Document ID: chunk:federal_register_of_legislation:F2006B09359:body:0
Version: federal_register_of_legislation:F2006B09359
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Eurocopter AS 350 (Ecureuil) Series Helicopters

AD/ECUREUIL/53 Cyclic Pitch Change Rod 11/94

            Applicability: Models B, BA, D, B1 and B2 fitted with cyclic pitch change control rod P/No 704A34-113-279, and not fitted with an auto-pilot.

 Requirement: Action in accordance with Eurocopter AS 350 Service Bulletin 01-42.

            Note: DGAC AD 94-180-069(B) refers.

 Compliance: Within 100 hours time in service after 13 October 1994.

 Background: The manufacturer has determined that some control rods may not be "in safety".