# Canadair CL-600-2A12

- Type: Aircraft model (FAA registry)
- Registry code: 1900304
- Manufacturer (registry): CANADAIR LTD
- Model: CL-600-2A12
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-fan
- Seats: 22
- Weight class: 20,000 lb and over
- Certification: Type certificated
- Data sheet: [TCDS A21EA](https://openairdocs.org/tcds/A21EA) (OpenAirDocs)
- Holder: Bombardier Inc.
- Registered aircraft: 19
- Page: https://openairdocs.org/model/canadair-cl-600-2a12

Model codes come from the FAA registry's reference file. ADs are matched to them by model name and maker.

## ADs that may apply (OpenAirDocs)

Matched to this model by model name and maker. Each AD's applicability may narrow it by serial number, part number or equipment.

- [AD 2026-14-09](https://openairdocs.org/ad/2026-14-09): Time Limits/Maintenance Checks · Bombardier CL-600-1A11 (600), CL-600-2B16 (601-3A Variant), CL-600-2B16 (601-3R Variant) and 2 more. Effective Aug 18, 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 2026-07-01](https://openairdocs.org/ad/2026-07-01): Landing gear · Bombardier CL-600-1A11 (600), CL-600-2A12 (601), CL-600-2B16 (601-3A Variant) and 2 more. Effective May 8, 2026
- [AD 2025-24-11](https://openairdocs.org/ad/2025-24-11): Auxiliary Power · Bombardier CL-600-2A12 (601), CL-600-2B16 (601-3A Variant), CL-600-2B16 (601-3R Variant) and 1 more. Effective Jan 16, 2026
- [AD 2025-07-09](https://openairdocs.org/ad/2025-07-09): Oxygen · Bombardier CL-600-1A11 (600), CL-600-2A12 (601), CL-600-2B16 (601-3A Variant) and 2 more. Effective Jul 2, 2025
- [AD 2023-17-06](https://openairdocs.org/ad/2023-17-06): Flight Controls · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Oct 19, 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 2023-06-04](https://openairdocs.org/ad/2023-06-04): Oxygen System · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective May 18, 2023
- [AD 2023-06-02](https://openairdocs.org/ad/2023-06-02): Equipment/furnishings · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective May 18, 2023
- [AD 2022-20-05](https://openairdocs.org/ad/2022-20-05): Flight Controls · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Nov 25, 2022
- [AD 2022-12-13](https://openairdocs.org/ad/2022-12-13): Auto flight · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 1 more. Effective Oct 19, 2022
- [AD 2022-10-10](https://openairdocs.org/ad/2022-10-10): Ice and Rain Protection · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Jul 5, 2022
- [AD 2022-09-01](https://openairdocs.org/ad/2022-09-01): Ice and Rain Protection, Potable Water System · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective May 31, 2022
- [AD 2021-25-13](https://openairdocs.org/ad/2021-25-13): Time Limits/Maintenance Checks · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Feb 15, 2022
- [AD 2021-13-12](https://openairdocs.org/ad/2021-13-12): Time Limits/Maintenance Checks · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Sep 9, 2021
- [AD 2019-21-03](https://openairdocs.org/ad/2019-21-03): Navigation · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 1 more. Effective Dec 18, 2019
- [AD 2019-10-01](https://openairdocs.org/ad/2019-10-01): Wings · Bombardier CL-600-2A12 (CL-601). Effective Jul 18, 2019
- [AD 2019-08-08](https://openairdocs.org/ad/2019-08-08): Hydraulic power · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Jun 27, 2019
- [AD 2018-17-02](https://openairdocs.org/ad/2018-17-02): Flight controls · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Sep 19, 2018
- [AD 2018-09-17](https://openairdocs.org/ad/2018-09-17): Flight Controls · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Jun 25, 2018
- [AD 2017-23-09](https://openairdocs.org/ad/2017-23-09): Periodic inspections · Bombardier CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and 1 more. Effective Dec 26, 2017
- [AD 2017-20-11](https://openairdocs.org/ad/2017-20-11): Fuselage · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 1 more. Effective Nov 15, 2017
- [AD 2017-19-06](https://openairdocs.org/ad/2017-19-06): Wings · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Oct 27, 2017
- [AD 2016-20-09](https://openairdocs.org/ad/2016-20-09): Fuel · Bombardier CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and 1 more. Effective Jan 9, 2017
- [AD 2016-21-06](https://openairdocs.org/ad/2016-21-06): Wings · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 1 more. Effective Dec 19, 2016
- [AD 2015-25-05](https://openairdocs.org/ad/2015-25-05): Electrical Power · Bombardier CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and 1 more. Effective Jan 28, 2016
- [AD 2015-07-02](https://openairdocs.org/ad/2015-07-02): Wings · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Jun 4, 2015
- [AD 2014-15-13](https://openairdocs.org/ad/2014-15-13): Landing Gear · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Sep 25, 2014
- [AD 2014-03-17](https://openairdocs.org/ad/2014-03-17): Wings · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Mar 6, 2014
- [AD 2013-05-06](https://openairdocs.org/ad/2013-05-06): Powerplant · Bombardier CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and 1 more. Effective Apr 24, 2013
- [AD 2013-03-08](https://openairdocs.org/ad/2013-03-08): Periodic Inspections · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Mar 19, 2013
- [AD 2011-21-08](https://openairdocs.org/ad/2011-21-08): Equipment/Furnishings · ATR - GIE Avions de Transport Régional ATR42-200, ATR42-300, ATR42-320 and 202 more. Effective Nov 23, 2011
- [AD 2011-09-09](https://openairdocs.org/ad/2011-09-09): Ice and Rain Protection and Pneumatic, respectively · Bombardier CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and 1 more. Effective Aug 19, 2011
- [AD 2011-01-09](https://openairdocs.org/ad/2011-01-09): Oxygen · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 290 more. Effective Feb 9, 2011
- [AD 2010-10-26](https://openairdocs.org/ad/2010-10-26): Landing Gear · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Jun 25, 2010
- [AD 2009-06-05 R1](https://openairdocs.org/ad/2009-06-05-R1): Ice and Rain Protection · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Apr 1, 2010
- [AD 2009-24-18](https://openairdocs.org/ad/2009-24-18): Engine controls. · Bombardier CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A), CL-600-2B16 (CL-601-3R) and 1 more. Effective Jan 8, 2010
- [AD 2009-23-09](https://openairdocs.org/ad/2009-23-09): Electrical power · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601) and CL-600-2B16 (CL-601-3A). Effective Dec 14, 2009
- [AD 2009-14-03](https://openairdocs.org/ad/2009-14-03): Flight Controls · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Aug 12, 2009
- [AD 2008-21-09](https://openairdocs.org/ad/2008-21-09): Cold weather operation limitations · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 4 more. Effective Oct 31, 2008
- [AD 2006-25-16](https://openairdocs.org/ad/2006-25-16): Corrosion prevention and control program (CPCP) · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 1 more. Effective Jan 19, 2007
- [AD 2006-02-04](https://openairdocs.org/ad/2006-02-04): Rudder balance spring assembly · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Feb 24, 2006
- [AD 2005-26-04](https://openairdocs.org/ad/2005-26-04): Lower gimbal pin · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 33 more. Effective Jan 25, 2006
- [AD 2005-11-04](https://openairdocs.org/ad/2005-11-04): Microphone jack assemblies. · Dual Baker M1045 cockpit audio systems (Textron STC SA4900SW). Effective May 27, 2005
- [AD 2004-25-19](https://openairdocs.org/ad/2004-25-19): Airplane flight manual · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Jan 4, 2005
- [AD 2004-09-37](https://openairdocs.org/ad/2004-09-37): Inboard flap actuator beam · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Jun 11, 2004
- [AD 97-24-02 R1](https://openairdocs.org/ad/97-24-02-R1): Pressure bulkhead · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Feb 13, 2004
- [AD 2003-22-12](https://openairdocs.org/ad/2003-22-12): Electronic flight instrumetn system (EFIS) · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Dec 12, 2003
- [AD 2002-20-09](https://openairdocs.org/ad/2002-20-09): Adaptive flight display units · Bombardier CL-600-2A12 (CL-601), 525, 525A and 5 more. Effective Nov 12, 2002
- [AD 2001-22-14](https://openairdocs.org/ad/2001-22-14): Fire Extinguishing System Bottle Cartridges · Airbus A300 B2-1A, A300 B2-1C, A300 B2-203 and 105 more. Effective Dec 10, 2001

