| AD Number | 69-15-01 | Status | Active |
| Effective Date | July 21, 1969 | Issue Date | July 09, 1969 |
| Docket Number | Unknown | Amendment | 39-796 |
| Product Type | ["Aircraft"] | Product Subtype | ["Small Airplane"] |
| CFR Part | --- - Part 39 | CFR Section | --- - _EMPTY_ |
| Citation | This information is not available. | ||
| Manufacturer(s) | Piper Aircraft Inc. |
| Model(s) | PA-28-180 PA-28-235 PA-28R-180 PA-28R-200 PA-32-260 PA-32-300 |
69-15-01 PIPER: Amdt. 39-796. Applies to the following models: PA-28-180/-235, PA- 28R-180/-200, and PA-32-260/-300. The following are affected serial numbers:
PA-28-180, Serial Nos. 28-4378 through 28-5406
PA-28-235, Serial Nos. 28-11040 through 28-11257
PA-28R-180, Serial Nos. 28-30005 through 28-31095
PA-28R-200, Serial Nos. 28-35001 through 28-35265
PA-32-260, Serial Nos. 32-1111 through 32-1165
PA-32-300, Serial Nos. 32-40566 through 32-40715
Compliance required within the next 25 hours' time in service after the effective date of this AD, unless already accomplished.
To prevent control wheel retaining pin from dislodging, install a self-tapping steel screw adjacent to the retaining pin for each control wheel in accordance with Piper Service Bulletin No. 295, or equivalent approved by Chief, Engineering and Manufacturing Branch, FAA Southern Region.
This amendment becomes effective 21 July 1969.