Document ID: chunk:federal_register_of_legislation:F2006B05948:body:0
Version: federal_register_of_legislation:F2006B05948
Segment Type: other
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Character Range: 0–570

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Piper PA-38 (Tomahawk) Series Aeroplanes

AD/PA-38/10 Stabiliser/Elevator Leading Edge - Inspection
 and Modification Applicability: All models PA-38-112 with S/Nos. 38-78A0001 to 38-78A0400. Document:               1. Piper SB No. 607A, Part III; or
            2. FAA AD 78-22-01, amendment 39-3323.

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            Compliance: Unless already accomplished, within 50 hours time in service after 20 November 1978.