Historical (superseded or no longer in force):

- [AD 2025-17-12](https://openairdocs.org/ad/2025-17-12) (historical): Time Limits/Maintenance Checks · Bombardier CL-600-1A11 (600), CL-600-2A12 (601), CL-600-2B16 (601-3A Variant) and 2 more. Effective Oct 31, 2025
- [AD 2020-19-13](https://openairdocs.org/ad/2020-19-13) (historical): Oxygen · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Nov 3, 2020
- [AD 2015-02-23](https://openairdocs.org/ad/2015-02-23) (historical): Wings · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 1 more. Effective Feb 18, 2015
- [AD 2010-14-05](https://openairdocs.org/ad/2010-14-05) (historical): Hydraulic power · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Aug 5, 2010
- [AD 2009-06-05](https://openairdocs.org/ad/2009-06-05) (historical): Wing anti-ice piccolo · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Apr 28, 2009
- [AD 2008-08-06](https://openairdocs.org/ad/2008-08-06) (historical): Airplane flight manuals (AFMs) · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 4 more. Effective Apr 21, 2008
- [AD 2007-14-02](https://openairdocs.org/ad/2007-14-02) (historical): Nose landing gear (NLG) · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Aug 16, 2007
- [AD 2005-15-04](https://openairdocs.org/ad/2005-15-04) (historical): Landing gear parts · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Aug 30, 2005
- [AD 2005-04-07](https://openairdocs.org/ad/2005-04-07) (historical): Airplane Flight Manuals (AFM) - Cold Weather Operations · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 4 more. Effective Feb 22, 2005
- [AD 2003-08-12](https://openairdocs.org/ad/2003-08-12) (historical): Flap Vane Bracket and Vane Actuator Beam of Wing Flap Systems · Bombardier Aerospace CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective May 8, 2003
- [AD 97-24-02](https://openairdocs.org/ad/97-24-02) (historical): Underfloor Pressure Bulkhead of Fuselage · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Dec 3, 1997

All 93: https://openairdocs.org/model/canadair-cl-600-2a12/ads.md

## Information bulletins (advisory) (6)

- [SAIB AIR-21-15R1](https://openairdocs.org/saib/AIR-21-15R1): Navigation System. Issued Sep 16, 2021
- [SAIB AIR-21-15](https://openairdocs.org/saib/AIR-21-15) (historical): Navigation System. Issued Aug 26, 2021
- [SAIB NM-20-03](https://openairdocs.org/saib/NM-20-03): Landing Gear: Brake Control Valve. Issued Mar 18, 2020
- [SAIB NM-11-51](https://openairdocs.org/saib/NM-11-51): Ice and Rain Protection: Wing Anti-Ice System. Issued Aug 30, 2011
- [SAIB NM-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010
- [SAIB NE-03-28](https://openairdocs.org/saib/NE-03-28): . Issued Mar 10, 2003

