Commonwealth legislation

AD/BEECH 200/3 Amdt 1 - Propeller Secondary Low Pitch Stop System

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This AD mandates a specific propeller-system modification for certain Beechcraft Model 200 (Super King Air) aeroplanes, to be performed exactly per Beechcraft Service Instruction No. 0808‑247, Rev 1, within 100 hours’ time in service after 31 May 1977. It affects owners/operators of the listed serial numbers, who must pay for the work and arrange the required Flight Manual amendment after installation.

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 200/3 Amdt 1 - Propeller Secondary Low Pitch Stop System.

AD/BEECH 200/3 Amdt 1 - Propeller Secondary Low Pitch Stop System

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 200 (Super King Air) Series Aeroplanes

AD/BEECH 200/3

Amdt 1

Propeller Secondary Low Pitch Stop System 5/77

Applicability: Models 200, S/Nos BB-2, BB-6 to BB-162.

Requirement: Action in accordance with Beechcraft SI No 0808-247, Rev 1. Compliance: Within 100 hours time in service after 31 May 1977.

Note: Flight Manual amendment is required following incorporation of this modification.

Source text

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