Commonwealth legislation

AD/CESSNA 210/46 - Turbocharger - Inspection

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

2/10 complexity

This airworthiness directive requires owners/operators of specified Cessna 210/T210 aeroplanes to inspect the turbocharger per Cessna SIL SE 80-24 or FAA AD 80-07-01 within 100 hours TIS after 30 June 1980. It applies to T210 S/Ns T210-0001–T210-0454 and listed 210 S/Ns, and is intended to prevent turbocharger anti-rotation pin failure and ingestion into the scavenge pump (which could disable pressure/scavenge pumps). Operators bear the cost and responsibility for inspection and any repairs.

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/CESSNA 210/46 - Turbocharger - Inspection.

AD/CESSNA 210/46 - Turbocharger - Inspection

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 Cessna 210 Series Aeroplanes

AD/CESSNA 210/46 Turbocharger - Inspection 6/80

Applicability: Model T210 S/Nos. T210-0001 thru T210-0454. Model 210 S/Nos. 21058140, 21059200 thru 21063954.

Document: 1. Cessna SIL No. SE 80-24; or

FAA AD 80-07-01, Amdt. 39-3719.

Compliance: Within 100 hours time in service after 30 June 1980.

Background: This Directive is issued to preclude a failure of the turbocharger anti-rotation pin and its ingestion into the scavenge pump. This in turn could cause a failure of the pressure and scavenge pumps.

Source text

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