## Registered aircraft (19)

- [N163JR](https://openairdocs.org/aircraft/N163JR): [Dodson International Parts Inc](https://openairdocs.org/faa-owner/DODSON%20INTERNATIONAL%20PARTS%20INC), [Rantoul, KS](https://openairdocs.org/faa-place/KS/Rantoul), S/N 3057
- [N211LM](https://openairdocs.org/aircraft/N211LM): [Park Avenue Aircraft Trust LLC Trustee](https://openairdocs.org/faa-owner/PARK%20AVENUE%20AIRCRAFT%20TRUST%20LLC%20TRUSTEE), [Dover, DE](https://openairdocs.org/faa-place/DE/Dover), built 1984, S/N 3024
- [N213TS](https://openairdocs.org/aircraft/N213TS): [Bank Of Utah Trustee](https://openairdocs.org/faa-owner/BANK%20OF%20UTAH%20TRUSTEE), [Salt Lake City, UT](https://openairdocs.org/faa-place/UT/Salt%20Lake%20City), built 1983, S/N 3013
- [N304CT](https://openairdocs.org/aircraft/N304CT): [Adams Aviation Services Inc Trustee](https://openairdocs.org/faa-owner/ADAMS%20AVIATION%20SERVICES%20INC%20TRUSTEE), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), built 1985, S/N 3044
- [N349CR](https://openairdocs.org/aircraft/N349CR): [Aviation Resource Group Inc](https://openairdocs.org/faa-owner/AVIATION%20RESOURCE%20GROUP%20INC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale), S/N 3049
- [N356CR](https://openairdocs.org/aircraft/N356CR): [Aviation Resource Group Inc](https://openairdocs.org/faa-owner/AVIATION%20RESOURCE%20GROUP%20INC), [Fort Lauderdale, FL](https://openairdocs.org/faa-place/FL/Fort%20Lauderdale), S/N 3056
- [N418PP](https://openairdocs.org/aircraft/N418PP): [Granger J Weldon](https://openairdocs.org/faa-owner/GRANGER%20J%20WELDON), [Houston, TX](https://openairdocs.org/faa-place/TX/Houston), built 1985, S/N 3041
- [N45WL](https://openairdocs.org/aircraft/N45WL): [Tvpx Aircraft Solutions Inc Trustee](https://openairdocs.org/faa-owner/TVPX%20AIRCRAFT%20SOLUTIONS%20INC%20TRUSTEE), [North Salt Lake, UT](https://openairdocs.org/faa-place/UT/North%20Salt%20Lake), S/N 3004
- [N600GA](https://openairdocs.org/aircraft/N600GA): [601 Holdings LLC](https://openairdocs.org/faa-owner/601%20HOLDINGS%20LLC), [Las Vegas, NV](https://openairdocs.org/faa-place/NV/Las%20Vegas), built 1985, S/N 3046
- [N601H](https://openairdocs.org/aircraft/N601H): [Gug LLC](https://openairdocs.org/faa-owner/GUG%20LLC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 3061
- [N601JG](https://openairdocs.org/aircraft/N601JG): [Challenger Aircraft Charters LLC](https://openairdocs.org/faa-owner/CHALLENGER%20AIRCRAFT%20CHARTERS%20LLC), [Newport Beach, CA](https://openairdocs.org/faa-place/CA/Newport%20Beach), built 1983, S/N 3006
- [N601RC](https://openairdocs.org/aircraft/N601RC): [Raytheon Co](https://openairdocs.org/faa-owner/RAYTHEON%20CO), [Tucson, AZ](https://openairdocs.org/faa-place/AZ/Tucson), built 1986, S/N 3055
- [N624EM](https://openairdocs.org/aircraft/N624EM): [Global Aircraft Trust Inc Trustee](https://openairdocs.org/faa-owner/GLOBAL%20AIRCRAFT%20TRUST%20INC%20TRUSTEE), [Cheyenne, WY](https://openairdocs.org/faa-place/WY/Cheyenne), S/N 3039
- [N657GF](https://openairdocs.org/aircraft/N657GF): [Challenger 601 - 3045 Inc](https://openairdocs.org/faa-owner/CHALLENGER%20601%20-%203045%20INC), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington), S/N 3045
- [N773CL](https://openairdocs.org/aircraft/N773CL): [Pollard Spares LLC](https://openairdocs.org/faa-owner/POLLARD%20SPARES%20LLC), [Roanoke, TX](https://openairdocs.org/faa-place/TX/Roanoke), built 1984, S/N 3032
- [N807MM](https://openairdocs.org/aircraft/N807MM): [Pollard Spares LLC](https://openairdocs.org/faa-owner/POLLARD%20SPARES%20LLC), [Fort Worth, TX](https://openairdocs.org/faa-place/TX/Fort%20Worth), built 1983, S/N 3014
- [N824DH](https://openairdocs.org/aircraft/N824DH): [Pollard Spares LLC](https://openairdocs.org/faa-owner/POLLARD%20SPARES%20LLC), [Roanoke, TX](https://openairdocs.org/faa-place/TX/Roanoke), built 1985, S/N 3047
- [N893TA](https://openairdocs.org/aircraft/N893TA): [Sta Aviation Management](https://openairdocs.org/faa-owner/STA%20AVIATION%20MANAGEMENT), [New York City, NY](https://openairdocs.org/faa-place/NY/New%20York%20City), built 1983, S/N 3016
- [N951RM](https://openairdocs.org/aircraft/N951RM): [Siilats Keith](https://openairdocs.org/faa-owner/SIILATS%20KEITH), [New York, NY](https://openairdocs.org/faa-place/NY/New%20York), S/N 3042

## NTSB investigations (4)

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 DCA18WA029](https://openairdocs.org/ntsb/DCA18WA029), Dec 4, 2017: Canadair CL 600 2A12 (N45WL), Caracas, Venezuela, substantial damage
- [NTSB CEN12IA662](https://openairdocs.org/ntsb/CEN12IA662), Sep 21, 2012: Canadair CL-600 Challenger (N125PS), Denver, CO, incident, no damage. Probable cause: The internal failure of the galley heater mat’s thermostat, which resulted in an overheat condition.
- [NTSB DEN05MA029](https://openairdocs.org/ntsb/DEN05MA029), Nov 28, 2004: Canadair CL-600-2A12 (N873G), Montrose, CO, destroyed, 3 fatal. Probable cause: the flight crew's failure to ensure that the airplane’s wings were free of ice or snow contamination that accumulated while the airplane was on the ground, which resulted in an attempted takeoff with…
- [NTSB SEA88IA028](https://openairdocs.org/ntsb/SEA88IA028), Dec 6, 1987: Canadair CL600-2A12 (N125PS), Twentynine Plms, CA, incident, no damage

## FAA accident and incident reports (8)

From the FAA Accident/Incident Data System. Reports are matched to registry aircraft by N-number and event date, checked against the reported make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [Incident 20200226002199I](https://openairdocs.org/incident/20200226002199I), Feb 26, 2020: Canadair Ltd CL-600-2A12 (N45WL), Minor damage. On feb 26, 2020, approximately 0940 local time, a challenger CL-601 registered as N45WL was enroute from nas to fll at level 200 when the left hand front…
- [Incident 20120921024269I](https://openairdocs.org/incident/20120921024269I), Sep 21, 2012: Canadair Ltd CL-600-2A12 (N125PS), Denver, CO, No damage. On 9/21/2012 at approximately 1430 hrs. MDT, N125PS, a Canadair Ltd. Model CL-600-2A12 challenger aircraft sustained no damage after making an emergency…
- [Incident 20080324013229I](https://openairdocs.org/incident/20080324013229I), Mar 24, 2008: Cndair CL6002A12 (N213TS), Grand Junction, CO, Minor damage. (-23) After take-off from kgjt the aircraft turned to its crosswind and at approximately 2000 feet above ground level (AGL) the pilots heard a loud bang. The…
- [Accident 20041128031429A](https://openairdocs.org/incident/20041128031429A), Nov 28, 2004: Cndair CL6002A12 (N873G), Montrose, CO, Destroyed, 3 fatal. (-23) On November 28, 2004 at 0955 MST, N873G, a Canadair ltd CL-600-2A12 owned by hop a jet and operated by air castle worldwide executive jet charter was…
- [Incident 19991126034669I](https://openairdocs.org/incident/19991126034669I), Nov 26, 1999: Cndair CL6002A12 (N873G), Palm Springs, CA, Minor damage. (-23) The pilot reported that landing at Palm Springs, California airport was normal, but upon applying thrust reversers and brakes, there was no indication of…
- [Incident 19901127062749I](https://openairdocs.org/incident/19901127062749I), Nov 27, 1990: Cndair CL6002A12 (N374G), New Orleans, LA, Minor damage. Left engine fire warning. Secured engine and landed. Combustion and burner cams damaged.
- [Incident 19891022056259I](https://openairdocs.org/incident/19891022056259I), Oct 22, 1989: Cndair CL6002A12 (N125PS), Santa Ana, CA, Minor damage. During engine start a jet blast caused minor damage to a parked aircraft. Pilot taxied away and departed.
- [Incident 19871206075519I](https://openairdocs.org/incident/19871206075519I), Dec 6, 1987: Cndair CL6002A12 (N125PS), Twenty Nine Pal, CA. Dutch roll at FL330 due to yaw damper problem caused by leaky galley water filter. Turned off autopilot. Landed ok.

## Service difficulty reports (78, newest 50)

As reported by operators and repair stations, by the model named in the report.

