# N120QS: 2022 Bombardier BD-700-1A11

- Status: Valid registration
- Airframe: [Bombardier BD-700-1A11](https://openairdocs.org/model/bombardier-bd-700-1a11) (registry code 1390022, 8 seats)
- Engine: [Rolls Deu BR700-710D521](https://openairdocs.org/engine/rolls-deu-br700-710d521) (registry code 54607)
- Data sheets: [TCDS T00003NY](https://openairdocs.org/tcds/T00003NY) (Bombardier Inc.), [TCDS E00057EN](https://openairdocs.org/tcds/E00057EN) (Rolls-Royce Deutschland Ltd & Co KG) (OpenAirDocs)
- Serial number: 60066
- Year built: 2022
- Type: Fixed wing multi engine
- Engine type: Turbo-fan
- Airworthiness: Standard, transport
- Airworthiness date: December 5, 2022
- Certificate issued: December 10, 2025
- Expires: December 31, 2032
- Mode S code: A05521
- Owner type: Co-owned, fractional ownership
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=120QS
- Page: https://openairdocs.org/aircraft/N120QS

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): 60 in force

### Matched by airframe (Bombardier BD-700-1A11)

- [AD 2026-15-09](https://openairdocs.org/ad/2026-15-09): Landing Gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 3, 2026
- [AD 2026-11-07](https://openairdocs.org/ad/2026-11-07): Equipment/furnishings · Bombardier BD-700-1A10, BD-700-1A11 and BD-700-2A12. Effective Jul 20, 2026
- [AD 2026-13-02](https://openairdocs.org/ad/2026-13-02): Navigation · Airbus Canada Limited Partnership 18, 49-46, 80-A and 555 more. Effective Jul 1, 2026
- [AD 2026-09-18](https://openairdocs.org/ad/2026-09-18): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 26, 2026
- [AD 2026-08-04](https://openairdocs.org/ad/2026-08-04): Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 29, 2026
- [AD 2025-14-51](https://openairdocs.org/ad/2025-14-51): Indicating/Recording System · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 4, 2026
- [AD 2025-12-01](https://openairdocs.org/ad/2025-12-01): Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 17, 2025
- [AD 2025-07-11](https://openairdocs.org/ad/2025-07-11): Hydraulic Power · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 2, 2025
- [AD 2025-09-04](https://openairdocs.org/ad/2025-09-04): Time Limits/Maintenance Checks · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 6, 2025
- [AD 2024-26-09](https://openairdocs.org/ad/2024-26-09): Time Limits/Maintenance Checks; Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 11, 2025
- [AD 2024-23-02](https://openairdocs.org/ad/2024-23-02): Landing Gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 15, 2025
- [AD 2024-23-08](https://openairdocs.org/ad/2024-23-08): Wings · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 6, 2025
- [AD 2024-07-09](https://openairdocs.org/ad/2024-07-09): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 17, 2024
- [AD 2024-03-08](https://openairdocs.org/ad/2024-03-08): Pneumatic · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 3, 2024
- [AD 2024-02-05](https://openairdocs.org/ad/2024-02-05): Wings · Bombardier BD-700-1A10 and BD-700-1A11. Effective Apr 9, 2024
- [AD 2023-24-08](https://openairdocs.org/ad/2023-24-08): Landing gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Feb 6, 2024
- [AD 2023-12-02](https://openairdocs.org/ad/2023-12-02): Time Limits/Maintenance Checks · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 7, 2023
- [AD 2023-13-15](https://openairdocs.org/ad/2023-13-15): Navigation · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 27, 2023
- [AD 2023-08-01](https://openairdocs.org/ad/2023-08-01): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 20, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2023-05-11](https://openairdocs.org/ad/2023-05-11): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 12, 2023
- [AD 2022-24-01](https://openairdocs.org/ad/2022-24-01): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 9, 2023
- [AD 2022-25-13](https://openairdocs.org/ad/2022-25-13): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 13, 2023
