Document ID: chunk:federal_register_of_legislation:F2006B08862:body:0
Version: federal_register_of_legislation:F2006B08862
Segment Type: other
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Character Range: 0–974

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

 DH 104 (Dove) Series Aeroplanes

 AD/DH 104/18
 Amdt 1

 Trim Tab Connecting Rod Eye End 11/91

 Applicability: Model DH 104 series.

            Requirement: Remove the rudder and elevators, and the rudder and elevator trim tab connecting rod assemblies; carry out an inspection for cracking of the eye ends P/N CM-2A and
            CM-2B.

            Note: Hawker Siddeley Technical News sheet CT (104) No. 187 issue 1 refers.

            Compliance: At each check 4 inspection. The compliance time of the previous issue of this Directive was at intervals not exceeding 500 hours time in service.

 Background: A cracked eye end was found on a Heron aircraft elevator trim tab connecting rod.
            The same part is fitted to Dove aircraft. This amendment extends compliance to align with Country of Origin AD.