# N65CL: Canadair CL215 1A10

- Status: Valid registration
- Airframe: [Canadair CL215 1A10](https://openairdocs.org/model/canadair-cl215-1a10) (registry code 1900111, 10 seats)
- Data sheets: [TCDS A14EA](https://openairdocs.org/tcds/A14EA) (De Havilland Aircraft of Canada Limited) (OpenAirDocs)
- Serial number: 1065
- Type: Fixed wing multi engine
- Engine type: Turbo-jet
- Certificate issued: January 7, 2020
- Expires: January 31, 2027
- Mode S code: A88A9E
- Registered owner: [Cl415 Aviation Salvage LLC](https://openairdocs.org/faa-owner/CL415%20AVIATION%20SALVAGE%20LLC)
- Location: [Belgrade, MT](https://openairdocs.org/faa-place/MT/Belgrade)
- Owner type: LLC
- Owner's area on the map: 45.9725° N, 111.1347° W: Placed by OpenAirDocs at the center of ZIP code 59714, within about 12 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=65CL
- Page: https://openairdocs.org/aircraft/N65CL

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 29 in force

### Matched by airframe (Canadair CL215 1A10)

- [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 2023-07-10](https://openairdocs.org/ad/2023-07-10): Equipment/furnishings · Viking Air CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Jun 20, 2023
- [AD 2023-10-02](https://openairdocs.org/ad/2023-10-02): Indicating/Recording System, Navigation · Boeing 18, 23, 35 and 1,060 more. Effective May 26, 2023
- [AD 2019-25-11](https://openairdocs.org/ad/2019-25-11): Wings · Viking Air CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Feb 10, 2020
- [AD 2019-02-05](https://openairdocs.org/ad/2019-02-05): Wings · Viking Air CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Mar 22, 2019
- [AD 2017-17-17](https://openairdocs.org/ad/2017-17-17): Hydraulic power · Viking Air CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Oct 11, 2017
- [AD 2012-11-04](https://openairdocs.org/ad/2012-11-04): Wings · Bombardier CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Jul 9, 2012
- [AD 2012-05-05](https://openairdocs.org/ad/2012-05-05): Equipment/Furnishings · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Apr 24, 2012
- [AD 2011-22-06](https://openairdocs.org/ad/2011-22-06): Landing Gear · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Nov 14, 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 2004-25-16 R1](https://openairdocs.org/ad/2004-25-16-R1): Fuel regulator shutoff valve · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 64 more. Effective Jun 20, 2005
- [AD 2004-21-05](https://openairdocs.org/ad/2004-21-05): B-Seires Combustion Heaters · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant), CL-215-6B11 (CL-415 Variant) and 41 more. Effective Nov 19, 2004
- [AD 2004-03-13](https://openairdocs.org/ad/2004-03-13): Main landing gear (MLG) axles · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 17, 2004
- [AD 2002-12-12](https://openairdocs.org/ad/2002-12-12): Wing-to-Fuselage Frame Angles · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Jul 25, 2002
- [AD 96-23-13](https://openairdocs.org/ad/96-23-13): DC Generators · Bombardier CL-215-1A10. Effective Dec 5, 1996
- [AD 96-05-06](https://openairdocs.org/ad/96-05-06): Inspect Main Distribution Center and Electrical Components · Bombardier CL-215-1A10. Effective Mar 22, 1996
- [AD 93-16-06 R2](https://openairdocs.org/ad/93-16-06-R2): Rudder-Aileron Interconnect Tab · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Oct 25, 1995
- [AD 78-08-02](https://openairdocs.org/ad/78-08-02): Water Door Hinge Plates · Bombardier CL-215-1A10. Effective Apr 14, 1978
- [AD 77-17-13](https://openairdocs.org/ad/77-17-13): Nose Landing Gear Doors · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Aug 30, 1977
- [AD 77-15-03](https://openairdocs.org/ad/77-15-03): Elevator Torque Tube Quadrant · Bombardier CL-215-1A10. Effective Jul 27, 1977
- [AD 77-13-05](https://openairdocs.org/ad/77-13-05): Missing Rivets In Bulkhead · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Jun 29, 1977
- [AD 77-10-14](https://openairdocs.org/ad/77-10-14): Main Landing Gear Actuator · Bombardier CL-215-1A10. Effective May 26, 1977
- [AD 77-09-06](https://openairdocs.org/ad/77-09-06): Lower Rudder Bearing · Bombardier CL-215-1A10. Effective May 9, 1977
- [AD 77-09-05](https://openairdocs.org/ad/77-09-05): Nose Landing Gear · Bombardier CL-215-1A10. Effective May 9, 1977
- [AD 77-09-04](https://openairdocs.org/ad/77-09-04): Main Landing Gear Wheel Well · Bombardier CL-215-1A10. Effective May 9, 1977
- [AD 75-12-02](https://openairdocs.org/ad/75-12-02): Engine Fire Bottles · Bombardier CL-215-1A10. Effective May 30, 1975
- [AD 72-15-04](https://openairdocs.org/ad/72-15-04): Flame Propagation In Engine Fire Zone · Bombardier CL-215-1A10. Effective Jul 25, 1972
- [AD 71-04-04](https://openairdocs.org/ad/71-04-04): Failure Water Door Tension Rod · Bombardier CL-215-1A10. Effective Feb 25, 1971
- [AD 70-01-05](https://openairdocs.org/ad/70-01-05): Chine Spray Strips · Bombardier CL-215-1A10. Effective Dec 8, 1970

