# N149QS: 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)
- Data sheets: [TCDS T00003NY](https://openairdocs.org/tcds/T00003NY) (Bombardier Inc.) (OpenAirDocs)
- Serial number: 60221
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Certificate issued: October 6, 2026
- Expires: October 31, 2033
- Mode S code: A0C58E
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=149QS
- Page: https://openairdocs.org/aircraft/N149QS

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): 59 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

### 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

All 63: https://openairdocs.org/aircraft/N149QS/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 N149QS.

## FAA accident and incident reports

None matched to N149QS.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N149QS not matched to an aircraft (21)

They name N149QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2012052404978](https://openairdocs.org/sdr/DXTA2012052404978), May 23, 2012: WIRE. BURNED. DURING APPROACH, CREW SMELLED ELECTRICAL SMOKE (NOT VISIBLE). ON LANDING, DISCOVERED "PWR FDR" 1/2A BREAKER (ON STBY PWR PANEL) POPPED. T/S & FOUND RCCB 8 & 107
- [SDR DXTA2012030604906](https://openairdocs.org/sdr/DXTA2012030604906), Mar 5, 2012: UPLOCK SWITCH. MALFUNCTIONED. ON GEAR RETRACTION, THE RED LIGHT IN THE GEAR HANDLE REMAINED ILLUMINATED. SOME UNUSUAL TURBULENCE WAS FELT DURING THE FLIGHT BUT DID NOT SEEM TO BE COMING FROM
- [SDR DXTA2011080104678](https://openairdocs.org/sdr/DXTA2011080104678), Jul 29, 2011: BRAKE. DRAGGING. ON TAKEOFF ROLL IT FELT LIKE BRAKES WERE DRAGGING. ABORTED THE TAKEOFF AND CHECKED THAT PARKING BRAKE WAS FULLY RELEASED AND PERFORMED AN ANTISKID CHECK. ON TAX
- [SDR DXTA2011051204579](https://openairdocs.org/sdr/DXTA2011051204579), May 12, 2011: MOTOR. FAILED. BLOWER AND FREON AIR SYS MAKES A NOTICEABLE GRINDING AND BUZZING SOUND ACCOMPANIED BY A FRICTION BURNING ODOR. IT IS MOST APPARENT AT THE AIR EXHAUST. THIS WORS
- [SDR DXTA201105120479](https://openairdocs.org/sdr/DXTA201105120479), May 12, 2011: A/C PACK. NOISY. BLOWER AND FREON AIR SYSTEM MAKES A NOTICABLE GRINDING/ BUZZING SOUND ACCOMPANIED BY A FRICTION/BURNING ODOR. IT IS MOST APPARENT AT THE AIR EXHAUST. THIS WORSE
- [SDR E81RJW304141](https://openairdocs.org/sdr/E81RJW304141), Feb 3, 2011: DOOR. OUT OF RIG. AFTER DEPARTURE, FLIGHT CREW NOTED RED WARNING LIGHT IN LANDING GEAR CONTROL HANDLE REMAINED ILLUMINATED AFTER LANDING GEAR RETRACTION. FLIGHT CREW RETURNED TO 
- [SDR DXTA2011020304448](https://openairdocs.org/sdr/DXTA2011020304448), Feb 3, 2011: DOOR. OUT OF RIG. AFTER TAKEOFF, GEAR HANDLE "RED" LIGHT WOULD NOT EXTINGUISH. REDUCED HYD PRESS TO 950 PSI IAW MM 32-00-00. FOUND NLG DOORS RIGGED TOO TIGHT. ADJUSTED DOORS IAW 
- [SDR DXTA2010122204371](https://openairdocs.org/sdr/DXTA2010122204371), Dec 20, 2010: LANDING GEAR. FAILED. ABORTED TAKEOFF, DUE TO LT MLG FAILURE AT 80KTS. ACCELERATION TO 80KTS APPEARED NORMAL UNTIL 80KTS, THEN ACCELERATION IMPAIRED & DIRECTIONAL CONTROL EFFECTED. I
- [SDR DXTA2010120604355](https://openairdocs.org/sdr/DXTA2010120604355), Dec 6, 2010: WARNING LIGHT. FALSE ACTIVATION. AFTER GEAR RETRACTION RED GEAR UNSAFE LIGHTS ON GEAR HANDLE REMAINED ILLUMINATED. DURING APPROACH GEAR EXTENSION WAS NORMAL AND RED UNSAFE LIGHTS EXTINGUISHED. 
