Document ID: chunk:federal_register_of_legislation:F2006B05338:body:0
Version: federal_register_of_legislation:F2006B05338
Segment Type: other
Provision Reference: 
Character Range: 0–893

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

 Partenavia P68 Series Aeroplanes

 AD/P68/11
 Amdt 1

      Rudder Control Pulleys at Fuselage Frame No. 3 - Inspection

 5/82

            Applicability: All models P68 and P68B with S/Nos. referenced in Partenavia SB No. 40 Rev. 1 or with S/Nos. referenced in subsequent issues or revisions of that SB.

 Document: Partenavia SB No. 40, Rev. 1.

            Note: RAI AD 78-181/P68-17 refers.

 Compliance: As detailed in the requirement document.

            Background: Incidents have occurred where frame 3 has been found cracked and rivets working where the mounting brackets for rudder control cable pulleys are attached to this frame. This Revision results from an extension of compliance times for initial and repeat inspections.