Commonwealth legislation

AD/CESSNA 310/8 - Main Landing Gear Side Brace Link - Inspection

RepealedCTH

This Act has been repealed and is no longer in force. It is retained for historical reference.

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD mandates recurring inspections of the main landing gear side brace link on Cessna 310/310B aircraft (serial numbers below 35550 fitted with the early-style link). Owners and operators must inspect the link every 100 hours’ time-in-service using the procedures in Cessna Service Letter No. 310-34.

The requirement reduces the risk of side brace failure and potential landing gear collapse during takeoff or landing, protecting aircraft integrity and occupant safety.

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Current sections

Direct links to the current provisions in AD/CESSNA 310/8 - Main Landing Gear Side Brace Link - Inspection.

AD/CESSNA 310/8 - Main Landing Gear Side Brace Link - 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 Cessna 310 Series Aeroplanes

AD/CESSNA 310/8 Main Landing Gear Side NK

Brace Link - Inspection Applicability: All model 310 and 310B prior to S/No. 35550 fitted with early style link. Document: Cessna SL No. 310-34.

Compliance: At intervals not exceeding 100 hours time in service.

Source text

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