AD/G21/2 - Horizontal Stabiliser Lower Strut Fittings - Inspection and Life Limitation
1AD/G21/2 - Horizontal Stabiliser Lower Strut Fittings - Inspection and Life Limitation
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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 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.
- 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.
- Before exceeding 3200 hours time in service.