Commonwealth legislation

AD/FU24/38 - Main Landing Gear Lower Torque Link - Modification

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Commonwealth

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legislative instrument

Plain English Summary

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This directive mandates a specific modification to the main landing gear lower torque link on Airparts (NZ) FU‑24 aeroplanes with serial numbers 139–155, to be done in accordance with Air Parts Service Bulletin No. AP61 and completed before 30 July 1971. Owners/operators bear the cost and must schedule certified maintenance to meet the fixed deadline; the Civil Aviation Safety Authority enforces compliance.

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AD/FU24/38 - Main Landing Gear Lower Torque Link - Modification

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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/FU24/38 Main Landing Gear Lower Torque Link - Modification

Applicability: All models with S/Nos. 139 to 155. Document: Air Parts SB No. AP61.

Compliance: Before 30 July 1971.

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Source text

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