# Canadair CL600-1A11

- Type: Aircraft model (FAA registry)
- Registry code: 1900316
- Manufacturer (registry): CANADAIR LTD
- Model: CL600-1A11
- Aircraft type: Fixed wing multi engine
- Category: Airplane
- Engines: 2 · Turbo-jet
- Seats: 23
- 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: 2
- Page: https://openairdocs.org/model/canadair-cl600-1a11

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 2025-07-09](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 2025-07-01](https://openairdocs.org/ad/2025-07-01): Air Data Computer · Synthetic Vision Electronic Flight Information System (Arrow STC SR09595RC or ST01523WI). Effective May 15, 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 2019-08-08](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 2017-20-11](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 2017-13-09](https://openairdocs.org/ad/2017-13-09): Engine Exhaust · Bombardier CL-600-1A11 (CL-600). Effective Aug 3, 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 2015-07-02](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 2013-03-08](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 2011-01-09](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 2009-23-09](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 2002-22-12](https://openairdocs.org/ad/2002-22-12): Titeflex hoses · BAE Systems ATP, Avro 146-RJ100A, Avro 146-RJ70A and 122 more. Effective Dec 13, 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
- [AD 2000-24-01](https://openairdocs.org/ad/2000-24-01): Main Landing Gear Wheel Bay Protection Shields · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Dec 19, 2000
- [AD 2000-19-01](https://openairdocs.org/ad/2000-19-01): Main Landing Gear · Bombardier CL-600-1A11 (CL-600) and CL-600-2A12 (CL-601). Effective Oct 25, 2000
- [AD 99-26-16](https://openairdocs.org/ad/99-26-16): MLG Hydraulic And Fuel Lines · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 2 more. Effective Feb 1, 2000
- [AD 98-03-02](https://openairdocs.org/ad/98-03-02): Anti-Noise Filter on Standby & APU · Bombardier CL-600-1A11 (CL-600) and CL-600-2A12 (CL-601). Effective Mar 6, 1998
- [AD 95-22-01](https://openairdocs.org/ad/95-22-01): Fluorescent Lighting System · Aerospace Lighting Fluorescent lighting systems, A310-203, A310-204 and 74 more. Effective Dec 4, 1995
- [AD 95-18-07](https://openairdocs.org/ad/95-18-07): Inspect Rudder Control Quadrant · Bombardier CL-600-1A11 (CL-600), CL-600-2A12 (CL-601), CL-600-2B16 (CL-601-3A) and 17 more. Effective Oct 30, 1995

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 2014-16-02](https://openairdocs.org/ad/2014-16-02) (historical): Engine Exhaust · Bombardier CL-600-1A11 (CL-600). Effective Aug 12, 2014
- [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 96: https://openairdocs.org/model/canadair-cl600-1a11/ads.md

## Information bulletins (advisory) (3)

- [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-10-13](https://openairdocs.org/saib/NM-10-13): Navigation: Flight Management System. Issued Jan 7, 2010

## Registered aircraft (2)

- [N108AD](https://openairdocs.org/aircraft/N108AD): [Marquez Padilla Inc](https://openairdocs.org/faa-owner/MARQUEZ%20PADILLA%20INC), [Bonita, CA](https://openairdocs.org/faa-place/CA/Bonita), built 1983, S/N 1080
- [N619TS](https://openairdocs.org/aircraft/N619TS): [Mavana Heli Support USA Inc](https://openairdocs.org/faa-owner/MAVANA%20HELI%20SUPPORT%20USA%20INC), [Miami, FL](https://openairdocs.org/faa-place/FL/Miami), built 1981, S/N 1019, Non-citizen corporation, flight hours not reported

## NTSB investigations

None matched to aircraft with this model.

## FAA accident and incident reports

None matched to aircraft with this model.

