- Effective
- May 30, 1975
- Model
- CL-215-1A10
- Data sheet
- TCDSA14EA
- Registered aircraft
- 2 matched by model
- Product
- Aircraft · Large airplane
- Amendment
- 39-2220
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 | 1fd279ad…cad44ff | FAA DRS (API key needed) |
On this page
The airworthiness directive
75-12-02 CANADAIR: Amendment 39-2220. Applies to Canadair CL-215-1A10 airplanes certificated in all categories.
Compliance required with the next twenty-five hours' time in service after the effective date of this AD unless already accomplished.
To preclude the possibility of incorrect connection being made to the engine Firex bottles, accomplish the following:
Modify the routing of the wire harness to the engine Firex bottles in accordance with Canadair Service Information Circular No. 66-CL-215, Revision A, dated August 13, 1974, or an equivalent modification approved by Chief, Engineering and Manufacturing Branch, FAA, Eastern Region.
This amendment is effective May 30, 1975.
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.