Document ID: chunk:federal_register_of_legislation:F2006B10116:body:0
Version: federal_register_of_legislation:F2006B10116
Segment Type: other
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Character Range: 0–889

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

 Grumman G21 (Goose) Series Aeroplanes

                  AD/G21/2  Horizontal Stabiliser Lower Strut Fittings - Inspection and Life Limitation

 Applicability: All model G21A.

10/77

             Requirement: 1 Inspect the threaded portion of the strut lower adjustable end fitting P/N 12561-3 for cracks using a magnetic particle inspection technique.

            2. Retire from service strut lower adjustable end fittings P/N 12561-3.

            Note: Grumman Customer Bulletin G21A No. 3 and FAA AD 53-31-2 refer.

             Compliance: 1. Initially, before issue of Certificate of Airworthiness and thereafter at intervals not exceeding 1000 hours time in service.

            2. Before exceeding 3200 hours time in service.