Commonwealth legislation

AD/BN-2/67 Amdt 1 - Control Column Sliding Tube

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Jurisdiction

Commonwealth

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legislative instrument

Plain English Summary

2/10 complexity

This AD requires owners/operators of Pilatus Britten Norman BN‑2 series (BN2, BN2A, BN2B, BN2T) to inspect the control column sliding tube following B‑N Group Mandatory Service Bulletin BN2/SB.243 Issue 2, with initial compliance before 8 September 2002 and repeat inspections at intervals not to exceed 500 hours if no wear is found. CASA's delegate adopted the measure after manufacturer reports of wear that could cause cracking. Owners/operators bear inspection and repair costs; corrective work must follow the Service Bulletin (Requirement; Compliance; Background).

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AD/BN-2/67 Amdt 1 - Control Column Sliding Tube

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

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AIRWORTHINESS DIRECTIVE

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For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/BN-2/67 and issues the following 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.

Pilatus Britten Norman BN-2 Series Aeroplanes

AD/BN-2/67

Amdt 1

Control Column Sliding Tube 8/2002

Applicability: All Model BN2, BN2A, BN2B, and BN2T aircraft.

Requirement: Action in accordance with B-N Group Ltd Mandatory Service Bulletin BN2/SB.243 Issue 2.

Compliance: Before 8 September 2002; thereafter at intervals not to exceed 500 hours time in service, if no wear is found. If wear is found refer to the Requirement document.

This Amendment becomes effective on 8 August 2002.

Background: The manufacturer received reports of wear in the control column sliding tube. This wear could lead to cracking of the tube.

Amendment 1 is issued in response to a revision of the Requirement document, which introduces changes to Accomplishment Instructions procedures.

The original issue of this Airworthiness Directive became effective on 17 June 1999.

View image in the official source

David Alan Villiers

Delegate of the Civil Aviation Safety Authority 28 June 2002

View image in the official source

The above AD is notified in the Commonwealth of Australia Gazette on 17 July 2002.

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Source text

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

1 AD/BN-2/67 Amdt 1 - Control Column Sliding Tube

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

AIRWORTHINESS DIRECTIVE

For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/BN-2/67 and issues the following 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.

Pilatus Britten Norman BN-2 Series Aeroplanes

AD/BN-2/67

Amdt 1

Control Column Sliding Tube 8/2002

Applicability: All Model BN2, BN2A, BN2B, and BN2T aircraft.

Requirement: Action in accordance with B-N Group Ltd Mandatory Service Bulletin BN2/SB.243 Issue 2.

Compliance: Before 8 September 2002; thereafter at intervals not to exceed 500 hours time in service, if no wear is found. If wear is found refer to the Requirement document.

This Amendment becomes effective on 8 August 2002.

Background: The manufacturer received reports of wear in the control column sliding tube. This wear could lead to cracking of the tube.

Amendment 1 is issued in response to a revision of the Requirement document, which introduces changes to Accomplishment Instructions procedures.

The original issue of this Airworthiness Directive became effective on 17 June 1999.

David Alan Villiers

Delegate of the Civil Aviation Safety Authority 28 June 2002

The above AD is notified in the Commonwealth of Australia Gazette on 17 July 2002.

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