https://openairdocs.org/sdr/DXTA2026082109351), Aug 19, 2026: PROXIMITY SENSOR. FAULTED. ON APPROACH TO LANDING WITH GEAR SELECTED DOWN, CAS MESSAGE PROX SYS FAULT APPEARED B3-224420. REPEAT WRITE UP. ON LANDING ROLLOUT, AFTER SIGNIFICANT SHUDDERING
- [SDR DXTA2025081504618](https://openairdocs.org/sdr/DXTA2025081504618), Aug 15, 2025: TRANSDUCER. OUT OF ADJUST. AIRCRAFT PULLS TO THE LEFT WHILE TAXING. CONSTANT RIGHT TILLER OR RUDDER IS REQUIRED. AIRCRAFT PULLS HARDER TO THE LEFT WHEN MODERATE BRAKING IS APPLIED. PERFOR
- [SDR DXTA2024031311184](https://openairdocs.org/sdr/DXTA2024031311184), Mar 13, 2024: TRANSDUCER. DEFECTIVE. AFTER TAKEOFF WE RECEIVED A R HYD TEMP HIGH AMBER CAS. RAN QRH. HYDRAULIC TEMP ON RIGHT SIDE EXCEEDED 155° (APPROXIMATELY 209°) AND PROCEEDED TO SHUTDOWN RT ENG
- [SDR DXTA2020100504171](https://openairdocs.org/sdr/DXTA2020100504171), Oct 5, 2020: DCU. FAULTED. DCU B B3-006531 DCU "A" B3-006494 BRAKE FAULT B3-22442 UPON SELECTING GEAR DOWN WE GOT A MAGENTA BOX WITH DASHES ON THE RIGHT MAIN GEAR. WE ALSO GOT THE FOLLOWI

## Service difficulty reports on N700QS not matched to an aircraft (22)

They name N700QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2013112005574](https://openairdocs.org/sdr/DXTA2013112005574), Nov 19, 2013: ENGINE. DAMAGED. CLIMBING THROUGH 38000' IN MAX CLIMB DETENT 290KTS TWO DISTINCT BANGS, SIMILAR TO COMPRESSOR STALLS, WERE FELT THROUGH FLOOR, RUDDERS & CONTROLS. ALL INSTRUMENT
- [SDR DXTA2012051104974](https://openairdocs.org/sdr/DXTA2012051104974), May 9, 2012: WARNING LIGHT. ILLUMINATED. ON APPROACH, AT 170KIAS THE LANDING GEAR WAS LOWERED. THE NOSE AND LT MAIN GEAR INDICATIONS WERE NORMAL. THE RT MAIN GEAR SHOWED AMBER FOR ABOUT 10 SECONDS FOLL
- [SDR DXTA2012030704907](https://openairdocs.org/sdr/DXTA2012030704907), Mar 6, 2012: SELECTOR VALVE. LEAKING. ON GEAR EXTENSION, RECEIVED GREEN LIGHTS FOR LT MAIN AND NOSE GEAR BUT THE RT MAIN INDICATED YELLOW FOR APPROX 20 SECONDS FOLLOWED BY A RED "UNSAFE" INDICATION 
- [SDR DXTA2012030104893](https://openairdocs.org/sdr/DXTA2012030104893), Feb 29, 2012: SELECTOR VALVE. INOPERATIVE. ON GEAR EXTENSION, RECEIVED GREEN LIGHTS FOR THE LT MAIN AND NOSE GEAR BUT THE RT MAIN INDICATED YELLOW FOR APPROX 20 SECONDS FOLLOWED BY A RED "UNSAFE" INDICAT
- [SDR DXTA2011112804803](https://openairdocs.org/sdr/DXTA2011112804803), Nov 27, 2011: ACTUATOR. SLOW. RT MAIN GEAR DIDN'T INITIALLY COME DOWN WHEN SELECTED. GO AROUND INTIATED MAINTAINING APPROX 170 KNOTS. QRH REFERENCED, GEAR CAME DOWN AFTER APPROX 2 MINUTES. L
- [SDR DXTA2011111504791](https://openairdocs.org/sdr/DXTA2011111504791), Nov 14, 2011: STRUT. LEAKING. AFTER GEAR RETRACTION NOSE GEAR STUCK INDICATION. NO RELATED AIR NOISE FROM GEAR HANGING OUT NOTED. EXTENDED GEAR AND LANDED NORMAL. HYD FLUID LEAKAGE COMING FR
- [SDR DXTA2011091204723](https://openairdocs.org/sdr/DXTA2011091204723), Sep 10, 2011: ACTUATOR. LEAKING. WHEN PUTTING GEAR DOWN, NOSE & LT MAIN LOCKED DOWN NORMALLY. RT MAIN DIDN'T GIVE A INDICATION FOR ABOUT 5 SECONDS THEN TURNED YELLOW FOR ABOUT ANOTHER 5 SECONDS
