Commonwealth legislation

AD/BEECH 35/34 - Turbocharger Oil Inlet Fitting

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This Act has been repealed and is no longer in force. It is retained for historical reference.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

1/10 complexity

This is a mandatory aviation safety instruction (called an Airworthiness Directive) that applies to specific Beechcraft Bonanza aeroplanes.

What it requires Owners and operators of turbocharged models V35-TC, V35A-TC, and V35B-TC must take corrective action regarding the turbocharger oil inlet fitting. The specific repair or inspection steps are contained in a manufacturer document called Beechcraft Executive Airplane Safety Communique No. 35-10.

Who must comply Anyone operating or maintaining these three specific turbocharged Beechcraft models.

Deadline The work must be completed within 100 hours of flight time (time in service) after 31 October 1972.

Why it matters This directive addresses a specific mechanical defect that could compromise the turbocharger oil system, potentially leading to engine failure. Compliance is legally mandatory to keep the aircraft airworthy and certified for flight.

JSON API

Deep dive

Want the full deep dive?

Zoe can write the in-depth analysis on top of the summary above: how it works, who it affects and what each part actually does.

Current sections

Direct links to the current provisions in AD/BEECH 35/34 - Turbocharger Oil Inlet Fitting.

AD/BEECH 35/34 - Turbocharger Oil Inlet Fitting

meta-content-style-type: text/css meta-content-type: application/xhtml+xml; charset=utf-8 meta-generator: Aspose.Words for .NET 22.10.0

?xml version="1.0" encoding="utf-8" standalone="no"?>

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 35/34 Turbocharger Oil Inlet Fitting 10/72

Applicability: Turbocharged models V35-TC, V35A-TC and V35B-TC.

Requirement: Action in accordance with Beechcraft Executive Airplane Safety Communique, No.

35-10.

Compliance: Within 100 hours time in service after 31 October 1972.

Source text

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