AD 77-09-04
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | CL-215-1A10 | Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes |
Unsafe Condition
Cracks in main landing gear wheel well angles, part numbers 215-32200-58, -59, -60, -61, could compromise structural integrity.
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Required Actions
Inspect for cracks and modify in accordance with Canadair Service Information Circular No. 104-CL-215 dated September 5, 1975, or an equivalent approved by the Chief, Engineering and Manufacturing Branch, Eastern Region. Repeat inspections at intervals not exceeding 150 hours in service.
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Compliance Time
Before the next flight for aircraft with 1000 or more hours in service; at or before 1000 hours in service for those with less. Subsequent inspections must be repeated at intervals not to exceed 150 hours in service.
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Affected Aircraft
Canadair Model CL-215-1A10 airplanes, serial numbers 1001 to 1040 inclusive, not altered with Canadair Reinforcement Kit K215-30043 or an FAA approved equivalent.
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Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
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