Document ID: chunk:federal_register_of_legislation:F2006B05390:body:0
Version: federal_register_of_legislation:F2006B05390
Segment Type: other
Provision Reference: 
Character Range: 0–962

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

 Piper PA-18 and 19 (Super Cub) Series Aeroplanes

 AD/PA-18/11
 Amdt 1

  Lower Horizontal Stabiliser Brace Wire Fuselage Attachment Tab - Inspection and Modification

 12/81

 Applicability: All models PA-18-150 with S/Nos. 18-8602 to 18- 8109013.

 Document: Piper Service Bulletin No. 706A. (FAA AD 81-06-80 Letter of 13-3-81 refers).

            Note: Aircraft modified to Piper SB No. 706 do not require further rework.

             Compliance: 1. Unless already accomplished, inspect within 100 hours time in service after 31 December 1981.

             2. Unless already accomplished, modify within 300 hours time in service after 31 December 1981.

            Background:  Revision "A" of Piper SB introduces a revised template shape for horizontal stabiliser brace wire additional support plate.