# Bombardier CL-600-2A12

- Type: Aircraft model (FAA registry)
- Registry code: 1390018
- Manufacturer (registry): BOMBARDIER INC
- 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: 1
- Page: https://openairdocs.org/model/bombardier-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/bombardier-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 (1)

- [N480LA](https://openairdocs.org/aircraft/N480LA): [Luxury Aero Collection LLC](https://openairdocs.org/faa-owner/LUXURY%20AERO%20COLLECTION%20LLC), [Scottsdale, AZ](https://openairdocs.org/faa-place/AZ/Scottsdale), built 1983, S/N 3003

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## 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/bombardier-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/bombardier-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/bombardier-cl-600-2a12/pma.md

## The same model under other registry codes

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

- [Canadair CL-600-2A12](https://openairdocs.org/model/canadair-cl-600-2a12): 19 registered aircraft, registry code 1900304
- [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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