## Service difficulty reports (69, newest 50)

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

- [SDR CA190402017](https://openairdocs.org/sdr/CA190402017), Nov 12, 2018: LANYARD. WRONG PART. (CAN) FOLLOWING AN ISSUE ON THE CL605 (CL6-CA-35-7), TCCA HAS REQUESTED BOMBARDIER TO CONFIRM THAT CL600/601 WAS NOT IMPACTED BY THIS ISSUE. BOMBARDIER CONDUCTE
- [SDR CA140106008](https://openairdocs.org/sdr/CA140106008), Jan 3, 2014: THRUST REVERSER. FAILED. (CAN) RIGHT THRUST REVERSER DEPLOYMENT JAN 3. 2014. ACFT DEPARTED YOW. TAKEOFF WENT WITHOUT INCIDENT. CLIMBING THROUGH 5000 FT. WE HEARD A BANG, ACFT YAWED AND 
- [SDR 2012FA0000169](https://openairdocs.org/sdr/2012FA0000169), Mar 12, 2012: CARBON SEAL. DEFECTIVE. AFTER PERFORMING SEVERAL PREFLIGHTS, IT WAS NOTED THAT THE NR 2 INTEGRATED DRIVE GENERATOR HAD AN INCREASE IN THE FREQUENCY AND QUANITY OF OIL SERVICING. AFTER 
- [SDR 2008FA0000537](https://openairdocs.org/sdr/2008FA0000537), Jul 24, 2008: SKIN. CORRODED. SURFACE CORROSION (PITTING) DISCOVERED ON BOTH WINGS LOWER SURFACES ADJACENT TO AND OB OF WHEEL WELLS, CORROSION DEEMED UNUSUALLY SEVERE. (K)
- [SDR ZLJ2008F00000](https://openairdocs.org/sdr/ZLJ2008F00000), Jul 24, 2008: SKIN. CORRODED. SURFACE CORROSION DISCOVERED ON FUSELAGE SKIN ADJACENT TO PRE-COOLER EXHAUSTS ON LT AND RT SIDES OF FUSELAGE. DISCREPANCY DISCOVERED WHILE PERFORMING PROCEDURE 
- [SDR 2007F00069](https://openairdocs.org/sdr/2007F00069), Dec 13, 2007: WINDSHIELD. CRACKED. EN ROUTE AT FL330, THE CAPTAIN NOTICED A CRACK IN THE EXTERIOR PANEL OF THE LT FWD WINDSHIELD. THE APPROPRIATE CHECKLIST WAS COMPLETED AND A SPEED REDUCTION AND
- [SDR WAI2007F00001](https://openairdocs.org/sdr/WAI2007F00001), Mar 6, 2007: FIRE LOOP. SHORTED. FLIGHT CREW REPORTED LT ENGINE FIRE DETECTION FAIL LIGHT CAME ON JUST PRIOR TO ROTATION, THEN FIRE LIGHT CAME ON JUST PRIOR TO ROTATION, THEN FIRE WARNING CAME 
- [SDR 2007F00023](https://openairdocs.org/sdr/2007F00023), Mar 6, 2007: FIRE LOOP. SHORTED. FLIGHT CREW REPORTED LT ENGINE FIRE DETECTION FAIL LIGHT CAME ON JUST PRIOR TO ROTATION, THEN FIRE WARNING CAME ON AT 1,500 FEET DURING CLIMB. STAYED ON AFTER D
- [SDR 2006FA0000563](https://openairdocs.org/sdr/2006FA0000563), Apr 24, 2006: ADG. DEPLOYED. AIR DRIVEN GENERATOR (ADG) UNEXPECTED DEPLOYED ON POST TAKEOFF CLIMB OUT. PRECAUTIONARY LANDING ACCOMPLISHED. ADG MECHANICALLY RETRACTED/ SAFED; AIRCRAFT FERRIE