- [SDR 2021FA0000132](https://openairdocs.org/sdr/2021FA0000132), Feb 19, 2021: FLAP TRACK. BINDING. FAILURE OF THE FLAPS AT 10 DEGREES. CORRECTIVE ACTION WAS LUBRICATION OF THE FLAP ACTUATORS IN ACCORDANCE WITH BOMBARDIER MAINTENANCE MANUALS FOLLOWED BY AN OPE
- [SDR MXIA201902084](https://openairdocs.org/sdr/MXIA201902084), Feb 7, 2019: SWITCH. CRACKED. DURING APPROACH, GEAR WAS SELECTED DOWN. NOSE GEAR GREEN LIGHT DID NOT COME ON & NOSE DOOR REMAINED OPEN. AS PER THE CHECKLIST THE GEAR WAS SELECTED UP, THE MAI
- [SDR 2017FA0000234](https://openairdocs.org/sdr/2017FA0000234), May 25, 2017: TIRE. BULGED. PRE-FLIGHT WALK AROUND REVEALED A SMALL BULGE IN THE NR 2 MAIN TIRE. THE BULGE WAS ONLY EVIDENT WHEN THAT SPECIFIC AREA OF THE TIRE WAS ON THE BOTTOM. THE BULGE
- [SDR 4DUA20170101](https://openairdocs.org/sdr/4DUA20170101), Jan 26, 2017: FLAP SYSTEM. FAILED. DURING THE FINAL APPROACH, A FLAPS FAIL LIGHT WHEN THE FLAPS WERE PLACED IN THE 45 DEGREE POSITION. CONTINUED TO AVIATE AND GET THE AIRCRAFT ON THE GROUND. REPO
- [SDR 2016FA0000582](https://openairdocs.org/sdr/2016FA0000582), Nov 28, 2016: DIMMER. MELTED. FLIGHT CREW REPORTED A PORTION OF THE PILOTS INSTRUMENTATION BACK LIGHTING INOPERATIVE, TECHNICIAN REPLACED FAULTY INCANDESCENT LAMP DIMMER, VISUALLY INSPECTING
- [SDR 2016FA0000247](https://openairdocs.org/sdr/2016FA0000247), May 17, 2016: TIRE. FAILED. RIGHT MAIN INBD TIRE HAS A PORTION OF THE TREAD THAT SEPARATED ON LANDING. NEW TIRE WAS INSTALLED AT WHEEL ASSY O/H.
- [SDR 1KSA2015FA0000513](https://openairdocs.org/sdr/1KSA2015FA0000513), Oct 19, 2015: SKIN. CORRODED. DURING ROUTINE MAINTENANCE FOUND CORROSION UNDER VHF ANTENNA AT FS 360, BL0 AND UNDER TRANSPONDER ANTENNA, FS 386, LBL4.
- [SDR LOMA2015FA0000280](https://openairdocs.org/sdr/LOMA2015FA0000280), Jun 13, 2015: WARNING LIGHT. ILLUMINATED. RIGHT FUSELAGE BLEED WARNING CAME ON.
- [SDR 3BOR20150605001](https://openairdocs.org/sdr/3BOR20150605001), Jun 5, 2015: WIRE. MELTED. ELECTRICAL POWER WAS LOST DURING CRUISE FLIGHT. ACFT MADE AN UNSCHEDULED LANDING. VISUAL INSPECTION FOUND SEVERAL WIRES TO BE MELTED, SINGED AND/OR HEAT STRESSE
- [SDR LOMA2014FA0000687](https://openairdocs.org/sdr/LOMA2014FA0000687), Dec 4, 2014: LOOP. DEFECTIVE. RIGHT 10TH STAGE BLEED WARNING LIGHT CAME ON DURING DECENT. LANDED FOR REPAIR. REPLACED RT 10TH STAGE BLEED AIR WARNING LOOP A ELEMENT.
- [SDR LOMA2014FA0000688](https://openairdocs.org/sdr/LOMA2014FA0000688), Nov 25, 2014: VALVE. LEAKING. RIGHT 10TH STAGE WARNING LIGHT CAM ON DURING DECENT.
- [SDR LOMA2015F00009](https://openairdocs.org/sdr/LOMA2015F00009), Nov 18, 2014: SHUTOFF VALVE. LEAKING. RIGHT 10TH STAGE BLEED AIR WARNING ILLUMINATED. DIVERTED FOR REPAIR. REPLACED 10TH AND 14TH STAGE BLEED AIR SHUTOFF VALVES.
- [SDR CA140606002](https://openairdocs.org/sdr/CA140606002), Jun 5, 2014: CONTROL CABLE. FAILED. (CAN) DURING AN 60 MONTH INSPECTION. THE TECH FOUND BY VISUAL CHECK UP, WHEN HE OPEN THE PANEL IN THE VERTICAL STABILIZER RT SIDE.
- [SDR LOMA2014042500279](https://openairdocs.org/sdr/LOMA2014042500279), Apr 22, 2014: DETECTION SYS. FALSE ACTIVATION. RIGHT 10TH STAGE DUCT FAIL LIGHT ILLUMINATED DURING FLIGHT. TROUBLESHOT AND FOUND NO BLEED AIR LEAKS FROM RT 10TH STAGE MANIFOLD. FALSE INDICATION. REPLACED ALL
- [SDR BQVA20130507001](https://openairdocs.org/sdr/BQVA20130507001), May 3, 2013: SUPPORT ANGLE. CORRODED. CABIN DOOR WAS REMOVED AND SENT TO REPAIR FACILITY FOR COMPLIANCE OF BOMBARDIER SERVICE BULLETIN 601-0613 R1. THE FOLLOWING ITEMS WERE FOUND WITH CORROSION DURI
- [SDR 2012F00197](https://openairdocs.org/sdr/2012F00197), Sep 21, 2012: WATER HEATER. SHORTED. ENROUTE, CABIN ATTENDANT DETECTED AND SAW SMOKE COMING FROM THE GALLEY AREA. CONFIRMED LOCATION OF SMOKE AND PULLED ALL CIRCUIT BREAKERS TO GALLEY AND CAPTAIN S
- [SDR WWQA201209240001](https://openairdocs.org/sdr/WWQA201209240001), Sep 21, 2012: WATER HEATER. SHORTED. WHILE ENROUTE, THE CABIN ATTENDANT DETECTED AND SAW SMOKE COMING FROM THE GALLEY AREA. CAPTAIN HAD THE F/O GO BACK TO VERIFY & HELP LOCATE WHERE THE SMOKE WAS C
