AD/GAF-N22/43 Amdt 1 - Autopilot Aileron Servo Unit Bridle Cable Assembly P/N 1/N-45-1317 - Inspection

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

Legislation au F2006B10190 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-N22/43

Amdt 1


Autopilot Aileron Servo Unit Bridle Cable Assembly P/N 1/N-45-1317 - Inspection


8/82

 

Applicability: All models N22, N22B, N22S, N24 and N24A fitted with 2 axis autopilot (option G48, G48-24 and G48-22S) except those modified to Mod. N554 or SB NMD-27-22.

 

Document: GAF Alert SB No. ANMD-27-20.

 

Compliance: Unless previously accomplished initially inspect within 10 hours time in service after 11 September 1981 and thereafter at intervals not exceeding 120 hours time in service.

 

Background:  The autopilot aileron servo bridle cable has failed inflight on a local aeroplane causing restriction to aileron control movement. Amdt. 1 removes from the applicability those aircraft embodying Mod. 554 or SB NMD-27-22.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.