### Historical (superseded or no longer in force)

- [AD 2013-11-03](https://openairdocs.org/ad/2013-11-03) (historical): Wings · Bombardier CL-215-1A10 and CL-215-6B11 (CL-215T Variant). Effective Jun 14, 2013
- [AD 2011-03-08](https://openairdocs.org/ad/2011-03-08) (historical): Landing gear · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 14, 2011
- [AD 2005-18-05](https://openairdocs.org/ad/2005-18-05) (historical): Lower caps of the wing front spar and rear spar · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Oct 6, 2005
- [AD 99-16-04](https://openairdocs.org/ad/99-16-04) (historical): Inspect Fuselage Frame-Angles · Bombardier CL-215-1A10. Effective Sep 7, 1999
- [AD 98-04-08](https://openairdocs.org/ad/98-04-08) (historical): Inspect Lower Cap of Wing Front & Rear Spars · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Mar 4, 1998
- [AD 96-12-11](https://openairdocs.org/ad/96-12-11) (historical): Water Door Actuator Microswitches · Bombardier CL-215-1A10. Effective Jun 21, 1996
- [AD 95-22-04](https://openairdocs.org/ad/95-22-04) (historical): Main Landing Gear Axle · Bombardier CL-215-1A10, CL-215-6B11 (CL-215T Variant) and CL-215-6B11 (CL-415 Variant). Effective Nov 8, 1995

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N65CL.

## FAA accident and incident reports

None matched to N65CL.

## Service difficulty reports

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

## Service difficulty reports on N65CL not matched to an aircraft (2)

They name N65CL, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR HSRR2012F00045](https://openairdocs.org/sdr/HSRR2012F00045), Jan 18, 2012: HINGE. CRACKED. ELEVATOR INBOARD HINGE CASTING HAS A CRACK IN THE MOUNTING FLANGE FROM THE BOLT HOLE ATTACH POINT TO THE OUTER EDGE OF THE CASTING.
- [SDR HSRA2011F00147](https://openairdocs.org/sdr/HSRA2011F00147), Jun 17, 2011: PISTON. CRACKED. FLAP ACTUATOR PISTON FOUND CRACKED (SPLIT ACTUALLY) NEARLY ITS FULL LENGTH.

## STCs that may be installed (OpenAirDocs) (15)

Approved for this aircraft's airframe or engine model, in force first, then newest. The registry doesn't record which STCs an aircraft has; its records do.

### Approved for the airframe (Canadair CL215 1A10)

- [STC ST12461IB](https://openairdocs.org/stc/ST12461IB): Installation of Cockpit Voice Recorder with optional RIPS Upgrade. Mid- Canada Mod Center
- [STC ST04328NY](https://openairdocs.org/stc/ST04328NY): The Manufacture and Installation of Exterior Placards, Labels and Signs is to be performed, installed. Libellule Monde Inc
- [STC ST03875NY](https://openairdocs.org/stc/ST03875NY): Installation of interior placards, signs and markings. Libellule Monde 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 SA01967WI](https://openairdocs.org/stc/SA01967WI): Use of GAMI G100UL High Octane Unleaded Avgas. General Aviation Modifications Inc
- [STC ST04689NY](https://openairdocs.org/stc/ST04689NY): Installation of the Artex Emergency Locator Transmitter (ELT). Genesys Certification Services Inc
- [STC ST04653NY](https://openairdocs.org/stc/ST04653NY): Installation of the Collins Aerospace Angle of Attack Indicating System. B/E Aerospace Limited
- [STC ST04177AT](https://openairdocs.org/stc/ST04177AT): Installation of a Talon Aerospace LED Replacement General Purpose Lamps. Aaxico Technical Services Inc
- [STC SA00944CH](https://openairdocs.org/stc/SA00944CH): Replace Janitrol combustion heater Model 81D94-X (XX) with C&D Associates combustion heater Model CD25K, CD35K, and CD45K. Hartzell Engine Technologies, LLC
- [STC SA571NE](https://openairdocs.org/stc/SA571NE): Installation of cockpit vapor cycle air conditioning system kit No. 215-CCA-001. Rilpa Enterprises, Ltd
- [STC ST01425NY](https://openairdocs.org/stc/ST01425NY): Installation of a Flight Deck Cooling System. ACS-NAI Limited
- [STC ST01824NY](https://openairdocs.org/stc/ST01824NY): Installation of Northern Airborne Technology Satphone. Northern Airborne Technology Ltd
- [STC ST01468CH](https://openairdocs.org/stc/ST01468CH): Installation of various SMR Technologies electrical propeller deicer models. SMR Technologies
- [STC SQ00643NY](https://openairdocs.org/stc/SQ00643NY): Installation of spinners and balancing weights for dynamic propeller balancing. Airworthiness Resources Corporation
- [STC SA2178WE](https://openairdocs.org/stc/SA2178WE): Installation of liquid spray system. Aviation Specialties Inc

## Earlier aircraft with N65CL

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N65CL before.

- [Cancelled 1991-10-16](https://openairdocs.org/deregistered/N65CL-1991-10-16): Boeing Of Canada/Dehav Div DHC-8-102, S/N 065. Exported to Canada. Owner: [Wilminton Trust Co](https://openairdocs.org/faa-owner/WILMINTON%20TRUST%20CO), [Wilmington, DE](https://openairdocs.org/faa-place/DE/Wilmington)

## Related

- Other Canadair CL215 1A10 aircraft: https://openairdocs.org/model/canadair-cl215-1a10/aircraft.md

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