- [SDR DXTA2010100104255](https://openairdocs.org/sdr/DXTA2010100104255), Sep 30, 2010: SERVO. FAILED. FLASH OF RUDDER BOOST FAIL ANNUNCIATOR AND YAW DAMP KICKED OFF SHORTLY AFTER TAKEOFF. 600-800 FT. TWICE DURING DESCENT, AUTOPILOT AND YAW DAMP KICKED OFF WITH G
- [SDR DXTA2010022203998](https://openairdocs.org/sdr/DXTA2010022203998), Feb 19, 2010: BRAKE. ODOR. BRAKE ODOR OCURRED IN FLIGHT AND AGAIN DURING TAXI IN. REMOVED WHEEL ASSY AND INSPECTED BRAKES. NO DISCRPANCYS NOTED. REINSTALLED WHEEL ASSY IAW MM CHP 32-40-00
- [SDR DXTA2010020403970](https://openairdocs.org/sdr/DXTA2010020403970), Feb 3, 2010: LANDING GEAR. FALSE INDICATION. ON TAKEOFF, WE PUT THE GEAR UP, THE 3 GREEN LIGHTS WENT OUT BUT THE RED HANDLE LIGHT REMAINED ON. PUT GEAR BACK DOWN AND IT OPERATED PROPERLY. PERFORMED 25 GEAR
- [SDR DXTA2009121103894](https://openairdocs.org/sdr/DXTA2009121103894), Dec 10, 2009: INDICATOR. MALFUNCTIONED. AFTER GEAR RETRACTION, ALL GREEN LIGHTS WENT OUT BUT RED LIGHTS IN HANDLE STAYED ON, EXTENDED GEAR ALL GREEN LIGHTS CAME ON AND RED LIGHTS IN HANDLE WENT OUT. C
- [SDR DXTA2009113003872](https://openairdocs.org/sdr/DXTA2009113003872), Nov 29, 2009: INDICATOR. NO INDICATION. WHEN ON APPROACH, THE LT MLG LIGHT WOULD NOT ILLUMINATE. IAW ABNORMAL PROCEDURES, TESTED THE LIGHT AND IT TESTED NORMALLY. THUS THE CHECKLIST DIRECTED US TO LAN
- [SDR DXTA2009110603850](https://openairdocs.org/sdr/DXTA2009110603850), Nov 5, 2009: UNKNOWN. VIBRATION. AFTER COMPLETEING A MISSED APPROACH AND RETRACTING THE GEAR, FLAPS AND LANDING LIGHTS, WE EXPERINCIED A PERODIC VIBRATION THAT WOULD LAST 5-15 SEC AND WAS AUDIB
- [SDR DXTA200802798](https://openairdocs.org/sdr/DXTA200802798), Jan 25, 2008: BELLCRANK. OUT OF ADJUST. NR2 ENGINE WOULD NOT MAINTAIN TAKEOFF TARGET N1 OF 96.9. INITIALLY NR2 N1 INDICATED 96.9 WITH POWER LEVER AT FULL FWD BUT IMMEDIATELY DROPPED TO AND MAINTAINED 
- [SDR DXTA200702246](https://openairdocs.org/sdr/DXTA200702246), Jun 6, 2007: DOOR. STUCK. MAIN CABIN DOOR WOULD NOT OPEN PRIOR TO DEPLANING AFTER A 1.2 HOUR FLIGHT. PASSENGERS AND CREW DEPLANED THROUGH THE EMERGENCY EXIT ESCAPE HATCH. [06-15-07] INSP
- [SDR DXTA200701998](https://openairdocs.org/sdr/DXTA200701998), Mar 4, 2007: ENGINE. SURGES. AFTER LEVEL OFF FOLLOWING AN UNRESTRICTED CLIMB TO FL 380, LT ENGINE BEGAN TO SURGE +- 2 PERCENT N1 (APPROX). ENGINE SYNC-ON. EGT, N2 AND FUEL FLOW WERE ALSO FL
- [SDR DXTA200701855](https://openairdocs.org/sdr/DXTA200701855), Jan 14, 2007: RESERVOIR. UNDERSERVICED. ON TAXI OUT, RT BRAKE PEDAL, CAPT, PRESSED TO FLOOR. NO PRESSURE OR BRAKING ACTION. LT PEDAL HAD PRESSURE BUT ALSO NO BRAKING ACTION. APPLIED EMER BRAKE TO STOP
- [SDR DXTA200701843](https://openairdocs.org/sdr/DXTA200701843), Jan 9, 2007: BRAKE ASSY. MALFUNCTIONED. RT BRAKE ON LT SEAT PILOT INOPERATIVE. THE BRAKE WORKS INTERMITTENTLY. BRAKE ON RT PANEL GOES TO THE FLOOR THEN WILL START TO WORK AGAIN FOR A SHORT TIME. RT SE
- [SDR DXTA200601629](https://openairdocs.org/sdr/DXTA200601629), Oct 3, 2006: CONNECTOR. DEFECTIVE. FOUND STRONG BURNING ODOR ON CLIMB-OUT. SUSPECTED FREON AIR AS PROBLEM. TURNED OFF FREON AIR AND ODOR WENT AWAY. REPLACED DEFECTIVE GALLEY CONNECTOR IAW HAWKER 

## 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/N149QS/stcs.md

## Related

- Other Bombardier BD-700-1A11 aircraft: https://openairdocs.org/model/bombardier-bd-700-1a11/aircraft.md

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