- Published
- May 21, 1968
- Issued
- May 10, 1968
- Model
- PA-32S-300
- Data sheet
- TCDSA3SO
- Registered aircraft
- 3 matched by model
- Product
- Aircraft · Small airplane
- Amendment
- 39-602
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.
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|---|---|---|---|
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The airworthiness directive
68-01-03 PIPER: Amdt. 39-602. Applies to Model PA-32 Seaplanes, Serial Numbers 32S-40228, 32S-40229, 32S-40230, 32S-40239, 32S-40251, 32S-40263, 32S-40265, 32S-40268, 32S-40270, 32S-40272, 32S-40276, 32S-40277, 32S-40279, and 32S-40282.
Compliance required within the next 10 hours' time in service after the effective date of this AD unless already accomplished.
NOTE: Serial Numbers 32S-40230 and 32S-40268, which are presently operating in the landplane configuration, shall comply with this airworthiness directive when floats are installed.
To prevent damage to the forward and rear wing to fuselage attachment fittings, modify the float structure in accordance with the instructions contained in Piper Kit No. 760-172V, or in an equivalent manner approved by the Chief, Engineering and Manufacturing Branch, FAA Southern Region.
Effective January 11, 1968.
Revised May 21, 1968.
Affected TCDS · 1
The type certificate data sheets for the models this AD names, matched by model and maker.
Registered aircraft · 3
Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.
| 1967 | 1 |
|---|---|
| 1970 | 1 |
| 1971 | 1 |