Document ID: chunk:federal_register_of_legislation:F2006B04577:body:0
Version: federal_register_of_legislation:F2006B04577
Segment Type: other
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Character Range: 0–833

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

 Bell Helicopter Textron 212 Series Helicopters

AD/BELL 212/45 Tailboom Upper Longeron Splice 2/91

 Applicability: All model 212 helicopters S/Nos 30501 - 30999, 31101 - 31311, 32101 - 32142 and
            35001 - 35022.

 Requirement: Action in accordance with Bell Alert SB No 212-90-63 dated 20 July 1990.

            Compliance: For Part 1: Within 300 hours time in service after 24 January 1991. Repeat the inspections (Part 2) at intervals not to exceed 300 hours time in service.

            Background: Recent incidents of cracked longeron splices have created a requirement for provision of an inspection opening and repetitive inspection of the upper longeron splices.