- [SDR 2012FA0000203](https://openairdocs.org/sdr/2012FA0000203), Feb 14, 2012: CONTROLLER. FAILED. AIRCRAFT ON RAMP, APU WAS SHUTDOWN AFTER RUNS AND ADG AUTOMATICALLY DEPLOYED. THIS OPERATION SHOULD NOT HAVE HAPPENED UNLESS ACFT IS IN THE AIR. TROUBLESHOOTING
- [SDR CA111102004](https://openairdocs.org/sdr/CA111102004), Nov 1, 2011: SEAL. BENT. (CAN) HARD CHAFING CONDITION AND DAMAGED MOVING PART HAVE BEEN FOUND BY MX PERSONNEL WHILE PERFORMING POST FLIGHT CHECK FOLLOWING ACFT FIRST FLIGHT. RT AILERON 
- [SDR 2011FA0000384](https://openairdocs.org/sdr/2011FA0000384), Jun 17, 2011: SELECTOR. FAILED. LANDING GEAR DID NOT EXTEND NORMALLY. ALTERNATE EXTENSION USED SUCCESSFULLY FOR DOWN AND LOCKED.
- [SDR CA110615007](https://openairdocs.org/sdr/CA110615007), Jun 11, 2011: GPS. MALFUNCTIONED. APPROXIMATELY ONE HOUR AFTER TAKEOFF AND ENROUTE, CREW REPORTED BACK TO MX THAT BOTH GPS RECEIVERS HAD LOST THE SATELITE FIX AND HAD STARTED TO REACQUIRE. CREW 
- [SDR CA110418006](https://openairdocs.org/sdr/CA110418006), Apr 18, 2011: TUBE. CHAFED. (CAN) MOTIVE FLOW SENSE LINE, RT, T/O MAIN EJECTOR PRESSURE SWITCH CHAFED THROUGH UNDER AND BY CLAMP, PN 417-4. THE ANTI-CHAFE MATERIAL WAS IN PLACE ON THE CLAM
- [SDR CA120426011](https://openairdocs.org/sdr/CA120426011), Jan 12, 2011: PIN. MISINSTALLED. (CAN) THROUGH AN SRPSA, 58446, REPORTED DAMAGE TO THE ANTI-ROTATION TAB OF SIDE STAY FITTING 601-10374-1/-2. AFTER INVESTIGATION, SHAFT, 600-10237-5 WAS FOUND I
- [SDR 2011F00005](https://openairdocs.org/sdr/2011F00005), Dec 23, 2010: TIRE. FAILED. DURING LANDING, THE NR 2 TIRE TREAD SEPARATED FROM THE TIRE. THE TIRE STAYED INFLATED. WHEN THE TREAD SEPARATED, IT CUT THE NR 2 ANTI-SKID HARNESS IN HALF AND D
- [SDR 2010FA0000201](https://openairdocs.org/sdr/2010FA0000201), Feb 5, 2010: FRAME. CRACKED. FWD FUSELAGE FRAME AT FS235 ABOVE FLOOR, PILOTS AND COPILOTS SIDE, FOUND CRACKED. DURING 240 MONTH INSP.
- [SDR 2010FA0000200](https://openairdocs.org/sdr/2010FA0000200), Feb 4, 2010: FRAME. CRACKED. FWD FUSELAGE FRAME AT FS 235 ABOVE FLOOR, PILOTS AND COPILOTS SIDE, FOUND CRACKED DURING 240 MONTH INSP.
- [SDR WWQ2007F00001](https://openairdocs.org/sdr/WWQ2007F00001), Aug 5, 2007: WIRE HARNESS. SHORTED. DURING APPROACH, THE CREW EXTENDED THE LANDING GEAR (NORMAL PROCEDURE). SEVERAL SECONDS AFTER THE GEAR EXTENSION THE NOSE LANDING GEAR DOWN AND LOCKED GREEN LIG
- [SDR 2007FA0000000](https://openairdocs.org/sdr/2007FA0000000), Dec 1, 2006: ENGINE. FAILED. RT ENGINE FAILURE AT T/O. ALL INDICATIONS WERE NORMAL ON ENGINE START AND TAXI. UPON THRUST ADVANCEMENT FOR TAKEOFF, AT APPROXIMATELY 60 PERCENT N1 WE HEARD AND
- [SDR 2006FA0000949](https://openairdocs.org/sdr/2006FA0000949), Sep 7, 2006: WINDSHIELD. CRACKED. LT WINDSHIELD (PILOTS) OUTER-PLY CRACKED DURING FLIGHT. NO KNOWN CAUSE AS TO THE EVENTS LEADING TO CRACK. KNOWN TO BE A COMMON FAILURE ON CHALLENGER ACRYLIC WIN
- [SDR DJFA2005103](https://openairdocs.org/sdr/DJFA2005103), May 30, 2005: RELIEF VALVE. LEAKING. SHORTLY AFTER T/O, TOWER REPORTED FUEL SPRAYING FROM RT WING. CREW VISUALLY VERIFIED, RETURNED AND LANDED WITHOUT INCIDENT. INSP FOUND FUEL LEAKING FROM RT WING
- [SDR DJFA2005086](https://openairdocs.org/sdr/DJFA2005086), Apr 25, 2005: BULB. BURNED OUT. CREW REPORTED THAT UPON GEAR EXTENSION THEY DID NOT RECEIVE THE NOSE GEAR DOOR INDICATION. A FLY-BY PAST THE TOWER WAS PERFORMED TO VERIFY NOSE GEAR POSITION. D
- [SDR 041251](https://openairdocs.org/sdr/041251), Apr 12, 2005: CLAMP. BROKEN. APU HAD BEEN RUNNING ON THE GROUND FOR APPROXIMATELY ONE HOUR AND SHUT ITSELF DOWN DUE TO HIGH OIL TEMP AS INDICATED BY (BYTE) LIGHT. VISUAL INSPECTION SHOWED T
- [SDR N382005F00003](https://openairdocs.org/sdr/N382005F00003), Feb 16, 2005: GCU. BURNED. UPON AIRCRAFT TEST FLIGHT FOR COMPLETION OF TAWS INSTALLATION. AIRCRAFT EXPERIENCED SMOKE IN THE CABIN AND COCKPIT. CREW DECLARED AND EMERGENCY LANDING AND PERF
