- Effective
- May 26, 1977
- Model
- CL-215-1A10
- Data sheet
- TCDSA14EA
- Registered aircraft
- 2 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-2908
Unofficial copy of the text in the FAA’s Dynamic Regulatory System. The FAA’s own copy is the authoritative one. DRS record last changed May 30, 2024.
Copies of the files this page was built from, with their SHA-256. Retrieved October 18, 2026.
| File | Size | SHA-256 | Original |
|---|---|---|---|
| FAA DRS HTML | 19 KB | 1e4637f1…b53d11a | FAA DRS (API key needed) |
On this page
The airworthiness directive
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.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 2
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.