Document ID: chunk:federal_register_of_legislation:F2006B08202:body:0
Version: federal_register_of_legislation:F2006B08202
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Character Range: 0–1074

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

 Cessna 320 Series Aeroplanes

                            AD/CESSNA 320/23  Main Landing Gear Attachment - Inspection

 Applicability: All models 320 to 320D inclusive. Requirement:  With aeroplane on jacks:
              1. Remove Main Landing Gear Attaching "U" Bolts and Shafts.

8/75

2.    Visually inspect the "U" Bolts, with the aid of a 10X glass, in the area of the thread root ends for cracks.

3.    Visually inspect the Attaching Shafts, with the aid of a 10X glass, in the area of the roll pin hole for cracks.

             Compliance: 1. For MLG attachment shafts and "U" bolts which have achieved 2500 hours at 12 August 1975; within 100 hours time in service and thereafter at intervals not exceeding 200 hours time in service.

             2. All other MLG attachment shafts and "U" bolts; before achieving 2500 hours time in service and thereafter at intervals not exceeding 200 hours time in service.