Commonwealth legislation

AD/ROBIN/35 - Fuel Shut-off Valve Control

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Commonwealth

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legislative instrument

Plain English Summary

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This Airworthiness Directive requires owners/operators of Robin HR 200, R2100, R2112 and R2160 aircraft that do not already have a fuel shut-off control protection device to install a guard over the fuel shut-off control in accordance with Robin Aviation Service Bulletin 180. The work must be completed within 200 flight hours of the AD becoming effective; the installation cost and scheduling are borne by aircraft owners/operators and CASA enforces compliance.

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AIRWORTHINESS DIRECTIVE

View image in the official source

View image in the official source
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Robin Aviation Series Aeroplanes

AD/ROBIN/35 Fuel Shut-off Valve Control

AD/ROBIN/35 Fuel Shut-off Valve Control 9/2001

Applicability: All Robin HR 200, R2100, R2112, R2160 series aircraft not incorporating a fuel shut- off control protection device.

Requirement: Incorporate a guard over the fuel shut-off control in accordance with Robin Aviation Service Bulletin 180.

Note: DGAC AD 2001-262(A) refers.

Compliance: Within 200 hours after the effective date of this Airworthiness Directive.

This Airworthiness Directive becomes effective on 6 September 2001.

Background: Inadvertent operation of the fuel shut-off control has occurred, resulting in loss of engine power.

Signature of Eugene Paul Holzapfel Delegate of the Civil Aviation Safety Authority

Eugene Paul Holzapfel

Delegate of the Civil Aviation Safety Authority 27 July 2001

View image in the official source

The above AD is notified in the Commonwealth of Australia Gazette on 15 August 2001.

Source text

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

AIRWORTHINESS DIRECTIVE AIRWORTHINESS DIRECTIVE

AIRWORTHINESS DIRECTIVE

For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

Robin Aviation Series Aeroplanes

AD/ROBIN/35 Fuel Shut-off Valve Control AD/ROBIN/35 Fuel Shut-off Valve Control 9/2001

AD/ROBIN/35 Fuel Shut-off Valve Control 9/2001

Applicability: All Robin HR 200, R2100, R2112, R2160 series aircraft not incorporating a fuel shut- off control protection device.

Requirement: Incorporate a guard over the fuel shut-off control in accordance with Robin Aviation Service Bulletin 180.

Note: DGAC AD 2001-262(A) refers.

Compliance: Within 200 hours after the effective date of this Airworthiness Directive.

This Airworthiness Directive becomes effective on 6 September 2001.

Background: Inadvertent operation of the fuel shut-off control has occurred, resulting in loss of engine power.

Eugene Paul Holzapfel

Delegate of the Civil Aviation Safety Authority 27 July 2001

The above AD is notified in the Commonwealth of Australia Gazette on 15 August 2001.