AD 77-09-05
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Bombardier Inc. | CL-215-1A10 | Airworthiness Directives; CANADAIR Model CL-215-1A10 Airplanes |
Unsafe Condition
Structural failure of the nose landing gear door closing rods, P/N 215-85009, and the sequencing redundancy mechanism rod, P/N 215-85026, which could compromise structural integrity.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Inspect and rework in accordance with Canadair Service Information Circular No. 101-CL-215 dated May 6, 1975, or an equivalent method approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Compliance is required as indicated unless already accomplished. For aircraft in service 12 months or more, compliance is required and flight operations are restricted to land operations until compliance. For aircraft in service less than 12 months, compliance is required before achieving 12 months in service.
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Canadair Model CL-215-1A10 airplanes, Serial Numbers 1001 to 1040 inclusive.
AI-generated summary from the source AD text. Verify against the official source before acting.
Source: Official FAA Source ↗
Retrieved: Apr 8, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.