- Effective
- January 6, 1975
- Published
- January 2, 1975
- Issued
- December 20, 1974
- Model
- PA-36-285
- Registered aircraft
- 40 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-2058
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 November 21, 2025.
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 | 4f0316de…42c6c34 | FAA DRS (API key needed) |
On this page
The airworthiness directive
75-01-02 PIPER: Amendment 39-2058. Applies to Piper PA-36-285 airplanes serial numbers 36-7360001 through 36-7460026 and 36-7460034 certificated in all categories.
Compliance required within the next 50 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent possible undesirable elevator control forces accomplish the following:
Install Piper Flap Travel Modification Kit No. 760-903V in accordance with Piper Service Bulletin No. 439 or an equivalent approved by the Chief, Engineering and Manufacturing Branch, FAA Southern Region.
This amendment becomes effective January 6, 1975.
Registered aircraft · 40
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1973 | 4 |
|---|---|
| 1974 | 1 |
| 1975 | 22 |
| 1976 | 8 |
5 with no year recorded