Commonwealth legislation

AD/BEECH 35/55 - Ruddervator Control Push Rods

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

Owners/operators of specified Beechcraft 35‑series aeroplanes must carry out the inspections and corrective work set out in Beechcraft Service Instruction No. 0989 within 100 hours’ time‑in‑service after 30 June 1980. The directive responds to potential ruddervator pushrod misalignment/corrosion, shifting compliance costs and technical specification to operators and the manufacturer’s instruction.

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Current sections

Direct links to the current provisions in AD/BEECH 35/55 - Ruddervator Control Push Rods.

AD/BEECH 35/55 - Ruddervator Control Push Rods

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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 Beechcraft 35 (Bonanza) Series Aeroplanes

AD/BEECH 35/55 Ruddervator Control Push Rods 6/80

Applicability: All models 35, A35, B35, C35, D35, E35, F35, G35, H35, J35, K35, M35, N35, P35, S35, V35, V35-TC, V35A, V35A-TC, V35B and V35B-TC with S/Nos. D-1 to D- 10187.

Requirement: Action in accordance with Beechcraft SI No. 0989. Compliance: Within 100 hours time in service after 30 June 1980.

Background: There is a possibility that the ruddervator control pushrods may be misaligned and/or affected by internal corrosion.

Source text

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