Document ID: chunk:federal_register_of_legislation:F2006B10190:body:0
Version: federal_register_of_legislation:F2006B10190
Segment Type: other
Provision Reference: 
Character Range: 0–971

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

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            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.