Commonwealth legislation

AD/ANSON/22 - Mainplane Spar Boom Joints - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This airworthiness directive requires owners/operators of Avro Anson and Avro 19 aircraft to inspect mainplane spar boom joints and replace specified bolts (per Avro TSB No. 88) before an aircraft can be issued or reissued a Certificate of Airworthiness.

After initial compliance tied to the C of A, repeat inspections are required at intervals not exceeding five years. Compliance is enforced by the Civil Aviation Safety Authority; owners/operators bear costs and scheduling impacts.

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Current sections

Direct links to the current provisions in AD/ANSON/22 - Mainplane Spar Boom Joints - Inspection.

AD/ANSON/22 - Mainplane Spar Boom Joints - 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 Avro Anson and Avro 19 Series Aeroplanes

AD/ANSON/22 Mainplane Spar Boom Joints - Inspection 10/62

Applicability: Anson and Avro 19. Document: Avro TSB No. 88.

Compliance: Inspection - Before issue of C of A and at intervals not exceeding 5 years. Bolt replacement - Before issue of C of A.

Source text

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