Document ID: chunk:federal_register_of_legislation:F2006B05952:body:0
Version: federal_register_of_legislation:F2006B05952
Segment Type: other
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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-38/14 Control Column Installation - Modification 11/79

 Applicability: All models PA-38-112 with S/Nos. 38-78A0001 to 38-79A1160. Document:  Piper SB No. 661.
            Compliance: Unless already accomplished, within 100 hours time in service after 30 November 1979.

            Background:  It has been reported to the manufacturer that roughness or binding of the control shaft in the instrument panel can occur at the extremes of control movement.