- [SDR 2006FA0000589](https://openairdocs.org/sdr/2006FA0000589), Apr 12, 2006: BATTERY. LEAKING. A STRONG ACIDIC ODOR WAS PRESENT AFTER REMOVING ELT BATTERY FROM ELT INSPECTION FOUND A THICK WHITE LIQUID ON THE NEGATIVE SIDE OF ONE BATTERY CELL. THE EXPIRAT
- [SDR 2005FA0000845](https://openairdocs.org/sdr/2005FA0000845), May 24, 2005: FLOOR SUPPORT. CRACKED. FLOOR SUPPORT LOCATED AT RBL 9.0 FS 460 CRACKED AT FLANGE. DURING FLOORBEAM REPLACEMENT A VISUAL INSPECTION REVEALED CRACK AT FLANGE. INSPECTED 3 OTHER FLOOR SU
- [SDR DJFA2006372](https://openairdocs.org/sdr/DJFA2006372), Oct 18, 2003: FUEL CONTROL. UNKNOWN. AT FLIGHT LEVEL 390 FT NR 2 ENGINE SHUTDOWN ON IT'S OWN. PILOTS DESCENDED AND AT FLIGHT LEVEL 100 FT THEY WERE ABLE TO GET THE ENGINE STARTED. LANDED WITH NO FU
- [SDR DJFA200300003](https://openairdocs.org/sdr/DJFA200300003), Oct 18, 2003: FUEL CONTROL. MALFUNCTIONED. AT FLIGHT LEVEL 390 FT NR 2 ENGINE SHUTDOWN ON IT'S OWN. PILOTS DESENDED AND AT FLIGHT LEVEL 100 FT, WAS ABLE TO GET THE ENGINE STARTED. LANDED WITH NO FURTHER 
- [SDR 103901](https://openairdocs.org/sdr/103901), Sep 4, 2003: DUCT. DISCONNECTED. DETECTED A RISE IN CABIN ALTITUDE THAT WAS NOT CONSIDERED NORMAL. MADE A PRECAUTIONARY DESCENT AND PERFORMED THE CABIN PRESSURE LOW CHECKLIST. LANDED AIRCRAFT A
- [SDR EXO2003F00001](https://openairdocs.org/sdr/EXO2003F00001), Jan 21, 2003: MOUNT. CRACKED. DURING INSPECTION OF THE RT THRUST REVERSER TRANSLATING SLEEVE. THE TOP JACKSCREW MOUNTING WAS FOUND CRACKED AROUND THE O-RING.
- [SDR EXO2003F00000](https://openairdocs.org/sdr/EXO2003F00000), Nov 21, 2002: THRUST REVERSER. DAMAGED. DURING CLIMB THROUGH FL130 A LOUD BANG FOLLOWED BY RT THRUST REVERSER UNLOCK LIGHT, RETURNED TO AIRPORT. FOUND 12 O'CLOCK BALL SCREW ACTUATOR AFT ATTACH POINT F
- [SDR CA020517008](https://openairdocs.org/sdr/CA020517008), Apr 4, 2002: CROSSBEAM. CRACKED. (CAN) DURING INTERNAL STRUCTURAL INSPECTION OF THE TAIL AREA, A 5/8 INCH CRACK WAS FOUND ON THE RUDDER CONTROL CROSS BEAM SUPPORT (EMPENNAGE).THE PROBABLE CAUSE
- [SDR J8G2001F00000](https://openairdocs.org/sdr/J8G2001F00000), Jun 29, 2001: BEARING. DEFECTIVE. FLIGHT CREW NOTICED SMOKE IN THE CABIN AFTER TAKE-OFF FROM AIRPORT. THE AIRCRAFT RETURNED TO THE AIRPORT WITH NO FURTHER INCIDENT. INITIAL TROUBLESHOOTING INDIC
- [SDR 20010612CW007](https://openairdocs.org/sdr/20010612CW007), Jun 4, 2001: WINDSHIELD. DELAMINATED. OUTER FACE PLY DELAMINATION OF LEFT HAND PILOTS WINDSHIELD. PLY SEPARATION WAS BEYOND LIMITS OF MANUFACTURES STRUCTURAL REPAIR MANUAL TO CONTINUE OPERATION.
