Document ID: chunk:federal_register_of_legislation:F2006B02483:body:0
Version: federal_register_of_legislation:F2006B02483
Segment Type: other
Provision Reference: 
Character Range: 0–1132

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

 Eurocopter AS 355 (Twin Ecureuil) Series Helicopters

 AD/AS 355/3 Tail Rotor Blades, Bonding Separation of Stainless
                  Steel Leading Edge Protectors - Inspection

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 Applicability: All model AS 355 helicopters fitted with tail rotor blades 350A.12.0030.00 to .05. Requirement:              Action in accordance with Aerospatiale Workcard AS 355 No. 64.10.00.601.
            Note: Bureau Veritas AD 82-25-4(B) refers.

 Compliance: A.  For blades between 0 and 100 hours time in service since new or overhaul:

                Before further flight and thereafter at intervals not exceeding 10 hours time in service until accumulation of 100 hours time in service.

                B. For blades with more than 100 hours time in service since new or overhaul: Within 10 hours time in service after 24 March 1982.
            Background: The manufacturer has reported several cases of severe bonding separation of the leading edge stainless steel protectors.