AD 59-13-02

Airworthiness directive · Aileron Balance Weight · Piper PA-24 and PA-24-250

Published
July 9, 1959
Issued
July 1, 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

59-13-02 PIPER: Applies to Models PA-24 and PA-24 "250" Aircraft Serial Numbers 24-1 to 24-978 Inclusive and 24-980.

Compliance required within the next 100 hours of operation or by October 1, 1959, whichever occurs first.

Service experience indicates that cracks have developed in the aileron balance weight attachment bulkheads. These bulkheads are riveted to the front spar of the aileron and are the supports to which the balance weight arm is attached. To reduce the probability of failure of the aileron balance weight arm attachment install reinforced bulkheads on both ailerons except on Serial Number 24-980 replace the balance weight attachment bulkhead on right aileron only.

(Piper Service Bulletin No. 173 also covers this subject and states "Service Kit, Part Number 734-233, is available from your nearest Piper distributor or dealer free of charge if the airframe serial number is included on the purchase order.")

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
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19541971
Registered aircraft by year built: 1,332 aircraft
19541
19561
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1958203
1959345
1960263
1961216
1962139
1963109
196444
19652
19681
19691
19711

235 with no year recorded

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