Commonwealth legislation

AD/WILGA/3 - Tailplane to Fuselage Joint

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legislative instrument

Plain English Summary

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This AD requires owners/operators of PZL-104 WILGA 80 aircraft to carry out the corrective actions set out in PZL Mandatory Service Bulletin 10400030 to address a reported failure of the front tailplane-to-fuselage joint (Applicability; Requirement; Background). Compliance is mandatory before next flight after 17 July 2000, so operators bear the inspection and repair cost and any operational downtime; the CASA delegate enforces the requirement and references the Polish AD that prompted it (Compliance; Requirement; Background).

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Current sections

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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.

AD/WILGA/3 Tailplane to Fuselage Joint 9

AD/WILGA/3 Tailplane to Fuselage Joint 9/2000 TX

Applicability: Model PZL-104 WILGA 80 aircraft.

Requirement: Action in accordance with PZL Mandatory Service Bulletin 10400030.

Note: Polish General Inspectorate of Civil Aviation AD No. SP-0064-2000-A refers.

Compliance: Before further flight after 17 July 2000, unless already accomplished.

This Airworthiness Directive becomes effective on 17 July 2000.

Background: A failure of the front tailplane to fuselage joint has been reported. The Polish regulatory authority requires certain actions to be accomplished in order to assure the continued airworthiness of the aircraft.

Signature of David Alan Villiers Delegate of the Civil Aviation Safety Authority

David Alan Villiers

Delegate of the Civil Aviation Safety Authority 14 July 2000

View image in the official source

The above AD is notified in the Commonwealth of Australia Gazette on 17 July 2000.

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.

AD/WILGA/3 Tailplane to Fuselage Joint 9 AD/WILGA/3 Tailplane to Fuselage Joint 9/2000 TX

AD/WILGA/3 Tailplane to Fuselage Joint 9/2000 TX

Applicability: Model PZL-104 WILGA 80 aircraft.

Requirement: Action in accordance with PZL Mandatory Service Bulletin 10400030.

Note: Polish General Inspectorate of Civil Aviation AD No. SP-0064-2000-A refers.

Compliance: Before further flight after 17 July 2000, unless already accomplished.

This Airworthiness Directive becomes effective on 17 July 2000.

David Alan Villiers

Delegate of the Civil Aviation Safety Authority 14 July 2000

The above AD is notified in the Commonwealth of Australia Gazette on 17 July 2000.