# N749QS: 2017 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)
- Engine: [Honeywell AS907-2-1A](https://openairdocs.org/engine/honeywell-as907-2-1a) (registry code 33401)
- Data sheets: [TCDS T00005NY](https://openairdocs.org/tcds/T00005NY) (Bombardier Inc.), [TCDS E00010LA](https://openairdocs.org/tcds/E00010LA) (Honeywell Aerospace US LLC) (OpenAirDocs)
- Serial number: 20713
- Year built: 2017
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 21, 2017
- Certificate issued: April 16, 2025
- Expires: April 30, 2032
- Mode S code: AA1568
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=749QS
- Page: https://openairdocs.org/aircraft/N749QS

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): 55 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

### Matched by engine (Honeywell AS907-2-1A)

- [AD 2018-04-13](https://openairdocs.org/ad/2018-04-13): Engine Controls Section · Honeywell International AS907-1-1A, AS907-2-1A, AS907-2-1G and 1 more. Effective Apr 12, 2018

### 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 61: https://openairdocs.org/aircraft/N749QS/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 N749QS.

## NTSB investigations on N749QS not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB ERA11IA316](https://openairdocs.org/ntsb/ERA11IA316), May 27, 2011: Israel Aircraft Industries Gulfstream 200 (N749QS), Newburgh, NY, incident, minor damage. Probable cause: The flight crew did not ensure that the landing gear selector handle was in the full down (extend) position. Contributing to the incident was inadequate checklist information.

## FAA accident and incident reports

None matched to N749QS.

## Reports on N749QS not matched to an aircraft (1)

They name N749QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [Incident 20110527012289I](https://openairdocs.org/incident/20110527012289I), May 27, 2011: Israel Aircraft Industries GULFSTREAM 200 (N749QS), New Windsor, NY, Minor damage. On may 27, 2011, the subject aircraft was repositioned from savannah/hilton head international airport,savannah, ga (ksav) to greenville spartanburg…

## Service difficulty reports (5)

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 DXTA2026101410122](https://openairdocs.org/sdr/DXTA2026101410122), Oct 10, 2026: ENGINE. FLAMED OUT. DURING DESCENT AUDIBLE AND TACTILE VIBRATION OCCURRED FOLLOWED BY AMBER VIB INDICATION. RIGHT ENGINE INDICATIONS FLUCTUATED. RIGHT ENGINE FLAMED OUT. SECURED EN
- [SDR 2026FA0000162](https://openairdocs.org/sdr/2026FA0000162), Mar 8, 2026: ACCESS PANEL. CORRODED. CORROSION WAS FOUND ON THE LH AND RH WING ACCESS PLANK OPENINGS AND THERE WERE SEVERAL AREAS OUT OF LIMITS PER THE CL350 SRM WHICH REQUIRED ENGINEERING DISPOSIT
- [SDR DXTA2026010906468](https://openairdocs.org/sdr/DXTA2026010906468), Jan 6, 2026: AIR DATA MODULE. FAULTED. AT FL360 WE RECEIVED AMBER EFIS MISCOMPARE WITH AMBER ATL. THE RIGHT SIDE READ 200¿ LOWER THAN THE LT & STANDBY. WHEN SELECTING AIR DATA 1 PER THE CHECKLIST. R
- [SDR DXTA2025040102871](https://openairdocs.org/sdr/DXTA2025040102871), Mar 30, 2025: OVERHEAT LOOP. FAULTED. BLEED LOOP FAULT CYAN CAS: 2.5 HOURS INTO THE FLIGHT AT FL430 GOT CYAN BLEED LOOP FAULT CAS. IT REMAINED ON FOR ABOUT ANOTHER 30 MINUTES AND THEN EXTINGUISHED F
- [SDR DXTA2025031702661](https://openairdocs.org/sdr/DXTA2025031702661), Mar 13, 2025: POWER SUPPLY. FAULTY. CABIN EMERG LIGHT: DURING PREFLIGHT FIRST FLIGHT OF THE DAY TEST OF EMER LIGHTS TO ON POSITION SEATS 3R AND 2L DUAL USE EMER/READING LIGHTS DID NOT ILLUMINATE. 