- [SDR DXTA2011080204680](https://openairdocs.org/sdr/DXTA2011080204680), Jul 31, 2011: ACTUATOR. INOPERATIVE. UPON GEAR EXTENSION, THE RT MAIN GEAR INDICATION TURNED AMBER FOR A SHORT PERIOD OF TIME, THEN TURNED RED. THE RT ANTI-SKID OFF ILLUMINATED AS WELL. RECYCLED TH
- [SDR DXTA2011080204679](https://openairdocs.org/sdr/DXTA2011080204679), Jul 25, 2011: LANDING GEAR. MALFUNCTIONED. AFTER GEAR EXTENSION, RECEIVED A RED GEAR UNSAFE INDICATION. FOLLOWED THE QRH WITH 2 EXTENSIONS BEFORE THE INDICATION WAS GEAR DOWN AND LOCKED. COMPLIED WITH GE
- [SDR DXTA2011062404635](https://openairdocs.org/sdr/DXTA2011062404635), Jun 23, 2011: TRIM SYSTEM. MALFUNCTIONED. ON CLIMBOUT, AUTOPILOT PITCH TRIM FAIL EICAS MESSAGE ILLUMINATED. THE AUTOPILOT CONTINUED TO TRY TO TRIM, BUT TRIM CHANGE WAS NOT OCCURRING. AUTOPILOT DISCONNEC
- [SDR DXTA2011061404613](https://openairdocs.org/sdr/DXTA2011061404613), Jun 12, 2011: ACTUATOR. INTERMITTENT. UPON GEAR EXTENSION THE RT MAIN GEAR INDICATION TURNED AMBER FOR A WHILE THEN IT TURNED RED AND STAYED RED FOR APPROX 1 TO 2 MINUTES. IT THEN TURNED GREEN. LAND
- [SDR DXTA2010060104107](https://openairdocs.org/sdr/DXTA2010060104107), May 27, 2010: ACTUATOR. FAULTY. UPON LANDING GEAR EXTENTION THE RT MLG SHOWED A AMBER UNKNOWN POSITION THEN A RED UNSAFE POSITION. AFTER A MINUTE IT SHOWED A DOWN AND LOCKED POSITION. REMOVED 
- [SDR DXTA200803089](https://openairdocs.org/sdr/DXTA200803089), Jun 1, 2008: WIRE. OUT OF POSITION. UPON FULL POWER APPLICATION AT APPROX 40KTS, RED BLEED PRESS / TEMP HI WARNING LIGHTCAME ON. ABORTED TAKEOFF. FOUND OVERPRESSURE SWITCH WIRES VERY CLOSE TO AN A
- [SDR DXTA200802759](https://openairdocs.org/sdr/DXTA200802759), Jan 10, 2008: FLOAT VALVE. FAILED. IN CRUISE FLIGHT AT FL380 WE NOTICED FUEL LEAKING OUT OVER THE LT AILERON. REMOVED DEFECTIVE LEFT WING VENT FLOAT VALVE AND INSTALLED NEW VALVE PER G200 CMP 285
- [SDR DXTA200702431](https://openairdocs.org/sdr/DXTA200702431), Aug 27, 2007: SIGHT GLASS. CRACKED. LT ENG OIL PRESS LOW EICAS MSG ON CLIMB OUT. (OIL PRESS 5 PSI INDICATED ON LT ENG) COMPLIED WITH QRH AND SECURED/SHUTDOWN ENG. REMOVED LT ENGINE UPPER AND LOWER
- [SDR DXTA200601483](https://openairdocs.org/sdr/DXTA200601483), Jul 5, 2006: ODOR. UNKNOWN. DURING FLIGHT FROM AFW TO EGE, STRONG EXHAUST ODOR IN THE COCKPIT AND DID NOT GO AWAY UNTIL AFTER SHUTDOWN. BORESCOPED LT, RT, APU BLEED AIR DUCTS LEADING TO AC
- [SDR DXTA200601317](https://openairdocs.org/sdr/DXTA200601317), Mar 24, 2006: ENGINE. WARNING MESSAGE. UPON APPLICATION OF TAKEOFF POWER, HAD A MASTER WARNING INDICATION. IT APPEARED TO BE THE BLEED PRESS/TEMP HI MESSAGE. MESSAGE WENT OUT IMMEDIATELY WHEN RETARDI
- [SDR DXTA200500980](https://openairdocs.org/sdr/DXTA200500980), Sep 23, 2005: FUEL FILTER. CLOGGED. LEFT FUEL PRESS, LOW CAS MESSAGE ILLUMINATED ON TAKEOFF ROLL. ABORTED TAKEOFF AT 75 KNOTS. REPLACED FUEL FILTERS (BOTH ENGINES) AND LEAK CHECKED, NO LEAKS NOTED
