AD/G21/3 - Horizontal Stabiliser Forward Attachment and Strut Upper Terminal - Inspection
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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Grumman G21 (Goose) Series Aeroplanes
AD/G21/3 Horizontal Stabiliser Forward Attachment
and Strut Upper Terminal - Inspection
10/77
Applicability: All models.
Requirement: 1. Inspect visually the stabiliser forward attachment fittings P/Nos. 12548 and 12093 for cracks extending radially from the outside edge of the lugs to the inside of the hole into which the shoulder bushings are pressed.
- Inspect visually, the upper terminal P/N 12561-1 of stabiliser strut P/N 12560 for cracks extending radially from the outside edge of the lugs to the inside of the hole into which the shoulder bushings are pressed.
Note: FAA AD 53-24-1 Amendment 39-1264 refers.
Compliance: 1. Initially before issue of Certificate of Airworthiness and thereafter at intervals not exceeding 50 hours time in service.
- Initially before issue of Certificate of Airworthiness and thereafter at intervals not exceeding 100 hours time in service.
Federal Register of Legislative Instruments F2006B10117