# N745QS: 2022 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: 20935
- Year built: 2022
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 27, 2022
- Certificate issued: December 30, 2022
- Expires: December 31, 2029
- Mode S code: AA068C
- Owner type: Corporation
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=745QS
- Page: https://openairdocs.org/aircraft/N745QS

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/N745QS/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 N745QS.

## FAA accident and incident reports

None matched to N745QS.

## Service difficulty reports (1)

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 DXTA2026031307230](https://openairdocs.org/sdr/DXTA2026031307230), Mar 11, 2026: BRAKE. SMOKE. AFTER LANDING BOTH LEFT MAIN BRAKES WERE SMOKING EXCESSIVELY AND GENERATING HEAT. REQUEST EVALUATION. CORRECTIVE ACTION: PERFORMED INSPECTION OF LH MAIN BRAKE A

## Service difficulty reports on N745QS not matched to an aircraft (12)

They name N745QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2014092205889](https://openairdocs.org/sdr/DXTA2014092205889), Sep 19, 2014: FITTING. LOOSE. AFTER LANDING HEAVY SMOKE FROM BOTH MLG BRAKES. LANDING ROLL OUT WAS APPROX 6000FT FROM 100KTS TO TAXI SPEED BRAKES SEEMED TO FADE REQUIRING MORE PEDAL PRESSURE
- [SDR DXTA2013071705449](https://openairdocs.org/sdr/DXTA2013071705449), Jul 16, 2013: UNKNOWN. LEAKING. DURING CLIMB THROUGH 5000', RECEIVED A LT ENG OIL LEVEL LOW MESSAGE. CONFIRMED WITH IDICATOR AT 22 PSI. OIL INCREASED SLIGHTLY TO 33-36, RAPIDLY DROPPED TO 0 PS
- [SDR DXTA201307175549](https://openairdocs.org/sdr/DXTA201307175549), Jul 16, 2013: OIL SYSTEM. LEAKING. DURING CLIMB THROUGH 5000', RECEIVED A LT ENGINE OIL LEVEL LOW MESSAGE. CONFIRMED WITH IDICATOR AT 22 PSI. OIL INCREASED SLIGHTLY TO 33-36, THEN RAPIDLY DROPPED
- [SDR DXTA2013071105440](https://openairdocs.org/sdr/DXTA2013071105440), Jul 11, 2013: TIRE. DEFLATED. LEFT OTBD MAIN TIRE FLAT, WENT FLAT AFTER LANDING AND ANTI-SKID LIGHT CAME ON AND STAYED ON AFTER LANDING. REPLACED NR 1 & 2 WHEEL ASSY IAW MM 32-42-02. R & R N
- [SDR DXTA2013042905362](https://openairdocs.org/sdr/DXTA2013042905362), Apr 28, 2013: DIODE. FAILED. SHORT 15 MINUTES FLIGHT FROM T82 TO SAT AT 5000 FEET, WITHIN 5 MINUTES WE ENCOUNTER AN ELECTRIC BURNING SMELL IN THE COCKPIT. CONTINUED AND THE SMELL GOT STRONG
- [SDR DXTA2011072604673](https://openairdocs.org/sdr/DXTA2011072604673), Jul 25, 2011: CIRCUIT CARD. BURNED. AFTER TAKEOFF, NOTICED A VERY SLIGHT ELECTRICAL SMOKE ODOR. AFTER CLIMBING THROUGH 24000', ODOR STRONGER & "LT & RT ICE DETECT FAIL" EICAS CAUTIONS CAME ON SIMU
- [SDR DXTA2011040104534](https://openairdocs.org/sdr/DXTA2011040104534), Mar 31, 2011: CONTROL PANEL. FAILED. ON THE GROUND CABIN GALLEY COOLING FAN SOUND UNUSUALLY LOUD, ALMOST GRINDING SOUND. AFTER 5-10 MINUTES A BURNING ODOR WAS NOTICED IN THE CABIN. ONCE GALLEY POWE
- [SDR DXTA2011011904422](https://openairdocs.org/sdr/DXTA2011011904422), Jan 18, 2011: TRANSDUCER. MALFUNCTIONED. LT AND RT FADEC FAULTY EICAS MESSAGES CAME ON AT V1 (1 ST ONE) AND ABOUT 5 SECONDS LATER (2 ND ONE) ON TAKEOFF. ACFT WAS COLD SOAKED AT TEMP BELOW 0 DEG C FOR A
- [SDR DXTA200811393378](https://openairdocs.org/sdr/DXTA200811393378), Nov 29, 2008: FIRE WARNING. FALSE ACTIVATION. 15 MINS AFTER APU SHUTDOWN APU FIRE CAS MSG CAME ON IN FLIGHT. COULD NOT CANCEL MSG APU FIRE/OVERHEAT TEST NO GOOD. NO INDICATION OF FIRE VISIBLE ON GROUND. VIS
- [SDR DXTA2008120103378](https://openairdocs.org/sdr/DXTA2008120103378), Nov 29, 2008: WARNING LIGHT. FALSE ACTIVATION. 15 MINS AFTER APU SHUTDOWN APU FIRE CAS MSG CAME ON IN FLIGHT. NO INDICATION OF FIRE VISIBLE ON GROUND.
- [SDR DXTA200807203191](https://openairdocs.org/sdr/DXTA200807203191), Jul 20, 2008: FIRE LOOP. OUT OF POSITION. APU FIRE EICAS MSG. ILLUMINATED ON T/O AT ABOUT 90-100 KTS. EICAS MSG. WENT OUT ON ROLL OUT WITH NO INDICATION OF FIRE. APU EGT WAS NORMAL. POST FLT INSP REVEAL
- [SDR DXTA200803191](https://openairdocs.org/sdr/DXTA200803191), Jul 20, 2008: FIRE WARNING. FALSE ACTIVATION. APU FIRE EICAS MSG. ILLUMINATED ON T/O AT ABOUT 90-100 KTS. EICAS MSG. WENT OUT ON ROLL OUT WITH NO INDICATION OF FIRE. APU EGT WAS NORMAL. POST FLT INSPECTION 

## 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/N745QS/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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