Document ID: chunk:federal_register_of_legislation:F2006B05478:body:0
Version: federal_register_of_legislation:F2006B05478
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Piper PA-23 (Apache and Aztec) Series Aeroplanes

 AD/PA-23/51
 Amdt 1

 Landing Gear Selector Lever - Inspection 3/79

             Applicability: All models PA-23, PA-23-235 and PA-23-250 unless fitted with landing gear selector lever P/N 761-213.

             Requirement: Inspect landing gear lever P/N 752-303 for cracks in the vicinity of the two right- angle bends. Where adhesive tape has been used to secure the warning light wires to the lever, the tape shall not be replaced over the area between the bends.

             Note: Piper SB No. 635 refers to this subject.

 Compliance: At intervals not exceeding 100 hours time in service.