AD 82-01-01
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | CL-600-1A11 (CL-600) | Airworthiness Directives; CANADAIR Model CL-600 Airplanes |
| aircraft | Bombardier Inc. | CL-600-2A12 (CL-601) | Airworthiness Directives; CANADAIR Model CL-600 Airplanes |
| aircraft | Bombardier Inc. | CL-600-2B16 (CL-601-3A) | Airworthiness Directives; CANADAIR Model CL-600 Airplanes |
| aircraft | Bombardier Inc. | CL-600-2B16 (CL-601-3R) | Airworthiness Directives; CANADAIR Model CL-600 Airplanes |
| aircraft | Bombardier Inc. | CL-600-2B16 (CL-604) | Airworthiness Directives; CANADAIR Model CL-600 Airplanes |
| aircraft | Bombardier Inc. | CL-600-2B19 (Regional Jet Series 100) | Airworthiness Directives; CANADAIR Model CL-600 Airplanes |
Unsafe Condition
Asymmetric spoiler deployment due to improper rigging of left and right controlex cables (parts numbers 600-91305-5 and 600-91305-7).
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Visually inspect and adjust the left and right controlex cables for compliance with Canadair Alert Service Bulletin A600-0024, Revision 1, or an approved method. Airplanes may be flown under FAR 21.197 to a maintenance base for inspection.
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Compliance Time
within ten days after the effective date of this AD
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Affected Aircraft
Bombardier Inc. Model CL-600 airplanes with serial number 1002 to 1050 inclusive
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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