Commonwealth legislation

AD/SM-205/20 - Main and Nose Landing Gear Torque Link Pins and Bolts - Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

The Civil Aviation Safety Authority has issued AD/SM-205/20 requiring modification of main and nose landing gear torque‑link pins and bolts on SIAI Marchetti 205 series aircraft (S/Ns 001–003, 101–399, 4‑101–4‑212), to be carried out per SIAI Marchetti SB 205B35 within 100 hours time‑in‑service after 31 July 1972. The AD imposes the obligation on aircraft owners/operators; it does not state who pays or give technical detail beyond the referenced service bulletin.

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AD/SM-205/20 - Main and Nose Landing Gear Torque Link Pins and Bolts - 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 SIAI Marchetti S205 and S208 Series Aeroplanes

AD/SM-205/20 Main and Nose Landing Gear Torque

Link Pins and Bolts - Modification Applicability: All 205 series with S/Nos. 001 to 003, 101 to 399 and 4-101 to 4-212. Document: SIAI Marchetti SB 205B35.

Compliance: With 100 hours time in service after 31 July 1972.

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Source text

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