AD/HS 748/23 - Aileron Operating Arm Bracket

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

Legislation au F2006B10558 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

 


British Aerospace (Hawker Siddeley) HS 748 Series Aeroplanes

 

AD/HS 748/23 Aileron Operating Arm Bracket 5/98

Applicability: All HS 748 aircraft.

 

Requirement: Action in accordance with Jetstream Aircraft Mandatory Service Bulletin HS748-27- 124.

 

Note: UK CAA AD 007-11-95 refers.

 

Compliance: Unless the initial inspection is already accomplished; within 1,000 flying hours or 6 months after 23 April 1998, whichever occurs first; thereafter as specified in the requirement document.

 

This airworthiness directive becomes effective on 23 April 1998.

 

Background: Cracks have been found in the forward flanges of the aileron operating arm bracket assembly.

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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.