AD 59-12-09

Airworthiness directive · Control Wheel Sprocket Stud · Piper PA-24 and PA-24-250

Effective
June 30, 1959
Published
June 30, 1959
Issued
June 24, 1959
Models
PA-24, PA-24-250
Data sheet
TCDS1A15
Registered aircraft
1,567 matched by model
Product
Aircraft · Small airplane

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.

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The airworthiness directive

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.)

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 1,567

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Piper1,567 aircraft
By year built
19541971
Registered aircraft by year built: 1,332 aircraft
19541
19561
19576
1958203
1959345
1960263
1961216
1962139
1963109
196444
19652
19681
19691
19711

235 with no year recorded

By model

Aircraft

See all 1,567 aircraft