AD/A320/134 - Fixed Lateral Cockpit Window

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B01881 In force Legislative Instrument

Legislation content

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 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.

 

Airbus Industrie A319, A320 and A321 Series Aeroplanes

 

AD/A320/134 Fixed Lateral Cockpit Window 3/2002

 

Applicability:  All Model A319, A320, and A321 aircraft, fitted with PPG Aerospace fixed lateral cockpit window part number NP-165313-1 or NP-165313-2 having a serial number below 95001H0001 (PPG Aerospace manufacturing date before January 1995).

 

Requirement: 1. Action in accordance with Airbus Industrie Service Bulletin A320-56-1009.

 

2. Windows found suspect must be re-inspected, and replaced if necessary, in accordance with Airbus Industrie Service Bulletin A320-56-1009.

 

Note: DGAC AD 2001-632(B) refers.

 

Compliance: 1. Within 500 flight hours after 21 March 2002, unless already accomplished.

 

2. Repeat at intervals not to exceed 500 flight hours, until replacement. This Airworthiness Directive becomes effective on 21 March 2002.

Background: The DGAC received an in-service report of outer glass ply separation from a fixed lateral cockpit window. Investigation revealed a deficient manufacturing process resulted in moisture ingress between the centre and outer glass ply.


 

David Alan Villiers

Delegate of the Civil Aviation Safety Authority 8 February 2002

 

 

 

 

 

 

 

 

 

 

The above AD is notified in the Commonwealth of Australia Gazette on 27 February 2002.

 


Page 1 of 1

Overview

The Civil Aviation Regulations 1998, as amended, include specific Airworthiness Directives to ensure the safety of aircraft in Australian airspace. One such directive, AD/A320/134 issued on 21 March 2002, pertains to Airbus Industrie A319, A320, and A321 series aeroplanes equipped with certain fixed lateral cockpit windows. This directive was enacted in response to a reported issue of outer glass ply separation in the cockpit windows, traced back to a manufacturing defect that allowed moisture ingress. The directive was issued by the Civil Aviation Safety Authority (CASA) to mandate corrective actions to address the unsafe condition and ensure compliance with safety standards. CASA delegates the authority to enforce this directive under subregulation 39.1 (1) of the Civil Aviation Regulations 1998, with the overarching policy objective being the enhancement of aviation safety by mitigating identified risks associated with the specified aircraft components.

Scope and Application

The Civil Aviation Regulations 1998, as amended, apply to all aircraft operating within Australian airspace and cover a broad range of safety and operational requirements. Specifically, the Airworthiness Directive (AD) issued under Part 39, section 105, addresses the safety of aircraft and aeronautical products through mandatory safety measures. This particular AD applies to all Airbus Industrie A319, A320, and A321 series aeroplanes that are fitted with certain fixed lateral cockpit windows manufactured by PPG Aerospace before January 1995. The directive mandates corrective actions to address the identified unsafe condition of potential moisture ingress between the centre and outer glass ply, which could lead to outer glass ply separation. Compliance with the AD requires that specified actions be taken within 500 flight hours after 21 March 2002, and subsequently at intervals not exceeding 500 flight hours, until the windows are replaced. The AD is effective from 21 March 2002 and is applicable nationally across Australia, as it is issued under the authority of the Civil Aviation Safety Authority (CASA).

Key Provisions

The main sections of the Civil Aviation Regulations 1998, Part 39, specifically focusing on the Airworthiness Directive for Airbus Industrie A319, A320, and A321 Series Aeroplanes (AD/A320/134), are the applicability, requirement, and compliance sections. The applicability section (1) specifies that the AD applies to all A319, A320, and A321 aircraft equipped with PPG Aerospace fixed lateral cockpit windows part numbers NP-165313-1 or NP-165313-2, provided these parts have a serial number below 95001H0001, indicating a manufacturing date before January 1995. The requirement section (2) mandates two actions: first, the implementation of Airbus Industrie Service Bulletin A320-56-1009, and second, that windows identified as suspect must be re-inspected and replaced if necessary, again in accordance with the same service bulletin. The compliance section (3) sets out that these actions must be completed within 500 flight hours following 21 March 2002, unless already performed, and must be repeated at intervals not exceeding 500 flight hours until the issue is fully resolved. The obligations and requirements imposed by this AD on the relevant parties include adhering to the specified maintenance and inspection protocols as detailed in Airbus Industrie Service Bulletin A320-56-1009. This involves identifying affected aircraft, conducting necessary inspections of the fixed lateral cockpit windows, and replacing any windows found to be defective. Operators must ensure that these actions are completed within the stipulated timeframes and repeated as necessary to maintain airworthiness standards. Additionally, operators must maintain records of compliance to demonstrate adherence to the AD. Failure to comply with the AD could lead to serious safety implications, potentially resulting in civil and criminal penalties. While the specific penalties are not detailed in the AD itself, under the Civil Aviation Act 1988, non-compliance with ADs can result in significant fines and potential criminal charges for operators. The severity of penalties can vary based on the nature and extent of the non-compliance, but the overarching intent is to ensure that all safety directives are strictly followed to prevent unsafe conditions from compromising flight safety.

Legal classification tags

Area of Law
Administrative Law
Instrument
Legislative Instrument
Concepts
Definitions & Interpretation
Compliance Obligations
Enforcement Powers

Interactions

Authorises

All Versions

Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.