Commonwealth legislation

AD/FU24/12 - Rudder Lowr Rib - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD requires licensed maintenance personnel to detach the rudder torque tube and inspect the rudder lower rib assembly (PN 242406) on Airparts FU 24 series aeroplanes for cracking and corrosion, at intervals not exceeding 500 hours TIS. It affects FU 24 operators, owners and maintenance organisations (unless James Aviation Mod HA/FU24/116 is installed), creating recurring inspection costs and potential repair expenses while aiming to detect defects before they pose a safety risk.

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AD/FU24/12 - Rudder Lowr Rib - Inspection

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

View image in the official source 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.

Source text

Sourced from the Federal Register of Legislation (legislation.gov.au), CC BY 4.0.