AD/GAF-N22/27 - Rudder Tab - Modification

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

Legislation au F2006B10174 In force Legislative Instrument

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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-N22/27 Rudder Tab - Modification 8/79

Applicability: All models N22 and N22B not modified in accordance with GAF SB No. NMD-27-3, Rev. 1.

 

Requirement: Modify in accordance with GAF SB No. NMD-27-3, Rev. 1.

 

Note: The speed of 180 Kts IAS should not be exceeded on aircraft not yet modified.

 

Compliance: Before 1 December 1979.

 

Background:  Manufacturer’s tests indicate that wear and backlash which may develop in the rudder tab system during normal service may erode the tab/rudder flutter speed margins.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.