Document ID: chunk:federal_register_of_legislation:F2006B02475:body:0
Version: federal_register_of_legislation:F2006B02475
Segment Type: other
Provision Reference: 
Character Range: 0–1112

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 355/19
 Amdt 1

 Rear RH & LH Steps 10/87

            Applicability: All Model AS 355 equipped with both raised skid-type landing gear and emergency flotation gear installations and which are not modified in accordance with Aerospatiale modification AMS 350 A07-1755.

 Requirement: Action in accordance with Aerospatiale AS 355 Telex Service 32-04A.

            Note: Bureau Veritas AD 86-32-27(B) refers.

            Compliance: Unless already accomplished, prior to 18 April 1986 and thereafter at each installation of the emergency flotation equipment.

            Background: The possibility of interference between the steps fitted to the raised skid type landing gear and the RH and LH flotation bags in the inflated configuration has been noted. This Directive requires removal of the steps to preclude flotation bag puncture.
            Amendment 1 clarifies the compliance statement.