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.