AD/A330/28 - Flight Control Primary Computer

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Legislation au F2006B02005 In force Legislative Instrument

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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 CASR 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.


 

Airbus Industrie A330 Series Aeroplanes

 

AD/A330/28 Flight Control Primary Computer 3/2004

DM

 

Applicability: All A330 series aeroplanes, all serial numbers, except for aeroplanes which have been modified as follows:

 

Airbus modification 49965 during production or Airbus Industrie Service Bulletin (SB) A330-27-3098 whilst in service (installation of flight control primary computer (FCPC) software standard P6&M14 2K1), or

 

Airbus modification 50058 during production or SB A330-27-3097 whilst in service (installation of FCPC software standard M14 2K0), or

 

Airbus modification 51341 during production or SB A330-27-3111 whilst in service (installation of FCPC software standard P6A&M14A 2K1).

 

Requirement: If not previously accomplished, amend the aircraft minimum equipment list (MEL) in accordance with the following DGAC approved temporary revisions related to the manufacturer MMEL:

 

SECTION 01: TR No. 01-27/03Z issue 2, and SECTION 02: TR No. 02-27/01Z issue 2.

Note 1: The Requirement 1 amendment may be removed from the MEL when new FCPC software standards, as specified in the Applicability Statement, are installed.

Note 2: DGAC AD F-2001-154 R2 refers.

 

Compliance: Within seven days after the effective date of this Directive.

 

This Airworthiness Directive becomes effective on 11 February 2004.

Airbus Industrie A330 Series Aeroplanes

 

AD/A330/28 (continued)

 

Background: An analysis by the manufacturer has demonstrated that if the PRIM 1 computer is inoperative, associated with dual loss of the Yellow and Blue hydraulic systems, sudden movement of the elevator may occur during the landing phase when commuting to flare law. Therefore, the manufacturer has issued a temporary revision of the Master Minimum Equipment List (MMEL) which prohibits dispatch of the aircraft with PRIM 1 computer inoperative.


James Coyne

Delegate of the Civil Aviation Safety Authority 5 February 2004

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


The above AD is notified in the Commonwealth of Australia Gazette on 11 February 2004.

Overview

The Civil Aviation Safety Authority (CASA) issued Airworthiness Directive AD/A330/28 on 5 February 2004, to address a safety issue identified in Airbus Industrie A330 series aeroplanes. The directive aims to correct an unsafe condition that could potentially lead to sudden elevator movements during landing due to a dual loss of the Yellow and Blue hydraulic systems when the PRIM 1 computer is inoperative. The directive was issued under subregulation 39.1 (1) of the Civil Aviation Safety Regulations 1998. The policy objective of the directive is to enhance the safety of the aircraft by mandating modifications to the aircraft minimum equipment list (MEL) in accordance with specific revisions approved by the French Civil Aviation Authority (DGAC). The directive became effective on 11 February 2004, requiring compliance within seven days of its publication in the Commonwealth of Australia Gazette.

Scope and Application

The Airworthiness Directive (AD) issued under subregulation 39.1(1) of the Civil Aviation Safety Regulations 1998 applies to all Airbus Industrie A330 series aeroplanes, irrespective of their serial numbers, with specific exceptions for those that have already undergone certain modifications. The directive mandates that if not previously done, the aircraft minimum equipment list (MEL) must be amended in accordance with the specified DGAC approved temporary revisions related to the manufacturer's Master Minimum Equipment List (MMEL). This requirement can be removed once new flight control primary computer (FCPC) software standards are installed, as outlined in the AD. The directive applies across the Commonwealth of Australia and becomes effective on 11 February 2004, with a compliance period of seven days from this date. The AD does not apply to A330 aeroplanes that have already been modified by specific production changes or service bulletins that install certain FCPC software standards. The application of this AD can be further detailed or extended through subordinate instruments, as necessary.

Key Provisions

The Airworthiness Directive (AD/A330/28) issued by the Civil Aviation Safety Authority (CASA) under subregulation 39.1 (1) of the Civil Aviation Safety Regulations 1998, applies to all Airbus A330 series aeroplanes except those that have already undergone specific modifications or service bulletins (section 3). The directive requires that an amendment be made to the aircraft’s Minimum Equipment List (MEL) in accordance with DGAC approved temporary revisions related to the manufacturer’s Master Minimum Equipment List (MMEL) (section 4). Specifically, the MEL must be amended to reflect the requirements of TR No. 01-27/03Z issue 2 and TR No. 02-27/01Z issue 2. This amendment must be completed within seven days of the directive becoming effective, which is on 11 February 2004 (section 5). This AD imposes obligations on the operators of Airbus A330 series aeroplanes to ensure that their MELs are updated in compliance with the directive. Operators must review and amend their MELs to reflect the changes specified in the DGAC approved temporary revisions. This involves understanding and applying the technical revisions, such as TR No. 01-27/03Z issue 2 and TR No. 02-27/01Z issue 2, to their MELs. Failure to comply with this requirement can result in the aircraft being non-compliant and potentially unsafe for operation, as the directive is aimed at preventing sudden elevator movements during landing that could arise from a specific inoperative condition. Failure to comply with the AD/A330/28 can lead to serious safety issues, as it pertains to the critical operational safety of Airbus A330 series aeroplanes. The AD indicates that non-compliance with the specified MEL amendments could result in unsafe conditions during flight operations, particularly during the landing phase. While the directive does not explicitly state specific civil or criminal penalties, non-compliance with CASA directives can generally lead to enforcement actions, including fines and potential grounding of the aircraft. The severity of the consequences depends on the nature and extent of the non-compliance, and CASA has the authority to take appropriate regulatory actions to ensure compliance and maintain aviation safety standards.

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