Document ID: chunk:federal_register_of_legislation:F2006B07126:body:0
Version: federal_register_of_legislation:F2006B07126
Segment Type: other
Provision Reference: 
Character Range: 0–1044

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

 Eurocopter AS 332 (Super Puma) Series Helicopters

AD/S-PUMA/5 Landing Gear Actuator Fairing 1/92

            Applicability: Model 332 helicopter, versions C, C1, L and L1 fitted with landing gear actuator fairing part numbers:

            332A21.1032, 332A21.1033, 332A21.1501, all dash numbers; and not incorporating modifications 332A07.23722 or 23723.

 Requirement: Action in accordance with the technical requirement of DGAC AD 91-206-044(B).

            Note: Aerospatiale AS 332 SB 05.35 refers.

            Compliance:  As specified in the requirement document with a revised effective date of 12 January 1991 for Australian Registered Aircraft. The effective date required by the DGAC is extended by three months.

            Background: The DGAC requires an inspection of the affected landing gear actuator fairings in order to prevent the possible loss of a fairing in flight.