- [AD 2022-14-07](https://openairdocs.org/ad/2022-14-07): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 19, 2022
- [AD 2022-13-05](https://openairdocs.org/ad/2022-13-05): Navigation · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 11, 2022
- [AD 2022-11-17](https://openairdocs.org/ad/2022-11-17): Time Limits/Maintenance Checks · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 22, 2022
- [AD 2022-12-01](https://openairdocs.org/ad/2022-12-01): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 19, 2022
- [AD 2021-21-04](https://openairdocs.org/ad/2021-21-04): Powerplant · Bombardier BD-700-1A10 and BD-700-1A11. Effective Dec 8, 2021
- [AD 2021-08-11](https://openairdocs.org/ad/2021-08-11): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Apr 27, 2021
- [AD 2020-12-14](https://openairdocs.org/ad/2020-12-14): Electrical power · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 8, 2020
- [AD 2020-12-15](https://openairdocs.org/ad/2020-12-15): Pneumatic · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jul 24, 2020
- [AD 2020-05-27](https://openairdocs.org/ad/2020-05-27): Fuselage · Bombardier BD-700-1A10 and BD-700-1A11. Effective May 7, 2020
- [AD 2020-03-21](https://openairdocs.org/ad/2020-03-21): Landing gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 12, 2020
- [AD 2020-02-15](https://openairdocs.org/ad/2020-02-15): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Mar 12, 2020
- [AD 2019-12-02](https://openairdocs.org/ad/2019-12-02): Electrical Power · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 12, 2019
- [AD 2019-03-22](https://openairdocs.org/ad/2019-03-22): Landing gear · Bombardier BD-700-1A10 and BD-700-1A11. Effective Apr 15, 2019
- [AD 2018-25-07](https://openairdocs.org/ad/2018-25-07): Fuselage · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jan 15, 2019
- [AD 2018-22-08](https://openairdocs.org/ad/2018-22-08): Fire protection · Bombardier BD-700-1A10 and BD-700-1A11. Effective Dec 10, 2018
- [AD 2018-20-20](https://openairdocs.org/ad/2018-20-20): Flilght Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Nov 20, 2018
- [AD 2018-21-03](https://openairdocs.org/ad/2018-21-03): Fuselage · Bombardier BD-700-1A10 and BD-700-1A11. Effective Nov 19, 2018
- [AD 2018-09-15](https://openairdocs.org/ad/2018-09-15): Engine · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 15, 2018
- [AD 2017-22-14](https://openairdocs.org/ad/2017-22-14): Navigation · Bombardier BD-100-1A10 (Challenger 300), BD-500-1A10, BD-500-1A11 and 13 more. Effective Dec 20, 2017
- [AD 2017-19-11](https://openairdocs.org/ad/2017-19-11): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Oct 23, 2017
- [AD 2017-14-15](https://openairdocs.org/ad/2017-14-15): Flight controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 31, 2017
- [AD 2016-17-16](https://openairdocs.org/ad/2016-17-16): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Oct 5, 2016
- [AD 2016-15-06](https://openairdocs.org/ad/2016-15-06): Oxygen · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 8, 2016
- [AD 2016-15-03](https://openairdocs.org/ad/2016-15-03): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Aug 31, 2016
- [AD 2016-10-06](https://openairdocs.org/ad/2016-10-06): Navigation · Bombardier BD-700-1A10 and BD-700-1A11. Effective Jun 23, 2016
- [AD 2016-01-12](https://openairdocs.org/ad/2016-01-12): Doors · Bombardier BD-700-1A10 and BD-700-1A11. Effective Feb 25, 2016
- [AD 2015-17-05](https://openairdocs.org/ad/2015-17-05): Flight Controls · Bombardier BD-700-1A10 and BD-700-1A11. Effective Sep 29, 2015

### Matched by engine (Rolls Deu BR700-710D521)

- [AD 2022-26-02](https://openairdocs.org/ad/2022-26-02): Accessory Gearboxes · Rolls-Royce Deutschland BR700-710A1-10, BR700-710A2-20, BR700-710C4-11 and 1 more. Effective Jan 27, 2023

### 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 64: https://openairdocs.org/aircraft/N120QS/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 N120QS.

## FAA accident and incident reports

None matched to N120QS.

