Commonwealth legislation

AD/ROBIN/11 - Carburettor Inlet Fitting

In ForceCTH

Jurisdiction

Commonwealth

Collection

legislative instrument

Plain English Summary

3/10 complexity

This AD requires owners/operators of Robin-series aeroplanes fitted with Lycoming O‑235, O‑320 or O‑360 engines to inspect the carburettor inlet fitting and follow Avions Pierre Robin Service Bulletin No. 112, with compliance by 26 May 1989. If leaks are found replace immediately; if not, replace at the next 50‑hour inspection. The operator bears inspection and replacement costs and must ensure the work meets the service bulletin to remain compliant.

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/ROBIN/11 - Carburettor Inlet Fitting.

AD/ROBIN/11 - Carburettor 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 Robin Aviation Series Aeroplanes

AD/ROBIN/11 Carburettor Inlet Fitting 7/89

Applicability: All models equipped with Lycoming O-235, O-320 or O-360 series engine. Requirement: Action in accordance with Avions Pierre Robin Service Bulletin No 112.

Note: DGAC AD 89-052(A) refers.

Compliance: By 26 May 1989.

Background: The manufacturer requires inspection and immediate replacement of the inlet fitting if leaks are detected. If no leaks are evident fitting must be replaced at next 50 hourly inspection.

Source text

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