AD/HS 125/92 - Nose Gear Pivot Pin

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

Legislation au F2006B10535 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 BAe 125 Series Aeroplanes

 

AD/HS 125/92 Nose Gear Pivot Pin  7/88 DM

 

Applicability: All models.

 

Requirement: Action in accordance with BAe-125 SB 32-217.

 

Note: CAA AD 008-02-88 refers.

 

Compliance: For components with more than 4000 landings, prior to 31 August 1988. For components with less than 4000 landings, before exceeding 4000 landings.

 

Background:  Recent analysis by the manufacturer has resulted in a requirement to crack detect pivot pins fitted to all nose leg assemblies which have achieved or exceeded 4000 landings.

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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.