Document ID: chunk:federal_register_of_legislation:F2006B08739:body:0
Version: federal_register_of_legislation:F2006B08739
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Eurocopter SA 360 and SA 365 (Dauphin) Series Helicopters

AD/DAUPHIN/28 Front Passenger Door 4/91

            Applicability: Model SA 365N and N1 helicopters S/N 6220, 6229, 6306, 6310, 6315, 6324, 6340 and 6346 equipped with a partition between the cockpit and the VIP lounge.

 Requirement: Action in accordance with the technical requirements of DGAC AD 91-022-029 (B).

            Note: Aerospatiale SA 365 SB 52-11 refers.

            Compliance: As specified in the Requirement Document but with a revised effectivity date of 18 April 1991 for Australian registered helicopters.

            Background: The DGAC requires this directive to prevent the possible jettisoning of the front passenger door due to loading in the jettison linkage; caused by interference between the door covering and the partition. Effective date required by the DGAC is extended by 10 weeks.