## Service difficulty reports on N749QS not matched to an aircraft (12)

They name N749QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2015091406084](https://openairdocs.org/sdr/DXTA2015091406084), Sep 11, 2015: SPRING. WORN. UNCOMMANDED AUTOPILOT DISCONNECT AT FL410. AILERONS WERE STIFF UNTIL REACHING FL270. REMOVED AND REPLACED A WORN AILERON FEEL SPRING. PERFORMED SATISFACTORY OPS
- [SDR DXTA2014120805941](https://openairdocs.org/sdr/DXTA2014120805941), Dec 6, 2014: BATTERY. OVERHEATED. DURING FLIGHT THE EMERGENCY BATTERY OVERHEAT EICAS ILLUMINATED. REPLACED THE EMERGENCY BATTERY. PERFORMED OPS CHECKS WITH NO DEFECTS NOTED. ACCOMPLISHED IAW AMM
- [SDR DXTA2014042505744](https://openairdocs.org/sdr/DXTA2014042505744), Apr 24, 2014: CONTROL COLUMN. CHAFED. LEFT PILOT CONTROL COLUMN HAS CHAFING MARKS FROM THE AILERON CABLE INSIDE COLUMN. RIGHT COPILOT CONTROL COLUMN HAS CHAFING MARKS FROM THE AILERON CABLE INSIDE C
- [SDR DXTA2013101405539](https://openairdocs.org/sdr/DXTA2013101405539), Oct 18, 2013: WINDOW. CRACKED. PILOT SIDE WINDSREEN, SPIDER WEB CRACKED, COVERING ENTIRE PANEL. REMOVED CRACKED WINDOW, PERFORMED WINDSHIELD AND SIDE WINDOW TEMP SENSING ELEMENT RESISTANCE CH
- [SDR DXTA2012120305199](https://openairdocs.org/sdr/DXTA2012120305199), Dec 1, 2012: UNKNOWN. ODOR. ELECTRICAL ODOR EMENATED FROM WHAT SEEMED LIKE THE OVERHEAD PANEL. FOUND NO EVIDENCE OF OVERHEATING OR SHORTING. OPERATED ELECTRICALS, NO EVIDENCE OF AN ELECTRI
- [SDR LM1R20120731002](https://openairdocs.org/sdr/LM1R20120731002), Jul 18, 2012: CARBON SEAL. FAILED. AFTER TAKEOFF, CREW NOTICED BURNING ODOR AND MIST IN CABIN. PERFORMED EMERGENCY RETURN TO DEPARTURE. FOUND OIL STREAKING IN EXHAUST AND FOD IN COMPRESSOR SECTIO
- [SDR DXTA201207190553](https://openairdocs.org/sdr/DXTA201207190553), Jul 18, 2012: ENGINE. ODOR. AFTER TAKEOFF, SMELLED A BURNING SMELL AND THERE WAS WHAT APPEARED TO BE A MIST IN THE CABIN. PERFORMED AN EMERGENCY RETURN TO DEPARTURE. INSPECTED RT ENGINE AN
- [SDR DXTA2011100604741](https://openairdocs.org/sdr/DXTA2011100604741), Oct 4, 2011: COMPUTER. SMOKE. WHEN ACFT WAS POWERED UP, SMOKE CAME OUT OF THE COMPUTER BOX. REMOVED COMPUTER AND INSTALLED A REPAIRED COMPUTER WITH ORIGINAL SOFTWARE CD. ALL OPS CHECKED GOOD
- [SDR DXTA2011052704596](https://openairdocs.org/sdr/DXTA2011052704596), May 27, 2011: LANDING GEAR. COLLAPSED. GEAR COLLAPSED ON LANDING.
- [SDR DXTA2010120504349](https://openairdocs.org/sdr/DXTA2010120504349), Dec 5, 2010: ACTUATOR. MALFUNCTIONED. RT MAIN GEAR WOULD NOT RETRACT. GREEN DOWN AND LOCKED INDICATION STAYED STEADY. CREW COULD FEEL A DRAG OF THE LANDING GEAR ON RETURN TO FIELD. REPLACED RT MLG A
- [SDR DXTA2010110804298](https://openairdocs.org/sdr/DXTA2010110804298), Nov 5, 2010: ECU. MALFUNCTIONED. WHILE CRUISING AT FL230 WE GOT A "GEAR NOT DOWN" CAS MESSAGE ALONG WITH THE GEAR WARNING HORN AND THE RT PFD AIRSPEED INDICATOR TURNED RED. RECEIVED ALL NORMAL 
- [SDR DXTA200802747](https://openairdocs.org/sdr/DXTA200802747), Jan 4, 2008: SQUAT SWITCH. MALFUNCTIONED. GROUND AIR BRAKES DEPLOYED ON FINAL APPROACH WHEN THE SWITCH WAS ARMED. R & R LT MLG WOW SWITCH AND HARNESS IAW AMM 32-60-05. OPERATIONAL & FUNCTIONAL CHECK GOO

## 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/N749QS/stcs.md

## Related

- Other Bombardier BD-100-1A10 aircraft: https://openairdocs.org/model/bombardier-bd-100-1a10/aircraft.md
- The Honeywell AS907-2-1A engine: https://openairdocs.org/engine/honeywell-as907-2-1a.md

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