- [SDR 20010612CW006](https://openairdocs.org/sdr/20010612CW006), Jun 4, 2001: WINDOW. DEBONDED. PILOTS LEFT SIDE WINDOW WAS DISBONDED AT FORWARD VERTICAL EDGE.
- [SDR 20010427CW001](https://openairdocs.org/sdr/20010427CW001), Apr 5, 2001: WINDSHIELD. CRACKED. DURING CRUISE FLIGHT, LEFT WINDSHIELD CRACKED. CREW CALLED MAINTENANCE. MAINTENANCE ADVISED TO TURN HEAT OFF. DELAMINATION STOPPED, CONTINUED TO DESTINATION.
- [SDR 20001019SH026](https://openairdocs.org/sdr/20001019SH026), Aug 31, 2000: COMPRESSOR. CRACKED. CUSTOMER REPORTED HIGH OIL CONSUMPTION AND OIL SMELL IN CABIN. APU DISASSEMBLED FOR COMPRESSOR REPAIR. DURING MAINTENANCE, FOUND COMPRESSOR ROTOR CRACKED AT SEV
- [SDR 20001019SH025](https://openairdocs.org/sdr/20001019SH025), Aug 9, 2000: COMPRESSOR. FRACTURED. CUSTOMER REPORTED APU FAILURE, SUDDEN STOPPAGE, AND GEARBOX FAILURE. ACFT WAS ON GROUND AND APU IDLE, NOT LOADED. APU SUSTAINED A POWER GROUP CONTAINED SEPARATI
- [SDR CA000724013](https://openairdocs.org/sdr/CA000724013), Jul 8, 2000: TURBINE. SEIZED. (CAN) AFTER LANDING, DURING ROLLOUT, THE CREW DEPLOYED THE THRUST REVERSER AND THE RT ENGINE SHUTDOWN. THE AIRCRAFT CONTINUED TO THE HANGAR AND AN INITIAL EVALU
- [SDR CA000724012](https://openairdocs.org/sdr/CA000724012), Jul 5, 2000: ENGINE. FAILED. (CAN) DURING CRUISE AT 41,000 FT THE FLIGHT CREW NOTICED A SMALL SURGE IN POWER ON THE RT ENGINE FOLLOWED ABOUT 10 SECONDS LATER BY A DECREASE IN RPM AND INCREA
- [SDR CA000516033](https://openairdocs.org/sdr/CA000516033), Apr 11, 2000: FAN. FAILED. (CAN) FOLLOWING A/C ROTATIONAT 100AGL THE NUMBER 2 ENGINE AUTOMATICALLY SHUTDOWN WITH AN OVERSPEED INDICATION. N1 FAN WOULD NOT ROTATE. ENGINE REPLACED.
- [SDR 20000424SH010](https://openairdocs.org/sdr/20000424SH010), Mar 12, 2000: HEATER. INOPERATIVE. PILOT'S RIGHT FRONT WINDSHIELD HEATER INOPERABLE. (X)
- [SDR 2000ZZZX836](https://openairdocs.org/sdr/2000ZZZX836), Mar 2, 2000: FITTING. CRACKED. IN THE LAST 2 MONTHS HAVE FOUND 3 T-FITTINGS CRACKED AND LEAKING. (TWO ON 600 CHALLENGER, ONE ON 601). ONE DID CAUSE AN INTERRUPTION OF A FLIGHT. ALL THREE ARE 
- [SDR CA991230029](https://openairdocs.org/sdr/CA991230029), Dec 20, 1999: ACTUATOR. INTERMITTENT. (CAN) DURING POST INSTALLATION TEST, CHANNEL 2 FOUND OPERATING INTERMITTENTLY. DURING TRIM COMMAND MOTOR WOULD OPERATE BUT SCREW JACK WOULD NOT ALWAYS TURN. COM
- [SDR CA991230028](https://openairdocs.org/sdr/CA991230028), Dec 20, 1999: ACTUATOR. FAILED. (CAN) DURING POST INSTALLATION TESTING,CHANNEL 2 FOUND HARD FAILED. UNIT WAS RECEIVED IN THIS CONDITION FROM SUPPLIER. 0.0 HOURS
