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

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B07126 In force Legislative Instrument

Legislation content

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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.