- [SDR DXTA200500975](https://openairdocs.org/sdr/DXTA200500975), Sep 18, 2005: TRIM SYSTEM. MALFUNCTIONED. IMMEDIATELY AFTER TAKEOFF THE NORMAL PITCH TRIM FROZE AT 2.6 DEG SETTING. AFTER SEVERAL MINUTES AND SEVERAL ATTEMPTS AT NOSE DOWN TRIM, SYSTEM WORKED NORMAL, HO
- [SDR DXTA200400269](https://openairdocs.org/sdr/DXTA200400269), Mar 18, 2004: AMPLIFIER. OVERHEATED. DURING FLIGHT CREW DETECTED SMOKE IN THE COCKPIT, NOTICED SMOKE COMING OUT FROM BEHIND THE BOTTOM FORWARD 2 DRAWS. TURNED THE GALLEY POWER OFF AND AFTER A FEW M
- [SDR DXTA200400258](https://openairdocs.org/sdr/DXTA200400258), Mar 8, 2004: ODOR. DETECTED. AFTER 1.5 HOURS INTO FLIGHT, CREW NOTICED EXHAUST ODOR IN COCKPIT, SELECTED DIFFERENT AIR SUPPLY AND PROBLEM REMAINED. PRECAUTIONARY DIVERTED TO ABQ. ITEM IS UN
- [SDR DXTA200300028](https://openairdocs.org/sdr/DXTA200300028), May 5, 2003: OIL CAP. LOOSE. ON CLIMBOUT RIGHT ENGINE LOW OIL PRESSURE MESSAGE CAME ON. RETARDED THROTTLE TO IDLE AND ENGINE PRESS DROPPED TO ZERO. SHUTDOWN THE RIGHT ENGINE PER CHECKLIST A

## 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-100-1A10)

- [STC ST11935CH](https://openairdocs.org/stc/ST11935CH): Installation of SpaceX Starlink Aviation System. Nextant Aerospace
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST00952LA](https://openairdocs.org/stc/ST00952LA): Installation of Mass Systems fire extinguisher cartridges as replacements for Kidde fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON LLC d/b/a MASS Systems
- [STC ST12288IB](https://openairdocs.org/stc/ST12288IB): Demonstration of TPED Tolerance. Bombardier Inc
- [STC ST00892LA](https://openairdocs.org/stc/ST00892LA): Installation of Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [STC ST12036WI](https://openairdocs.org/stc/ST12036WI): Installation of Gogo Business Aviation Galileo Half-Duplex (HDX). Gogo Business Aviation LLC
- [STC ST03292CH](https://openairdocs.org/stc/ST03292CH): Activation of an 802.11 a/b/g/n WiFi System. Elliott Aviation Technical Products Development, Inc
- [STC ST04560AT](https://openairdocs.org/stc/ST04560AT): Replacement of the existing Honeywell HTF7000 engine upper and lower thrust reverser door assemblies with Quiet Technology Aerospace modified upper and lower thrust reverser door assemblies. Quiet Technology Aerospace
- [STC ST01569LA](https://openairdocs.org/stc/ST01569LA): Installation of Floor Proximity Emergency Escape Path Marking System. Bruce Aerospace Inc
- [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 ST02691SE](https://openairdocs.org/stc/ST02691SE): Installation of Head-up Display System (HUD) Model 6650 and Enhance Vision System (EVS) Model 3600. Rockwell Collins Inc
- [STC ST01117DE](https://openairdocs.org/stc/ST01117DE): Installation of the Gogo ATG C1. Peregrine
- [STC ST00079IB](https://openairdocs.org/stc/ST00079IB): Integration of Halon-free Portable Fire Extinguisher HAFEX. UMLAUT ENGINEERING GMBH