- [SDR 99ZZZX4400](https://openairdocs.org/sdr/99ZZZX4400), Sep 23, 1999: BRACKET. CRACKED. INSPECTION OF THE ADG BAY REVEALED THE ATTACH BRACKET, IN TWO PLACES, TO BE CRACKED. REMOVED AND REPLACED WITH A NEW BRACKET. LANDINGS: 4,672.
- [SDR 99ZZZX3566](https://openairdocs.org/sdr/99ZZZX3566), Aug 30, 1999: DUCT. CHAFED. DURING SCHEDULED INSPECTION, THE BLEED AIR DUCT, PN 215-0809-501, WAS FOUND CHAFING ON NR 2 BEARING OIL TUBE, PN 2-263-060-01. BOTH PARTS WERE CHAFED BEYOND LIM
- [SDR 20001212AP012](https://openairdocs.org/sdr/20001212AP012), Aug 16, 1999: WINDSHIELD. CRACKED. TAKEOFF FROM PUEBLO, COLORADO WAS NORMAL. AFTER 1:45 OF FLIGHT, A CRACK APPEARED ON THE LEFT WINDSHIELD. THE LEFT WINDSHIELD HEAT C/B WAS MANUALLY SWITCHED OFF;
- [SDR 99ZZZX3568](https://openairdocs.org/sdr/99ZZZX3568), Aug 16, 1999: WINDSHIELD. CRACKED. PILOT'S WINDSHIELD CRACKED (OUTER LAYER ONLY) IN CRUISE FLIGHT.
- [SDR CA990119007](https://openairdocs.org/sdr/CA990119007), Jan 7, 1999: VALVE. FAILED. (CAN) NOSE GEAR DOORS FAILED TO OPEN WHEN GEAR SELECTED DOWN. PROBLEM INTERMITTENT AFTER COLD SOAK AT ALTITUDE.
- [SDR 98ZZZX4312](https://openairdocs.org/sdr/98ZZZX4312), Nov 6, 1998: IDG. FAILED. THE NR 2 GENERATOR DROPPED OFF-LINE ON LANDING. MAINTENNACE FOUND THE INTEGRATED DRIVE GENERATOR (IDG) DIFFERENTIAL INDICATORS POPPED AND THE OIL BLACK. THE OIL
- [SDR 99ZZZX436](https://openairdocs.org/sdr/99ZZZX436), Oct 27, 1998: BULKHEAD. CRACKED. CRACKED BULKHEAD WEB AT FS 409. REF: SB 600-679. DATE SEPT 10, 1997. AD 97-24-02 AMEND 39-10209 EFFECT DATE 12-3-97. FS 409 REPAIRED ERGINEERING ORDER 600-53-17
- [SDR CA980608009](https://openairdocs.org/sdr/CA980608009), May 30, 1998: RELAY. FAILED. (CAN) BATTERY CHARGER ANNUNCIATOR ILLUMINATED DURING GROUND OPERATION. RELAY KP7A FOUND FAULTY. WHEN RELAY IS LATCHED BY A DC SENSE CIRCUIT, IT, IN TURN, WILL A
- [SDR 98ZZZX3215](https://openairdocs.org/sdr/98ZZZX3215), Mar 29, 1998: SPACER. MISINSTALLED. HPN - NORMAL TAKEOFF EN ROUTE BAHAMAS. APPROX 1 HR EN ROUTE AT FL 310, PILOT NOTED NR 1 ENG VIBRATION INCREASE FROM .3 M/S TO .6 M/S AND INCREASE IN ENG NOISE. 
- [SDR 98ZZZX533](https://openairdocs.org/sdr/98ZZZX533), Jan 22, 1998: SENSOR. MISINSTALLED. LEFT AND RIGHT WING ANTI-ICE FAIL LIGHTS CAME ON INTERMITTENTLY ANY TIME WING ANTI-ICE SYSTEM SELECTED. FOUND THE LEFT AND RIGHT WING TEMP SENSORS INSTALLED BAC
