Document ID: chunk:federal_register_of_legislation:F2006B02499:body:0
Version: federal_register_of_legislation:F2006B02499
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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 355/45 Cyclic Pitch Change Rod 11/94

            Applicability: Models E, F, F1, F2 and N 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 355 Service Bulletin 01-38.

            Note: DGAC AD 94-179-051(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'.