- [STC ST01833WI](https://openairdocs.org/stc/ST01833WI): Modification of a Rockwell Collins Global Positioning System (GPS) installation. Rockwell Collins Inc
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST00200IB](https://openairdocs.org/stc/ST00200IB): Installation of Gogo AVANCE L5 System. Sky Service F.B.O. Inc
- [STC ST03424CH](https://openairdocs.org/stc/ST03424CH): Certification of Automatic Dependent Surveillance - Broadcast (ADS-B) Out System with Rockwell Collins TDR-94/-94D Transponders. CMD Flight Solutions LLC
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST01970WI](https://openairdocs.org/stc/ST01970WI): Installation of an Aircraft Health Management System (AHMS). Learjet Inc
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST01985WI](https://openairdocs.org/stc/ST01985WI): Installation of the Garmin GI-275 I Electronic Standby Instrument (ESI). Peregrine
- [STC ST02765LA](https://openairdocs.org/stc/ST02765LA): Installation of the Honeywell EDG-100 Connected Engine Data Access System. Honeywell International Inc
- [STC ST04544CH](https://openairdocs.org/stc/ST04544CH): Installation of a Viasat Business Aviation Router (VBR) P/N 1371388. StandardAero Business Aviation Services LLC
- [STC ST04327CH](https://openairdocs.org/stc/ST04327CH): Installation of High Speed Internet System and Wireless Activation. Nextant Aerospace LLC
- [STC ST01991WI](https://openairdocs.org/stc/ST01991WI): Installation of Switch Bezels. Duncan Aviation Inc
- [STC ST11285DS](https://openairdocs.org/stc/ST11285DS): An update to the existing Collins Aerospace Integrated Flight Information System (IFIS) FSU-5010 and upgrade the existing XMWR-1000 to a XMWR-1000S (Sirius XM) in Part 25. BHE & Associates Ltd
- [STC ST04490CH](https://openairdocs.org/stc/ST04490CH): Installation of a Viasat Business Aviation Router (VBR) P/N 1371388 in accordance with StandardAero Master Data List 1039044, Revision (B), dated November 13, 2020 or later FAA approved revision. Learjet Inc
- [STC ST02293SE](https://openairdocs.org/stc/ST02293SE): Installation of a Crane Aerospace & Electronics Tire Sensor Assembly. ELDEC Aerospace Corp
- [STC ST04508CH](https://openairdocs.org/stc/ST04508CH): Installation of a Collins KuSAT-2000 Tail-Mounted SATCOM System and a KuKa Radome in accordance with Master Data List (MDL), 1039410, Revision (F), dated November 05, 2021, or later FAA Approved Revision. StandardAero Business Aviation Services LLC
- [STC ST02047NY](https://openairdocs.org/stc/ST02047NY): Modification of Complete Custom Aircraft Interior to be completed. Bombardier Aerospace
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST04455CH](https://openairdocs.org/stc/ST04455CH): Installation of a Viasat Ka Radome in accordance with StandardAero Master Data List 1038145, Revision (E), dated November 13, 2020 or later FAA approved revision. Learjet Inc
