AD/S-PUMA/5 - Landing Gear Actuator Fairing
1AD/S-PUMA/5 - Landing Gear Actuator Fairing
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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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.