- [SDR 97ZZZX5136](https://openairdocs.org/sdr/97ZZZX5136), Nov 25, 1997: TIRE. DEFECTIVE. DURING POST-FLIGHT INSPECTION, A BUBBLE WAS FOUND ON THE SIDEWALL OF TIRE. AFTER TIRE WAS REPLACED, THE S/N WAS CHECKED AGAINST ANOTHER TIRE THAT HAD BEEN REMOV
- [SDR 97ZZZX4716](https://openairdocs.org/sdr/97ZZZX4716), Nov 7, 1997: HEATER ELEMENT. EXPLODED. THE HEATER ELEMENT FAILED WITH AN EXPLOSIVE LIKE CHARGE THAT SENT THE FAILED ELEMENT AND WIRES INTO THE HONEYCOMB GALLEY TOP.
- [SDR 97ZZZX3498](https://openairdocs.org/sdr/97ZZZX3498), Jul 22, 1997: CELL. SHORTED. AIRCRAFT BATTERY CHARGER DROPPING OFF-LINE. REMOVED AND SHIPPED BATTERY TO INSPECTION AND SERVICE. FOUND SHORTED CELL, STRAPS HAD BURNED SMALL HOLE THROUGH SIDE
- [SDR CA970314005](https://openairdocs.org/sdr/CA970314005), Mar 7, 1997: GEN CONTROL UNIT. FAILED. (CAN) DURING FLIGHT APU STARTED AND STABILIZED. THE #2 AC ESSENTIAL BUS WAS KNOCKED OFF LINE. APU GENERATOR CONTROL UNIT REPLACED AS WELL AS #2 GENERATOR CONTRO
- [SDR 96ZZZX5475](https://openairdocs.org/sdr/96ZZZX5475), Oct 8, 1996: TEE FITTING. LEAKING. 50 HRS AFTER MAJOR INSP, DEVELOPED LEAK IN LT WHEELWELL. FOUND NR 6 ELBOW CRACKED AND LEAKING. NEXT DAY FOUND HYD FLUID LEAKING OUT OF LT WHEELWELL AGAIN. FOUND
- [SDR 96ZZZX5474](https://openairdocs.org/sdr/96ZZZX5474), Oct 8, 1996: TEE FITTING. LEAKING. 50 HRS AFTER MAJOR INSP, DEVELOPED LEAK IN LT WHEELWELL. FOUND NR 6 ELBOW CRACKED AND LEAKING. NEXT DAY FOUND HYD FLUID LEAKING OUT OF LT WHEELWELL AGAIN. FOUND
- [SDR 96ZZZX5473](https://openairdocs.org/sdr/96ZZZX5473), Oct 8, 1996: ELBOW. LEAKING. 50 HRS AFTER MAJOR INSP, DEVELOPED LEAK IN LT WHEELWELL. FOUND NR 6 ELBOW CRACKED AND LEAKING. NEXT DAY FOUND HYD FLUID LEAKING OUT OF LT WHEELWELL AGAIN. FOUND
- [SDR CA960703019](https://openairdocs.org/sdr/CA960703019), Jul 17, 1996: ID GENERATOR. DEFECTIVE. (CAN) GENERATOR TRIPPPING OFF LINE. METAL IN SCAVENGE FILTER AND ON CHIP DETECTOR. COMPONENT CAUSING TROUBLE WILL HAVE TO BE DETERMINED ON TEARDOWN.
- [SDR 96ZZZM1323](https://openairdocs.org/sdr/96ZZZM1323), Jun 24, 1996: OUTFLOW VLV. MALFUNCTIONED. APPROX TWO HOURS INTO FLIGHT, CABIN PRESSURIZATION BEGAN TO FLUCTUATE 300 FEET IN AUTO MODE. AIR RUSHING NOISE COULD BE HEARD IN BAGAGE AREA. THE ELECTRO/PNEUMA
- [SDR 96ZZZX3018](https://openairdocs.org/sdr/96ZZZX3018), May 9, 1996: SUPPORT. CRACKED. DURING 300-HOUR ENGINE INSPECTION, A 6.5 INCH HORIZONTAL CRACK WAS FOUND IN THE FAN COWL SUPPORT AT 3 O'CLOCK POSITION. ALSO, VARIOUS BRACKETRY ATTACHED TO COWL

