Document ID: chunk:federal_register_of_legislation:F2006B04180:body:0
Version: federal_register_of_legislation:F2006B04180
Segment Type: other
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Character Range: 0–590

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

 Beechcraft 76 (Duchess) Series Aeroplanes

AD/BEECH 76/5 Main Landing Gear Fork Pin 8/79

 Applicability: All model 76 with S/Nos. ME-1 to ME-228. Requirement:  Action in accordance with Beechcraft SI No. 1073.
 Compliance: Within 50 hours' time in service, unless already accomplished, after 28 August 1979.

            Background: Failure of the existing fork pin retaining pin could result in separation of the wheel and fork assembly.