Document ID: chunk:federal_register_of_legislation:F2006B04584:body:0
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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 212/52 Main Driveshaft and Tail Rotor Drive
                        Over-Temperature Indicators

 10/94

 Applicability: All model Bell 212 helicopters S/N 30501 through 30999, 31101 through 31311,
            32101 through 32142 and 35001 through 35066.

 Requirement: Action in accordance with Bell Helicopter Alert Service Bulletin 212-93-89 Rev A.

            Note: Transport Canada AD CF-94-07 dated 11 April 1994 refers.

 Compliance: As specified in the Requirement Document effective from 15 September 1994.

            Note: The Pilot in Command may carry out and certify in the maintenance release the Requirement Document Part II Serviceability Check required by this directive.

            Background:  Bell Helicopter has advised that the self adhesive temperature indicators are a more reliable means of over temperature indication than that provided by the zinc chromate primer stripe.