- [SDR 2004F00032](https://openairdocs.org/sdr/2004F00032), Nov 25, 2003: WINDSHIELD. CRACKED. LEFT WINDSHIELD FAILED IN FLIGHT, OUTER PANE CRACKED AND SEPARATED. CREW FOLLOWED CHECKLIST PROCEDRUES AND LANDED AT A SUITABLE AIRFIELD. (M)
- [SDR N382003F00001](https://openairdocs.org/sdr/N382003F00001), Aug 1, 2003: FUEL CONTROL. FAILED. AT APPROXIMATELY 0650 PACIFIC TIME, WHILE ON CLIMB OUT AND CLIMBING THROUGH 5500 FT MSL THE AIRCRAFT EXPERIENCED AN UNCOMMANDED SHUTDOWN OF THE LEFT ENGINE. ALL
- [SDR SH52003F00000](https://openairdocs.org/sdr/SH52003F00000), Feb 14, 2003: FUEL CONTROL. INOPERATIVE. AIRCRAFT WAS HOLDING ON TAXIWAY WITH WINDS OVER 40 KNOTS AND BLOWING SNOW. A/C WAS BEHIND A/C WHICH WAS KICKING UP ADDITIONAL SNOW. PILOT PUT ON THE COWL ANTI-I
- [SDR SH52002F00000](https://openairdocs.org/sdr/SH52002F00000), Jan 9, 2002: SILL. CRACKED. DURING SCHEDULED INSPECTION FOUND LOWER WINDSHIELD SILL CRACKED (PRIMARY STRUCTURE) ON LEFT AND RIGHT SIDE OF COCKPIT. BOTH CRACKS ARE AT FS 235.0 WL 110.5 AND 
- [SDR QXEA0101591](https://openairdocs.org/sdr/QXEA0101591), Sep 25, 2001: SEAL. DENTED. PDX - MAIN CABIN DOOR SEAL MATING SURFACE IS DENTED MIDWAY ALONG THE FORWARD LENGTH OF DOOR APERATURE. REPAIRED IAW EA R-53-03.
- [SDR CA010912014](https://openairdocs.org/sdr/CA010912014), Sep 9, 2001: HANDLE. BROKEN. (CAN) THE RAMP PERSONNEL BROKE THE OUTER HANDLE OF THE SERVICE DOOR DURING NORMAL OPERATION. THE PERSON WORKING REPORTED THAT HE DID NOT USED ANY EXCESSIVE FORC
- [SDR CA010501008](https://openairdocs.org/sdr/CA010501008), Apr 16, 2001: WINDSHIELD. CRACKED. (CAN) R/H WINDSHIELD CRACKED WHILE ON APPROACH. MAINTENANCE REMOVED AND REPLACED RT WINDSHIELD WITH NEW UNIT. AIRCRFT BACK IN SERVICE.
- [SDR CA000720014](https://openairdocs.org/sdr/CA000720014), Jun 20, 2000: BATTERY. WRONG PART. (CAN) UPON ELT RECERTIFICATION, A NON TC APPROVED BATTERY WAS FOUND IN THE UNIT.ONLY THE DM U158-1 IS APPROVED BY TC (REF AWN BO14, EDITION 4) FOR USE IN THIS E
- [SDR 20000620SH027](https://openairdocs.org/sdr/20000620SH027), May 25, 2000: POTENTIOMETER. FAILED. A DIMMER POT (R3LM) WAS FOUND BURNT AND MELTED AFTER IT WAS REPORTED THE NR 1 F/D WAS TRIPPING THE CIRCUIT BREAKER ON THE DC ESSENTIAL BUSS. THE POT IS PART OF 
- [SDR CA000519016](https://openairdocs.org/sdr/CA000519016), May 15, 2000: ACTUATOR. FAILED. (CAN) WHILE TAXING TO RAMP PILOT MOVED STAB TRIM TO NOSE DOWN POSITION. CHANNEL 1 NOSE DOWN FAIL LIGHT CAME ON AND ACT WOULD NOT MOVE. MAINT CHANGED PITCH TRIM 
- [SDR 20000503SH050](https://openairdocs.org/sdr/20000503SH050), Apr 13, 2000: WINDOW POST. CRACKED. DURING THE ACCOMPLISHMENT OF THE AIRCRAFT MANUFACTURER''S REQUIRED 6,600 HOUR CHECKS, A CRACK WAS NOTED ON THE UPPER SURFACE OF THE WINDSCREEN LOWER SILL FRAME 
- [SDR 20000424SH011](https://openairdocs.org/sdr/20000424SH011), Mar 15, 2000: HEATER. INOPERATIVE. PILOT''S LEFT FRONT WINDSHIELD HEAT ELEMENT INOPERATIVE. (X)
- [SDR 2000ZZZX109](https://openairdocs.org/sdr/2000ZZZX109), Dec 10, 1999: COVER. CRACKED. THE LEFT NOSE COWL AIRLINE COVER (POCKET) FOR THE 14TH STAGE T/R PDU LINE SHOWS SIGNS OF HEAT DAMAGE AND IS BUCKLED AND CRACKED.
- [SDR CA991209046](https://openairdocs.org/sdr/CA991209046), Nov 13, 1999: ACTUATOR. FAILED. (CAN) OCCASIONALLY FLAPS FAILED IN COLD WEATHER. NR 3 ACTUATOR REPLACED AND PROBLEM WENT AWAY.
- [SDR CA991028064](https://openairdocs.org/sdr/CA991028064), Oct 7, 1999: BRAKE. FAILED. (CAN) TECHNICIAN NOTICED THE RIGHT OUTBOARD MAIN WHEEL WAS FLAT. THE FUSE PLUG WAS FOUND MELTED AS WELL AS A LOCALIZED WEAR (FLAT SPOT) ON THE TIRE. IT WAS NOTI
- [SDR CA990521046](https://openairdocs.org/sdr/CA990521046), May 13, 1999: ENGINE. MAKING METAL. (CAN) AT 7,000 FEET, A SHEARING NOISE WAS HEARD FROM NR 2 ENGINE. THE ENGINE WAS SHUT DOWN. POST-FLIGHT INSPECTION FOUND METAL IN THE MAIN OIL FILTER AND CHIP D
- [SDR CA990226006](https://openairdocs.org/sdr/CA990226006), Feb 2, 1999: PUMP. MALFUNCTIONED. (CAN) NR 2 ENGINE LOW OIL PRESSURE LIGHT IN-FLIGHT. POST-FLIGHT INSPECTION FOUND THE NR 2 ENGINE OIL PUMP WAS INOPERATIVE.

