AD 69-15-01

Active

Control Wheel Retaining Pin

Key Information
69-15-01
Active
July 21, 1969
July 09, 1969
Unknown
39-796
Applicability
["Aircraft"]
["Small Airplane"]
Piper Aircraft Inc.
PA-28-180 PA-28-235 PA-28R-180 PA-28R-200 PA-32-260 PA-32-300
Regulatory Text

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.

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References
This information is not available.
--- - Part 39
--- - _EMPTY_
Issuing Office
["AIR-720: Operational Safety Branch"]
FAA Documents