Document ID: chunk:federal_register_of_legislation:F2006B08062:body:0
Version: federal_register_of_legislation:F2006B08062
Segment Type: other
Provision Reference: 
Character Range: 0–1013

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

 Cessna 210 Series Aeroplanes

 AD/CESSNA 210/10
 Amdt 3

 Main Landing Gear Actuators - Modification 12/75

 Applicability: All 210 Series with S/Nos. 21058510 and below.

            Requirement: Unless previously accomplished, replace all integral flange and gear spindle assemblies, Cessna P/No. ED11935L and R, with modified splined shaft and sector listed in:

              1. Cessna SL SE69-17 - for aircraft S/No. 21058460 and below;

2.    Cessna SL SE75-21 - for aircraft S/Nos. 21058461 to 21058510.

            Compliance: For Sub-Para. 1 - Within 300 hours time in service after 29 June 1973 or at first major inspection after 1 September 1973, whichever occurs first.

            For Sub-Para. 2 - Before 1 September 1976.

            Note: Aircraft complying with DCA/CESSNA 210/10A or 10B satisfy compliance with this issue of the Directive.