All 78: https://openairdocs.org/model/canadair-cl-600-2a12/reports.md

## STCs that may be installed (OpenAirDocs) (495, first 50)

Approved for this model: the STC's model list names it on its data sheet, or a series that includes it. In force first, then newest. The registry doesn't record which STCs an aircraft has.

- [STC ST01305WI-D](https://openairdocs.org/stc/ST01305WI-D): Modification of a Collins ALT-50A or ALT-55B Radio Altimeter system installation to a Collins ALT-1000 or ALT-4000 Radio Altimeter system installation in accordance with Collins Drawing Index as listed on AML No. ST01305WI-D, Revision -, or later FAA approved revision. Rockwell Collins Inc
- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST00885LA](https://openairdocs.org/stc/ST00885LA): Installation of fire extinguisher cartridges as replacements for Pacific Scientific fire extinguisher cartridges in fire extinguisher bottles. AMETEK AMERON, LLC d/b/a MASS Systems
- [STC ST12422IB](https://openairdocs.org/stc/ST12422IB): Water System Modifications. Bombardier Inc
- [STC ST00197IB](https://openairdocs.org/stc/ST00197IB): Installation of the Universal Quick Access Recorder (uQAR). Flight Data Technologies Inc
- [STC ST04735NY](https://openairdocs.org/stc/ST04735NY): Installation of LAI Windshields. Lee Aerospace Inc
- [STC SA2622NM](https://openairdocs.org/stc/SA2622NM): Installation of Precise Flight Pulselite Control Unit in landing/taxi system. (767-200 B17) (DHC-8 101). Precise Flight Inc
- [STC ST11216DS](https://openairdocs.org/stc/ST11216DS): Installation of automatic dependent surveillance-broadcast (ADS-B) out on Part 25 aircraft. BHE & Associates Ltd
- [STC ST03885AT](https://openairdocs.org/stc/ST03885AT): Installation of an Avionica, Inc. avCM Cellular Module. Aircraft Systems and Manufacturing Inc
- [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 ST10973SC](https://openairdocs.org/stc/ST10973SC): Activation of a high power cabin telecommunication router. BHE & Associates LTD
- [STC ST00431WI-D](https://openairdocs.org/stc/ST00431WI-D): Installation of a Fairchild F-1000 Data Flight Data Recorder System. KGB Aviation Solutions LLC
- [STC SA6011NM](https://openairdocs.org/stc/SA6011NM): Installation of floor proximity emergency escape path marking system. Bruce Aerospace Inc
- [STC ST209CH](https://openairdocs.org/stc/ST209CH): Installation of a model TCAS 791 TCAS I. Acron Aviation 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 ST03810NY](https://openairdocs.org/stc/ST03810NY): Installation of the INGENIO Cockpit Tripod Electronic Flight Bag (EFB) Mount. Ingenio Aerospace Inc
- [STC ST04745NY](https://openairdocs.org/stc/ST04745NY): Installation of LAI Cockpit Side Windows. Lee Aerospace Inc
- [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 ST04653CH](https://openairdocs.org/stc/ST04653CH): Installation of Gogo L5 System with MB13 Antennas. STANDARDAERO BUSINESS AVIATION SERVICES LLC,
- [STC ST01936WI](https://openairdocs.org/stc/ST01936WI): Installation of LED lights. AeroLED's Holdings LLC
- [STC ST01066DE](https://openairdocs.org/stc/ST01066DE): Installation of the Aviation Clean Air Airborne Air & Surface Purification System. Lee Aerospace, 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 ST01012WI](https://openairdocs.org/stc/ST01012WI): Installation of an Emergency Vision Assurance System (EVAS). VisionSafe LLC
- [STC ST01556WI](https://openairdocs.org/stc/ST01556WI): Installation of the Universal Avionics Dual 1Lw Flight Management System (FMS). Global Aviation Tech LLC
- [STC ST04839NY](https://openairdocs.org/stc/ST04839NY): Installation of LED Position/Anti-Collision Lights. Sterling Helicopter
- [STC ST04575AT](https://openairdocs.org/stc/ST04575AT): Installation of the Rockwell Collins ALT-1000+/ -4000+ with 5G Filtering. Chippewa Aerospace Inc
- [STC ST04636CH](https://openairdocs.org/stc/ST04636CH): Install Sage-Popovich Aircraft Tire Kit P/N 601SP-01, which allows removal of the nose and main landing gear tires and the installation of alternate new FAA TSO approved tires. Sage-Popovich 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 ST04613NY](https://openairdocs.org/stc/ST04613NY): Emergency Equipment Modification. Bombardier Inc
- [STC ST04028NY](https://openairdocs.org/stc/ST04028NY): The installation of Portable Oxygen Bottle Bracket replacement. Bombardier Inc
- [STC ST10680SC](https://openairdocs.org/stc/ST10680SC): Installation of an aerodynamic fairing and mounting provisions for an Enhanced Vision System. Summit Aviation Inc
- [STC ST00105IB](https://openairdocs.org/stc/ST00105IB): Introduction of Activation of Wireless Charging Systems for Portable Electronic Devices. AMAC AEROSPACE SWITZERLAND AG
- [STC SA8717SW](https://openairdocs.org/stc/SA8717SW): Installation of passenger briefing system. Heads Up Technologies Inc
- [STC ST00098IB](https://openairdocs.org/stc/ST00098IB): Introduction of ADS-B Out. STC Twenty One Limited
- [STC ST02004WI](https://openairdocs.org/stc/ST02004WI): Installation of the Garmin GI-275 Instantaneous Vertical Speed Indicators (IVSI). Peregrine
- [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 ST01086DE](https://openairdocs.org/stc/ST01086DE): Installation of the True Blue Power TS60 Lithium-ion Nanophosphate batteries as an alternate to existing Grimes Emergency Exit Lighting (EEL) Power Supply. Peregrine
- [STC ST00408BO](https://openairdocs.org/stc/ST00408BO): Modification of exterior lighting systems to replace the baseline position, anti-collision and landing lights with dual-mode, visible/infrared (IR) lights. Pro Star Aviation LLC
- [STC ST02293SE](https://openairdocs.org/stc/ST02293SE): Installation of a Crane Aerospace & Electronics Tire Sensor Assembly. ELDEC Aerospace Corp
- [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 ST01930LA](https://openairdocs.org/stc/ST01930LA): Installation of Sandel Avionics SN4500 Electronic Horizontal Situation Indicator (EHSI). Sandel Avionics LLC
- [STC ST00047WI](https://openairdocs.org/stc/ST00047WI): Installation of a bulkhead across fuselage station 353 with a hinged swinging door and magazine racks. Learjet Inc
- [STC ST00050WI](https://openairdocs.org/stc/ST00050WI): Installation of a bulkhead across fuselage station 542 with a hinged swinging door, a lavatory with a sink and a toilet on the right hand side. Learjet Inc
- [STC ST00099WI](https://openairdocs.org/stc/ST00099WI): Installation of entertainment cabinet. Learjet Inc
- [STC ST00100WI](https://openairdocs.org/stc/ST00100WI): Installation of bulkhead. Learjet Inc
- [STC ST00101WI](https://openairdocs.org/stc/ST00101WI): Installation of galley. Learjet Inc
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC ST03402CH](https://openairdocs.org/stc/ST03402CH): Installation of CMC Electronics CMA-2200SB SwiftBroadband (SBB) Satcom Antenna System. Intelsat Inflight LLC
- [STC ST02703SE](https://openairdocs.org/stc/ST02703SE): Installation of a hand sanitizer unit on Bombardier Challenger 601 (CL-600-2A12) series airplanes. B/E Aerospace Inc - FSI

All 495: https://openairdocs.org/model/canadair-cl-600-2a12/stcs.md

## PMA parts (OpenAirDocs) (over 1,000, first 50)

Current parts manufacturer approvals (PMA): parts the FAA has approved companies to make as replacements or modifications. Each record lists its models as free text; OpenAirDocs matched them to this model on its data sheet, so check the FAA record before relying on it. Newest first.

