Commonwealth legislation

AD/BEECH 65/12 - Rudder Spar and Hinges - Inspection and Modification

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This Airworthiness Directive requires owners/operators of specified Beechcraft Queen Air aeroplanes (models A65/A65-8200 s/n LC-240–LC-319 and 65-80/65-A80/65-B80 s/n LD-1–LD-398) to inspect the rudder spar and hinges every 100 flight hours until completing a mandated modification by 1 Aug 1969. Compliance follows Beechcraft Service Instruction No. 0101-135; operators bear the costs and scheduling burden of recurring inspections and the required modification.

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 65/12 - Rudder Spar and Hinges - Inspection and Modification.

AD/BEECH 65/12 - Rudder Spar and Hinges - Inspection and Modification

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 65 and 70 (Queen Air) Series Aeroplanes

AD/BEECH 65/12 Rudder Spar and Hinges - Inspection

and Modification

5/69

Applicability: Models A65 & A65-8200 with S/Nos. LC-240 to LC-319. Models 65-80, 65-A80 & 65-B80 with S/Nos. LD-1 to LD-398.

Document: Beechcraft SI No. 0101-135.

Compliance: 1. Inspect within 100 hours’ time in service after 12 May 1969 and thereafter at intervals not exceeding 100 hours’ time in service until modified.

Modify before 1 August 1969.

Source text

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