AD/HS 748/16 - Main and Nose Landing Gear Life Limits

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

Legislation au F2006B10550 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 748/16 Main and Nose Landing Gear Life Limits 5/95

Applicability: All HS 748 aircraft.

 

Requirement: Retire from service nose and main landing gear components and associated equipment listed in Dowty Aerospace Landing Gear Service Bulletin (SB) 32-104E.

 

Compliance: Retire at the times specified in Dowty Aerospace Landing Gear SB 32-104E Tables 1 to 7 inclusive.

 

Background: The results of extensive fatigue testing indicate that a number of Structurally Significant Items on the main and nose landing gears are life limited and consequently a retirement life is specified.

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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.