AD/A320/199 - A319 - State of Design Airworthiness Directives

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

Legislation au F2007L00390 Not in force Legislative Instrument

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CIVIL AVIATION ACT 1988

CIVIL AVIATION SAFETY REGULATIONS 1998

ISSUE OF AIRWORTHINESS DIRECTIVE

Under section 98 of the Civil Aviation Act 1988, the Governor-General may make regulations for the purposes of the Act and in the interests of the safety of air navigation.  Under regulation 39.001 of the Civil Aviation Safety Regulations 1998, CASA may issue airworthiness directives (ADs) for kinds of aircraft or aeronautical products.  Subregulation 39.001(5) of the Civil Aviation Safety Regulations 1998 provides that an AD is a disallowable instrument for the purposes of section 46A of the Acts Interpretation Act 1901. Therefore, in accordance with section 6 of the Legislative Instruments Act 2003, an AD is a legislative instrument.

Under Annex 8 to the Convention on International Civil Aviation, the State of Design has overall responsibility for continuing airworthiness of an aircraft type, and must provide any information necessary to ensure the continuing airworthiness of a type to appropriate States of Registry.  ADs (and their equivalents) are the most common form of continuing airworthiness information, and are issued by most ICAO Contracting States.

The State of Registry of an individual aircraft is responsible for its continuing airworthiness.  Under Annex 8, the State of Registry must develop or adopt requirements to ensure the continuing airworthiness of aircraft.  When a State of Design issues an AD against a type of aircraft on the Australian Register, CASA, as Australia’s national airworthiness authority, must assess that information and, if appropriate, issue an Australian AD to mandate the requirements of the State of Design.

The French DGAC has issued the ADs listed in Schedule 1 affecting Airbus A319 series aircraft.  France is the State of Design for these types.  CASA has assessed the individual ADs and has issued Australian AD/A320/199 which will become effective on 15 March 2007.  This AD requires compliance with all applicable DGAC ADs listed in Schedule 1.

As this AD is issued because of Australia’s obligations under Convention on International Civil Aviation, and because it is issued in response to an AD raised by the relevant State of Design, no consultation of the Australian public has taken place on this AD.  The Office of Regulatory Review has determined that ADs do not require a Regulatory Impact Statement.

The AD has been made by the Manager, New Technologies and Systems, in the Manufacturing, Certification and New Technologies Office, on behalf of CASA, in accordance with subsection 84A (2) of the Act.

 

 

 

 

Schedule 1

DGAC AD

Effective Date

Title

1996-293(B)R1

28 December 1996

Auxiliary Power Unit APIC APS 3200

1997-203-102(B)R1

18 April 1998

Probe Heater Computer

1998-152-114(B)

18 April 1998

Probe Heater Computer (ATA 30) Test Procedures

1998-451-121(B)

28 November 1998

ILS Receiver (ATA 34)

1999-361-138(B)

18 September 1999

Litton GPSSU (ATA 34)

2000-004-142(B)

22 January 2000

Rockwell Collins Radio Altimeter Software Anomalies (ATA 34)

2001-271(B)

7 July 2001

Loss of Fuel Quantity Indication on Center Tank (ATA 28)

2001-363(B)

18 August 2001

Oxygen Systems - Inspection of Oxygen Passenger Containers - (Dräeger Type I and II) (ATA 35)

 

 

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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.