AD/GAF-N22/26 - Rudder Tab Mass Balance Hinge Pin - Inspection
1AD/GAF-N22/26 - Rudder Tab Mass Balance Hinge Pin - Inspection
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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 GAF N22 and N24 Series Aeroplanes
AD/GAF-N22/26 Rudder Tab Mass Balance Hinge Pin - Inspection
5/79
Applicability: All models N22, N22B, N24 and N24A with Mod. N39 fitted and delivered before 1 March 1979.
Document: GAF Alert SB No. ANMD-55-6.
Compliance: Within 50 hours time in service after 16 March 1979 and thereafter at intervals not exceeding 100 hours time in service until modified in accordance with Alert SB No. ANMD-55-6.
Background: An instance has occurred where the rudder tab mass balance hinge pin seized in its bush and sheared the split pin retaining the hinge pin.