- Effective
- April 14, 1978
- Model
- CL-215-1A10
- Data sheet
- TCDSA14EA
- Registered aircraft
- 2 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-3179
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 | d6143081…8a7d643 | FAA DRS (API key needed) |
On this page
The airworthiness directive
78-08-02 CANADAIR: Amendment 39-3179. Applies to Canadair CL-215-1A10 Airplanes, Serial Numbers 1001 through 1050 which incorporate aluminum alloy water door hinge plates 215-33159-2, -3, -6 or 7.
Compliance required prior to U.S. airworthiness certification.
Unless already accomplished replace the aluminum water door hinge plates, P/N 215- 33159-2, -3, -6 or -7 with steel hinge plates, P/N 215-33159-8 or approved equivalents in accordance with paragraph 2(d) of Canadair Service Information Circular No. 143-CL-215, Issue 3, Revision B, dated October 20, 1977, or an approved equivalent.
Equivalent replacement parts and installation procedures must be approved by the Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.
is amendment is effective April 14, 1978.
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.