| AD Number | 77-10-14 | Status | Active |
| Effective Date | May 26, 1977 | Issue Date | Not specified |
| Docket Number | Unknown | Amendment | 39-2908 |
| Product Type | ["Aircraft"] | Product Subtype | ["Large Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | N/A |
| Citation | This information is not available. | ||
| Manufacturer(s) | Bombardier Inc. |
| Model(s) | CL-215-1A10 |
77-10-14 CANADAIR: Amendment 39-2908. Applies to Canadair CL-215-1A10 Airplanes, Serial Numbers 1001 through 1040 and 1046 certificated in all categories that have not been altered in accordance with Canadair Service Information Circular No. 136-CL-215.
Compliance required prior to U.S. Airworthiness certification.
Inspect and alter main landing gear actuator attachment fitting P/N 215-34014-1 and -2 in accordance with Canadair Service Information Circular No. 136-CL-215, page 2 of 3 dated June 11, 1976, or an approved equivalent.
Equivalent inspections and parts must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.
This amendment becomes effective May 26, 1977.