AD 93-16-06 R2
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | CL-215-1A10 | Airworthiness Directives: Canadair Models CL-215-1A10 and CL-215-6B11 Series Airplanes |
| aircraft | Bombardier Inc. | CL-215-6B11 (CL-215T Variant) | Airworthiness Directives: Canadair Models CL-215-1A10 and CL-215-6B11 Series Airplanes |
| aircraft | Bombardier Inc. | CL-215-6B11 (CL-415 Variant) | Airworthiness Directives: Canadair Models CL-215-1A10 and CL-215-6B11 Series Airplanes |
Unsafe Condition
Potential flutter of the rudder-aileron interconnect tab, which could result in reduced controllability of the airplane.
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Required Actions
Install weights to the aileron balance weight mounting channel and install washers to the interconnect tab mass balance arms on the right wing, in accordance with Canadair Alert Service Bulletin 215-A435, dated August 14, 1990.
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Compliance Time
Within 12 months after the effective date of this AD
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Affected Aircraft
Bombardier Inc. Models CL-215-1A10 (serial numbers 1001 through 1125 inclusive) and CL-215-6B11 series airplanes not equipped with powered ailerons.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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