- [9143FR-0325](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194868012120260909221038.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR-0315](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID109435775720260909221037.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR-0200](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100760361520260909221037.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9522643-OAA](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID152058777320260729141228.0001): O-Ring. Omega Aircraft Articles LLC · PMA PQ4191CE · Replaces 9522643 · Jun 1, 2026
- [LSM-500-109](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID170829641820260909145845.0001): Boom Beam Instl Challenger 604 Wing Lights. Whelen Aerospace Technologies · PMA PQ1372CE · Modification part · May 22, 2026
- [1044478-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID128407871920260518152238.0001): Assembly, Beacon Light Spacer. StandardAero Business Aviation Services, LLC · PMA PQ2065CE · Modification part · Apr 10, 2026
- [BAI-CL60-WA01-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190649378720260312142042.0001): Pilot AMU Harness Pigtail. South West Aero Group · PMA PQ00026WB · Replaces STC Modification Part · Feb 17, 2026
- [SCD53001-501](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180892627720260312142043.0001): 0.38 Inch DZUS Panel. South West Aero Group · PMA PQ00026WB · Replaces STC Modification Part · Feb 17, 2026
- [SCD53001-504](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166936320620260312142043.0001): 1.50 Inch DZUS Panel. South West Aero Group · PMA PQ00026WB · Replaces STC Modification Part · Feb 17, 2026
- [BAI-CL60-WA01-502](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163037850120260312142042.0001): Copilot AMU Harness Pigtail. South West Aero Group · PMA PQ00026WB · Replaces STC Modification Part · Feb 17, 2026
- [SCD53001-502](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID156553259120260312142043.0001): 0.75 Inch DZUS Panel. South West Aero Group · PMA PQ00026WB · Replaces STC Modification Part · Feb 17, 2026
- [ST-9624-103-06](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194043882720260317193152.0001): CL600 Whelen Rear NAV/ACS Light Harness Assembly. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-101-102](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187713091720260317193148.0001): Orion 650E Adapter Sub-assembly. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-101-02](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID176795347720260317193148.0001): Orion 650E CL-600 Wingtip Adapter. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-101-101](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID175462223520260317193147.0001): Orion 500 Tail Can Sub-assembly. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-103-13B](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID174868985920260317193157.0001): CL600 Whelen left NAV Light Electrical Assembly. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-103-14A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID173876581720260317193157.0001): CL600 Whelen Right NAV Light Electrical Assembly. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-103-11](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID169056987120260317193155.0001): CL600 Whelen Right NAV/ACS Light Electrical Assembly. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-103-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID163986432420260317193155.0001): CL600 Whelen Left NAV/ACS Light Electrical Assembly. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-103-12](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID157468967020260317193156.0001): CL600 Whelen Rear NAV/ACS Light Electrical Assembly. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-103-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149476187620260317193149.0001): CL600 Whelen Left Light Harness Assembly. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-101-03](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID146489089620260317193149.0001): Harness Connector Bracket. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-103-15](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144446374620260317193158.0001): CL600 Whelen Rear NAV Light Electrical Assembly. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-103-14B](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143256999620260317193158.0001): CL600 Whelen Right NAV Light Electrical Assembly. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-103-13A](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143059448420260317193156.0001): CL600 Whelen left NAV Light Electrical Assembly. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-103-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139769750520260317193151.0001): CL600 Whelen Right Light Harness Assembly. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-103-09](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID107327703520260317193154.0001): CL600 Whelen Rear NAV Light Harness Assembly. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [ST-9624-101-01](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID103308393820260317193147.0001): Orion 500 Tail Light CL-600 CAN. Sterling Helicopter · PMA PQ10048NE · Modification part · Feb 12, 2026
- [5009885-1CCTS](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180643546320251204170214.0001): Screw, Button Head Cap. Carbon Component Tech Services · PMA PQ2157SW · Replaces 5009885-1 · Dec 3, 2025
- [5011211CCTS](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165032636120251204164434.0001): Pin,         Wear Indicator. Carbon Component Tech Services · PMA PQ2157SW · Replaces 5011211 · Dec 3, 2025
- [5010453-1CCTS](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145080833820251204164433.0001): Pin,       Wear Indicator. Carbon Component Tech Services · PMA PQ2157SW · Replaces 5010453-1 · Dec 3, 2025
- [AC9607F10Y3WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID147271060920260107201216.0001): Element, Filter. Wencor, LLC · PMA PQ1370NM · Replaces AC9607F10Y3 · Oct 30, 2025
- [4582201-5](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID180361333320260113211930.0001): Post Hinge Toilet Seat Assembly. Safran Cabin Inc. · PMA PQ1176NM · Replaces 4582201-5 · Aug 22, 2025
- [3868101N104](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID127515930620260113211931.0001): Panel Assy OX/LT/GSP RH. Safran Cabin Inc. · PMA PQ1176NM · Replaces 3868101N104 · Aug 22, 2025
- [WF336734](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190413661520250602133034.0001): Filter Element, Hydraulic. Donaldson Company Inc · PMA PQ2432CE · Replaces AC3258F-1297J · May 23, 2025
- [P-1119](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID165413741420250602133043.0001): Seal Assy. Donaldson Company Inc · PMA PQ2432CE · Replaces 3830159-1 · May 23, 2025
- [WF336733](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID144046950320250602133033.0001): Filter Element, Hydraulic. Donaldson Company Inc · PMA PQ2432CE · Replaces AC9607F10Y3, 7591357-001, 600-75118-2 · May 23, 2025
- [WF336732](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID117826719720250602133033.0001): Filter Element, Hydraulic. Donaldson Company Inc · PMA PQ2432CE · Replaces AC7031F8, 7593395-001, 600-75114-2 · May 23, 2025
- [WF337192](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID100012405720250602133038.0001): Filter Element, Air. Donaldson Company Inc · PMA PQ2432CE · Replaces 30475 · May 23, 2025
- [804-1250-10](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID199810876020250612143629.0001): avRDC QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [21149GK-1](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190552366020250612143625.0001): Installation Kit, miniQAR / avRDC QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [802-0100-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID182936014820250603134034.0001): Kit, avCM 4G Adapter. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [650-0100-04](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID153031048820250603134026.0001): Cellular Module (avCM 4G), GSM / GRPS 4G, Quad Band, SMA. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [400-21149G-3-101, 400-21149G-3-103, 400-21149G-3-105, 400-21149G-3-111, 400-21149G-3-113, 400-21149G-3-115, 400-21149G-3-205, 400-21149G-3-215, 400-21149G-3-715, 400-21149G-3-815](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID148333503020250603134037.0001): Assy, LRU Adapter (miniQAR MKIII). Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [804-1201, 804-1205, 804-1205-03, 804-1212, 804-1216](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143255315920250612143621.0001): miniQAR MKIII. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [804-1250-32](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID136274797320250612143633.0001): avRDC MAX QAR. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [650-0100-05](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID135085465420250603134030.0001): Cellular Module, avCM LTE. Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [400-21149G-3-305, 400-21149G-3-315, 400-21149G-3-405, 400-21149G-3-415, 400-21149G-3-505, 400-21149G-3-515, 400-21149G-3-605, 400-21149G-3-615, 400-21149G-3-915](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID108993224620250603134041.0001): Assy, LRU Adapter (avRDC or MAX). Avionica LLC. · PMA PQ1734CE · Modification part · Apr 18, 2025
- [663700-124WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID149233266820250226225452.0001): Packing. Wencor, LLC · PMA PQ1370NM · Replaces 663700-124 · Jan 30, 2025
- [LA600-33030-027](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID166345754520250129184217.0001): Cockpit Side Window Assembly, LH. Lee Aerospace, Inc. · PMA PQ3766CE · Modification part · Jan 24, 2025

All of them: https://openairdocs.org/model/canadair-cl-600-2a12/pma.md

## The same model under other registry codes

Amateur-built copies and renamed makers get their own codes.

- [Bombardier CL-600-2A12](https://openairdocs.org/model/bombardier-cl-600-2a12): 1 registered aircraft, registry code 1390018
- [Canadair CL-600-2A12(CL-601)](https://openairdocs.org/model/canadair-cl-600-2a12-cl-601): 1 registered aircraft, registry code 1900312

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