AD 59-12-09

Active

Control Wheel Sprocket Stud

Key Information
59-12-09
Active
June 30, 1959
June 24, 1959
Unknown
N/A
Applicability
["Aircraft"]
["Small Airplane"]
Piper Aircraft Inc.
PA-24 PA-24-250
Regulatory Text

59-12-09 PIPER: Applies to PA-24 and PA-24 "250" Aircraft Serial Numbers 24-1 Through 24-764, 24-766 Through 24-779, 24-781 Through 24-820, 24-822 Through 24-842, 24- 844 Through 24-849, 24-851 Through 24-856, 24-858, 24-860 Through 24-865, 24-867 Through 24-871, 24-875, 24-878, 24-880, 24-881, and 24-885.

Compliance required not later than July 30, 1959.

Due to a recent inflight incident where control wheel sprocket stud P/N 20913-00 failed, inspect the sprocket stud P/N 20913-00 where the sprocket was attached on all aircraft that have or have had an automatic control system installed and ascertain that the stud is not cracked or twisted and the hole is not elongated. Parts found cracked or damaged are to be replaced before further operation.

(Piper Service Bulletin No. 172 covers this inspection in detail.)

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