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 Brazilian ANAC and DAC have issued the ADs listed in Schedule 1 affecting Embraer ERJ 170 series aircraft. Brazil is the State of Design for these types. CASA has assessed the individual ADs and has issued Australian AD/ERJ-170/2 which will become effective on 4 April 2007. This AD requires compliance with all applicable ANAC and DAC 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
ANAC and DAC AD | Issue Date | Title |
2004-10-02 | 30 October 2004 | Engine Fire Handle Internal Circuit |
2004-11-06 | 29 November 2004 | Hydraulic Pump Outlet Tube |
E2004-12-04 | 27 December 2004 | Temporary Loss of Display Units |
2005-02-01R1 | 24 April 2006 | Contamination of the Air Data Smart Probes |
2005-03-01R1 | 19 June 2006 | Autopilot Coupled ILS Approach Procedures |
2005-03-02 | 20 April 2005 | Aircraft Maintenance Plan |
2005-04-04 | 30 April 2005 | VHF Antenna |
2005-04-05 | 30 April 2005 | Passenger Seat Track Attachments |
2005-11-01 | 8 December 2005 | Lavatories Waste Compartment Door Latches |
2005-12-05 | 19 January 2006 | Sealing of the Negative Pressure Relief Valve |
2006-01-03 | 7 February 2006 | Fire Extinguisher Drier Metering Unit |
2006-02-04 | 15 March 2006 | Integrated Drive Generators (IDG) |
2006-03-02R1 | 27 February 2007 | Thrust Reverser |
2006-05-02 | 23 May 2006 | Emergency Evacuation Slide |
2006-05-06 | 14 June 2006 | Ram-Air Turbine (RAT) Deployment Actuator |
2006-06-01 | 28 June 2006 | Software Primus EPIC Load 17.3 Version |
2006-06-03 | 7 July 2006 | Bonding Cable Fitting Clamp of the Fuel Lines |