All 69: https://openairdocs.org/model/canadair-cl600-1a11/reports.md

## STCs that may be installed (OpenAirDocs) (584, 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 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 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 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 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 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 ST03595NY](https://openairdocs.org/stc/ST03595NY): Installation of Honeywell Laseref IV Upgrade. Dassault Aircraft Services (DAS)
- [STC ST04293CH](https://openairdocs.org/stc/ST04293CH): Installation of a Honeywell JetWave System. StandardAero Business Aviation Services LLC
- [STC ST01270WI-D](https://openairdocs.org/stc/ST01270WI-D): Installation of Honeywell MK V and MK VII EGPWS Runway Awareness and Advisory System (RAAS). This approval is limited to specifically idenitfied aircraft. Duncan Aviation Inc
- [STC SA636GL](https://openairdocs.org/stc/SA636GL): Installation of a single or dual King Radio KHF950 HF SSB transceiver. Honeywell International Inc
- [STC ST02635LA](https://openairdocs.org/stc/ST02635LA): Modification to replace the existing Mode S Transponder system with the ACSS NXT-600 Mode S Transponder with ADS-B Out. Aviation Communication and Surveillance Systems (ACSS) LLC
- [STC SA8139NM-D](https://openairdocs.org/stc/SA8139NM-D): Installation of a Collins VHF-22C Comm System with CTL-22C. Learjet Inc
- [STC ST02828AT](https://openairdocs.org/stc/ST02828AT): Installation of a Collins VHF communication data radio model VHF-400 with VDL Mode 2 (VDL-2) capability. Chippewa Aerospace Inc
- [STC ST02879AT](https://openairdocs.org/stc/ST02879AT): Installation of a Rockwell Collins Model CMU-4000 Communications Management Unit (CMU) with Controller Pilot Data Link Communication (CPDLC) capability. Chippewa Aerospace Inc
- [STC ST00055SE](https://openairdocs.org/stc/ST00055SE): Installation of emergency medical stretcher, oxygen, and electrical systems. LifePort LLC
- [STC ST04340NY](https://openairdocs.org/stc/ST04340NY): Installation of TCAS 7.1 (ACAS II) upgrade of Prior Existing TCAS 7.0. Scandinavian Avionics Design ApS

All 584: https://openairdocs.org/model/canadair-cl600-1a11/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.

- [S9413-008WE](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID123161636820261009134004.0001): Packing, Preform - Fluorocarbon. Wencor, LLC · PMA PQ1370NM · Replaces S9413-008 · Oct 1, 2026
- [9143FR-0325](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID194868012120260909221038.0001): Corrosion Prevention Sealing Tape. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR-](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID192318595320260909221034.0001): Corrosion. 3M Aerospace · PMA PQ04414CE · Modification part · Jul 7, 2026
- [9143FR](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID138000704120260909221030.0001): Corrosion. 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
- [WF336734](https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID190413661520250602133034.0001): Filter Element, Hydraulic. Donaldson Company Inc · PMA PQ2432CE · Replaces AC3258F-1297J · 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-cl600-1a11/pma.md

## The same model under other registry codes

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

- [Canadair CL-600-1A11](https://openairdocs.org/model/canadair-cl-600-1a11): 5 registered aircraft, registry code 1900308

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