Document ID: chunk:federal_register_of_legislation:F2006B10535:body:0
Version: federal_register_of_legislation:F2006B10535
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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.