## Service difficulty reports (2)

As reported by operators and repair stations. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR DXTA2023091195140](https://openairdocs.org/sdr/DXTA2023091195140), Sep 10, 2023: UNKNOWN. UNKNOWN. WASTE DISPOSAL (TOILET): AFTER THE RT. ENGINE WAS STARTED A VERY STRONG ELECTRICAL BURNING ODOR WAS DETECTED IN THE AFT LAV AND ALSO THE AFT BAGGAGE COMPARTMENT
- [SDR DXTA2023021580550](https://openairdocs.org/sdr/DXTA2023021580550), Feb 15, 2023: NONE. NONE. R FADEC FAIL AMBER CAS: ON CLIMB OUT 36000 R FADEC FAULT CYAN ILLUMINATED 3 SECONDS LATER R FADEC FAIL ILLUMINATED ACCOMPANIED BY R ENGINE TCCV FAULT CYAN RAN C

## Service difficulty reports on N120QS not matched to an aircraft (17)

They name N120QS, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR DXTA2012112605190](https://openairdocs.org/sdr/DXTA2012112605190), Nov 23, 2012: DOOR. OUT OF ADJUST. RED LIGHT IN GEAR HANDLE WOULD NOT EXTINGUISH AFTER GEAR RETRACTION, TOWER NOTICED AND SAID IT APPEARS TO BE THE RT SIDE. GEAR WAS EXTENDED NORMALLY WITH A GEAR
- [SDR DXTA2012111205180](https://openairdocs.org/sdr/DXTA2012111205180), Nov 9, 2012: ACTUATOR. OUT OF ADJUST. RED GEAR HANDLE LIGHTS FAILED TO EXTINGUISH AFTER GEAR RETRACTION (GEAR DOOR UNSAFE NOT UP AND LOCKED INDICATION). RETURNED TO AIRPORT, LANDING GEAR EXTENTION W
- [SDR DXTA2012111205179](https://openairdocs.org/sdr/DXTA2012111205179), Nov 9, 2012: SWITCH. OUT OF ADJUST. RED GEAR HANDLE LIGHTS FAILED TO EXTINGUISH AFTER GEAR RETRACTION (GEAR DOOR UNSAFE NOT UP AND LOCKED INDICATION). RETURNED TO AIRPORT, LANDING GEAR EXTENTION W
- [SDR DXTA2012102205159](https://openairdocs.org/sdr/DXTA2012102205159), Oct 20, 2012: BRAKE ASSY. CONTAMINATED. AFTER BLOCK-IN, LEFT BRAKE SMOKING. DURING INSPECTION, LEFT TIRE AND WHEEL ASSY WAS EXTREMELY HOT AND A DISTINCT ODOR OF HOT BRAKES. LANDING WAS NORMAL WITH VER
- [SDR DXTA2012101105142](https://openairdocs.org/sdr/DXTA2012101105142), Oct 10, 2012: ACTUATOR. FAILED. AFTER TAKEOFF. SELECTED GEAR UP. GREEN LIGHTS WENT OUT, RED GEAR HANDLE LIGHT STAYED ON. ON LANDING, SELECTING GEAR DOWN, 3 GREEN LIGHTS ON AND RED LIGHT WENT O
- [SDR DXTA2012090405119](https://openairdocs.org/sdr/DXTA2012090405119), Sep 9, 2012: SPRING. FAILED. AFTER TAKEOFF WHEN GEAR HANDLE WAS RAISED, NOTICED RED IN TRANSIT LIGHT REMAINED ILLUMINATED AND ALL GREEN LANDING GEAR LIGHTS WERE OUT. TOWER REPORTED NOSE AND
- [SDR DXTA2012091005119](https://openairdocs.org/sdr/DXTA2012091005119), Sep 9, 2012: LANDING GEAR. MALFUNCTIONED. AFTER TAKEOFF, WHEN GEAR HANDLE WAS RAISED, NOTICED RED IN TRANSIT LIGHT REMAINED ILLUMINATED AND ALL GREEN LANDING GEAR LIGHTS WERE OUT. TOWER REPORTED NOSE AN
- [SDR DXTA2012040504944](https://openairdocs.org/sdr/DXTA2012040504944), Apr 4, 2012: BRAKE SYS. MALFUNCTIONED. BOTH PILOT AND COPILOT BRAKE PEDALS REQUIRE EXECESSIVE PRESSURE TO ACTUATE THE BRAKES. CHECKED BRAKE WEAR & FLUID LEVELS. NO DEFECTS NOTED. TAXIED ACFT AND PERF
