Document ID: chunk:federal_register_of_legislation:F2006B10152:body:0
Version: federal_register_of_legislation:F2006B10152
Segment Type: other
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Character Range: 0–850

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

 Gulfstream (Grumman American) GA-7 Series Aeroplanes

AD/GA-7/8 Rudder Bellcrank - Inspection and Modification NK

            Applicability: All models GA-7 with S/Nos. GA7-0002 to GA7-0093, GA7- 0096 to GA7-0099, and any model GA-7 which may have been fitted with rudder bellcrank assembly P/N 7CS10534-3 shipped from Grumman American Savannah, Georgia facility prior to 12 April 1979.

 Document: Grumman American SB No. ME-19.

 Compliance: 1. Inspect within 25 hours time in service after 4 July 1979.

            2. Modify within 100 hours time in service after 4 July 1979.

            Background: The rudder bellcrank may crack due to loads induced by wind gusts while aeroplane is parked.