AD/GAF-N22/26 - Rudder Tab Mass Balance Hinge Pin - Inspection

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B10173 In force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


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.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.