Document ID: chunk:federal_register_of_legislation:F2006B05957:body:0
Version: federal_register_of_legislation:F2006B05957
Segment Type: other
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Character Range: 0–740

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-38/19 Aileron Balance Weight Rib - Inspection 11/81

 Applicability: All models PA-38-112 with S/Nos. 38-78A0001 to 38-81A0051 and 38-81A0105. Document:               Piper SB No. 723.
            Compliance: Within 25 hours time in service after 22 September 1981, and thereafter at intervals not exceeding 100 hours time in until modified by incorporation of Piper Kit P/N 764 140.

            Background: The manufacturer has received reports of cracks developing in flange area of the aileron balance weight rib P/Nos. 77342-16 and -17.