Document ID: chunk:federal_register_of_legislation:F2006B09032:body:0
Version: federal_register_of_legislation:F2006B09032
Segment Type: other
Provision Reference: 
Character Range: 0–902

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

 DHC-2 (Beaver) Series Aeroplanes

 AD/DHC-2/15
 Amdt 1

 Applicability: All models.

       Main Undercarriage Lower Forward Bolt Attachment - Inspection

 8/84

            Requirement: Inspect the main undercarriage lower forward attachment bolts for cracking as follows:

              1. P/N C2U-487ND (part of bolt assembly No. C2U-185A) : magnetic particle inspect in accordance with ANO 108.8 or fluorescent penetrant inspect in accordance with ANO 108.10.

2.    P/N 02-B-16 (hard chrome plated bolts): fluorescent penetrant inspect in accordance with ANO 108.10.

            Compliance: At intervals not exceeding 100 hours time in service for aircraft engaged in agricultural operations, and 500 hours time in service for other aircraft.