Document ID: chunk:federal_register_of_legislation:F2006B10276:body:0
Version: federal_register_of_legislation:F2006B10276
Segment Type: other
Provision Reference: 
Character Range: 0–1074

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

 Aircraft - General

 AD/GENERAL/45
 Amdt 2

     Mitchell Automatic Pilot Servo Bridle Cable Clamp - Replacement

 8/80

            Applicability: All aircraft fitted with automatic pilot servo bridle clamps Mitchell Part No. 42A173 or 42A184 except aircraft fitted with Piper III Series automated Flight Control System bridle clamps incorporating a safety sleeve.

            Document: 1. Edo-Aire Mitchell Service Bulletin MBI dated 1 June 1970; or 2. FAA AD 70-15-18.
            Compliance: Within 300 hours time in service after 30 September 1970 for aircraft specified in FAA AD 70-15-18. Other aircraft within 300 hours time in service after 31 January 1974.

            Background:  The applicability has been revised to exempt bridle clamps installed by Piper which have a safety sleeve fitted. (Refer to Piper Service Manual instructions for Autocontrol III and Altimatic III for details of safety sleeves).