- [SDR DXTA2010120304344](https://openairdocs.org/sdr/DXTA2010120304344), Dec 2, 2010: BRAKE SYS. MALFUNCTIONED. ON LANDING, WHEN APPLYING BRAKES, BOTH PEDALS WERE HARD AND THERE WAS NO BRAKING ACTION UNTIL AFTER THE ACFT SLOWED BELOW 60KNTS. BRAKES WORKED NORMAL WITH THE 
- [SDR DXTA2010081804197](https://openairdocs.org/sdr/DXTA2010081804197), Aug 17, 2010: ADC. INOPERATIVE. CO-PILOT AIR DATA INOP. REMOVED ADC AND INSTALLED AN OVERHAULED UNIT. OPS CHECK OF SYSTEM SHOWS NORMAL OPERATION. PERFORMED PITOT-STATIC. LEAK CHECKED - COMPLIE
- [SDR DXTA2009061503688](https://openairdocs.org/sdr/DXTA2009061503688), Jun 13, 2009: CONTROL BOX. MALFUNCTIONED. ON TAXI IN, DISCOVERED WHEEL BRAKES WERE NOT RESPONDING PROPERLY. FIRST 1 TO 2 INCHES OF BRAKE APPLICATION THERE IS NO RESPONSE, THEN BRAKES WERE STIFF & GRABBY
- [SDR DXTA200702700](https://openairdocs.org/sdr/DXTA200702700), Dec 20, 2007: BULB. BURNED OUT. LT MAIN GEAR DOWN AND LOCK INDICATION INOPERATIVE. REPLACED LT MAIN LANDING GEAR DOWN INDICATION BULB. OPS CHECK GOOD IAW HAWKER 400XP MM CH 32-60-00.
- [SDR DXTA200702261](https://openairdocs.org/sdr/DXTA200702261), Jun 13, 2007: UNKNOWN. UNKNOWN. WHILE IN A 3000FPM DESCENT, WE EXTENDED THE SPEEDBRAKES. AIRCRAFT ABRUPTLY ROLLED RT 12-15 DEGREES AND THEN JUST AS ABRUPTLY ROLLED LT AFTER APPROX 2 SECONDS. P
- [SDR DXTA200701922](https://openairdocs.org/sdr/DXTA200701922), Feb 8, 2007: INDICATOR. NO INDICATION. WHEN GEAR WAS PLACED IN DOWN POSITION. THE RT GREEN R DID NOT ILLUMINATE. OHMED OUT GEAR INDICATOR HARNESS NO DEFECTS WERE NOTED. ACCESSED CONNECTOR P272 IN R/H
- [SDR DXTA200601242](https://openairdocs.org/sdr/DXTA200601242), Feb 15, 2006: FLT CONTROLS. OUT OF POSITION. ON TAKEOFF WARNING HORN CAME ON ABORTED TAKEOFF AT 50 KNOTS FLIGHT CONTROLS APPEARED TO BE IN CORRECT POSITION. COMPLIED WITH TAKEOFF WARNING HORN CHECK IAW RAY
- [SDR DXTA200601183](https://openairdocs.org/sdr/DXTA200601183), Jan 5, 2006: POSITION SWITCH. MALFUNCTIONED. ON TAKEOFF KTEB GEAR WOULD NOT RETRACT, USED OVER RIDE. GEAR RETRACTED NORMAL. JACKED A/C, RETRACTED GEAR SEVERAL TIMES, NO DEFECTS NOTED. CHECKED LT LANDING GE
- [SDR DXTA200500952](https://openairdocs.org/sdr/DXTA200500952), Sep 5, 2005: POSITION SWITCH. INOPERATIVE. DURING CRUISE FLIGHT AT FL,360/.78 MACH THE LT DEPLOY LIGHT ILLUMINATED (THE DEPLOY ONLY-NO ARM OR UNLOCK.) DESCENDED AND PUSHED EMERGENCY STOW. THE BOTTOM PORT

## 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/N120QS/stcs.md

## Related

- Other Bombardier BD-700-1A11 aircraft: https://openairdocs.org/model/bombardier-bd-700-1a11/aircraft.md
- The Rolls Deu BR700-710D521 engine: https://openairdocs.org/engine/rolls-deu-br700-710d521.md

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