Document ID: chunk:federal_register_of_legislation:F2006B08092:body:0
Version: federal_register_of_legislation:F2006B08092
Segment Type: other
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Character Range: 0–824

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

 Cessna 210 Series Aeroplanes

 AD/CESSNA 210/43
 Amdt 1

 Alternator Ground Strap - Installation 9/82

            Applicability: All model 210/P210/T210 with S/Nos. 21058783 to 21062666 except 21062650 and 21062662, P21000001 to P21000026, T210-0001 to T210-0454.

 Document: 1. Cessna SIL SE79-59; or

            2. FAA AD 79-25-07.

 Compliance: 1. Within 100 hours time in service after 31 March 1982.

            2. Each time an engine is installed in an aircraft following initial compliance.

            Background: Compliance has been amended by item 2 due to reports from industry that ground straps are being omitted from refitment on engine reinstallations.