Document ID: chunk:federal_register_of_legislation:F2006B09073:body:0
Version: federal_register_of_legislation:F2006B09073
Segment Type: other
Provision Reference: 
Character Range: 0–628

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

 DHC-3 (Otter) Series Aeroplanes

AD/DHC-3/24 Main Landing Gear Fuselage Attachment Bolts 3/69

 Applicability: All models.

            Requirement: Remove and inspect using a magnetic particle method main landing gear to fuselage attachment bolts P/Ns C3U72-3 and C3U142-5 for cracking particularly around the grease outlet hole.

            Compliance: Within 100 hours time in service after 15 April 1969 and thereafter at intervals not exceeding 500 hours time in service.