Document ID: chunk:federal_register_of_legislation:F2006B09981:body:0
Version: federal_register_of_legislation:F2006B09981
Segment Type: other
Provision Reference: 
Character Range: 0–885

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

 Airparts (NZ) Ltd. FU 24 Series Aeroplanes

 AD/FU24/2
 Amdt 1

 Structural Component - Corrosion - Inspection 7/68

 Applicability: All models.

            Requirement:  Inspect fuselage longerons, centre wing, main and rear spars, wing attachment fittings and other major structural components for signs of corrosion and effect any necessary repairs.

            Note: This inspection will involve dismantling the aircraft as it is not provided with sufficient inspection panels to complete inspection of the main structure.

            Compliance: At intervals not exceeding 3 years for aircraft engaged in agricultural operations. At intervals not exceeding 5 years for aircraft engaged in operations other than agricultural.