Document ID: chunk:federal_register_of_legislation:F2006B02576:body:0
Version: federal_register_of_legislation:F2006B02576
Segment Type: other
Provision Reference: 
Character Range: 0–806

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

 Auster/Beagle A.61 Series Aeroplanes

 AD/AUS/6
 Amdt 1

 Tailplane Bracing 5/95

 Applicability: All models manufactured before January 1947.

            Requirement: Visually inspect the tailplane bracing wire strap fittings for cracks near the retaining bolts.

            Note: The pilot in command may perform, endorse and certify on the Maintenance release for this inspection.

 Compliance: Before the first flight of the day.

            This AD is effective from 27 April 1995.

 Background: Cracks have been detected in the bracing wire attachment fittings.

            This amendment allows the pilot in command to perform the inspection.