Document ID: chunk:federal_register_of_legislation:F2006B08410:body:0
Version: federal_register_of_legislation:F2006B08410
Segment Type: other
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
 SCHEDULE OF AIRWORTHINESS DIRECTIVES

 Cessna 525 Series Aeroplanes

AD/CESSNA 525/1 Main Landing Gear Trunnion Bearings 4/97 DM

Applicability: Model 525 Serial numbers 525-0001 to 525-0153.

             Requirement: 1. Inspect the main landing gear trunnion pins in accordance with Cessna SLA 525- 32-11.

            2. Modify in accordance with Cessna SB.525-32-08 Rev 1.

Note: FAA AD 97-01-02 refers.

             Compliance: 1. Inspect within 25 hours time in service after 19 February 1997, and thereafter at intervals not exceeding 25 hours time in service until modified.

             2. Unless already accomplished as a result of Requirement 1, modify within 75 hours time in service after 19 February 1997.

            This Airworthiness Directive becomes effective on 19 February 1997.

            Background:  This Directive is the result of a MLG collapse during landing roll out, due to trunnion bearing failure caused by loss of dry film lubricant on the MLG trunnion bearings.