AD/GA-7/8 - Rudder Bellcrank - Inspection and Modification
1AD/GA-7/8 - Rudder Bellcrank - Inspection and Modification
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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Image unavailable in extracted text 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.
- 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.