Commonwealth legislation

AD/AMD 50/26 Amdt 1 - Structure

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legislative instrument

Plain English Summary

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This Airworthiness Directive requires operators of Dassault Mystere Falcon 50 aircraft (serial numbers 253–278) to perform the structural inspections and any corrective work set out in Dassault Service Bulletin F50‑332, to be completed within 6 years and 6 months after 13 June 2002. The CASA delegate issued and enforces the requirement; aircraft owners/operators pay for inspections and repairs. The DGAC describes the inspections as addressing ageing issues: fatigue, corrosion and fretting.

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AD/AMD 50/26 Amdt 1 - Structure

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/AMD 50/26 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.

AMD Falcon 50 and 900 Series Aeroplanes

AD/AMD 50/26

Amdt 1

Structure 7/2002

Applicability: Dassault Aviation Mystere Falcon 50 Aircraft, serial numbers 253 through 278. Requirement: Action in accordance with the requirements of Dassault Aviation Service Bulletin

F50-332.

Note: DGAC AD 2002-033-039(B) R1 refers.

Compliance: Within 6 years and 6 months after 13 June 2002.

The compliance time remains unchanged by this issue. This amendment becomes effective on 11 July 2002.

Background: The DGAC requires certain inspections to address ageing aircraft issues of fatigue, corrosion, and fretting of the aircraft structure.

Amendment 1 is issued in response to a revision of the related DGAC AD which corrects an applicability serial number error.

The original issue of this Airworthiness Directive became effective on 13 June 2002.

View image in the official source

David Alan Villiers

Delegate of the Civil Aviation Safety Authority 31 May 2002

View image in the official source

The above AD is notified in the Commonwealth of Australia Gazette on 19 June 2002.

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Source text

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

1 AD/AMD 50/26 Amdt 1 - Structure

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/AMD 50/26 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.

AMD Falcon 50 and 900 Series Aeroplanes

AD/AMD 50/26

Amdt 1

Structure 7/2002

Applicability: Dassault Aviation Mystere Falcon 50 Aircraft, serial numbers 253 through 278. Requirement: Action in accordance with the requirements of Dassault Aviation Service Bulletin

F50-332.

Note: DGAC AD 2002-033-039(B) R1 refers.

Compliance: Within 6 years and 6 months after 13 June 2002.

The compliance time remains unchanged by this issue. This amendment becomes effective on 11 July 2002.

Background: The DGAC requires certain inspections to address ageing aircraft issues of fatigue, corrosion, and fretting of the aircraft structure.

Amendment 1 is issued in response to a revision of the related DGAC AD which corrects an applicability serial number error.

The original issue of this Airworthiness Directive became effective on 13 June 2002.

David Alan Villiers

Delegate of the Civil Aviation Safety Authority 31 May 2002

The above AD is notified in the Commonwealth of Australia Gazette on 19 June 2002.

Page 1 of 1