- [STC ST04457CH](https://openairdocs.org/stc/ST04457CH): Installation of a Viasat Ka Terminal in accordance with StandardAero Master Data List 1038079, Revision (B), dated November 14, 2020 or later FAA approved revision. Learjet Inc
- [STC ST01270WI-D](https://openairdocs.org/stc/ST01270WI-D): Installation of Honeywell MK V and MK VII EGPWS Runway Awareness and Advisory System (RAAS). This approval is limited to specifically idenitfied aircraft. Duncan Aviation Inc
- [STC ST04352NY](https://openairdocs.org/stc/ST04352NY): Installation of Fire Extinguishers with Halocarbon Clean Extinguishing Agents. Bombardier Inc
- [STC ST04391NY](https://openairdocs.org/stc/ST04391NY): Installation of Galley with Compartment for Commercial-off-the-shelf (COTS) Appliances or Equipment. Bombardier Inc
- [STC ST00923DE](https://openairdocs.org/stc/ST00923DE): Demonstration of Aircraft Compatibility to Wireless Fidelity (WiFi) Data Transmissions (Ground & Flight). West Star Aviation
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS
- [STC ST00395BO](https://openairdocs.org/stc/ST00395BO): Installation of a Honeywell GoDirect Router. Pro Star Aviation, LLC
- [STC ST04236NY](https://openairdocs.org/stc/ST04236NY): Installation of Lavatory Glass Mirror. Bombardier Inc
- [STC ST00267BO](https://openairdocs.org/stc/ST00267BO): Installation of a Honeywell HD-710 High Speed Data Receiver, EMS AMT-50 High Gain Antenna System, and EMS CNX-200 Cabin Network Router in accordance with Pro Star Aviation Master Document List 20674-MDL-02, Revision D, dated March 17, 2008, or later FAA-approved revision. Pro Star Aviation, LLC
- [STC ST00268BO](https://openairdocs.org/stc/ST00268BO): Installation of an EMS Satcom AMT-50 High Gain Antenna System. Pro Star Aviation, LLC
- [STC ST02130LA](https://openairdocs.org/stc/ST02130LA): Installation of Honeywell MKV Enhanced Ground Proximity Warning System (EGPWS) with Runway Awareness and Advisory System (RAAS). Pro Star Aviation, LLC
- [STC ST04148NY](https://openairdocs.org/stc/ST04148NY): Installation of the Rockwell Collins TDR-94D ADS-B Out Upgrade. Mid Canada Mod Center
- [STC ST02976NY](https://openairdocs.org/stc/ST02976NY): Installation of ADS-B Out System in the Bombardier BD-100-1A10 (CH 300) aircraft with Rockwell Collins Pro Line 21 Series Avionics System. Flying Colours Corp
- [STC ST04123NY](https://openairdocs.org/stc/ST04123NY): Installation of Bleed Air Leak Detection System Loop Element Shell and Insert Assembly Replacement. Bombardier Inc
- [STC ST04290CH](https://openairdocs.org/stc/ST04290CH): Wireless Local Area Network (WLAN) Cabin Router and Aircraft Transmitting Portable Electronic Device (TPED) Compatibility. Comlux America LLC
- [STC ST00896DE](https://openairdocs.org/stc/ST00896DE): Installation of a 3-Place Side-Facing Divan. Lee Products Engineering Services, Inc

All 141: https://openairdocs.org/aircraft/N700QS/stcs.md

## Related

- Other Bombardier BD-100-1A10 aircraft: https://openairdocs.org/model/bombardier-bd-100-1a10/aircraft.md

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