AD/FU24/12 - Rudder Lowr Rib - Inspection

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

Legislation au F2006B09976 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

 


Airparts (NZ) Ltd. FU 24 Series Aeroplanes

 

AD/FU24/12 Rudder Lowr Rib - Inspection 6/68

Applicability: All models not incorporating James Aviation Mod. HA/FU24/116.

 

Requirement: Detach the torque tube from the rudder and examine the rudder lower rib assembly P/N 242406 at the attachment of the rudder torque tube flange P/N 242410 for cracking and corrosion.

 

Compliance: At intervals not exceeding 500 hours time in service.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

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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.