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 EASA and Direction Générale de l’Aviation Civile of France (DGAC) has issued the ADs listed in Schedules 1 and 2 affecting Eurocopter EC 225 series helicopters. France is the State of Design for these types. CASA has assessed the individual ADs and has issued Australian AD/EC 225/2 which will become effective on 22 August 2008. This AD requires compliance with all applicable EASA and DGAC ADs listed in Schedules 1 and 2.
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, Systems and New Technologies, in the Airworthiness Engineering Group, on behalf of CASA, in accordance with subsection 84A (2) of the Act.
Schedule 1
EASA AD Number | Effective Date | Title |
2006-0146 | 12 June 2006 | Engine Indicating- Torquemeter Printed Circuit Boards |
2006-0244 | 1 September 2006 | Rotor Flight Controls - Collective Lever Control |
2006-0299 | 15 October 2006 | Crash Position Indicator Interface Unit |
2006-0300 | 15 October 2006 | Crash Position Indicator ELT Water-activated Switch |
2006-0340R1 | 23 November 2006 | Equipment and Furnishings - Seal of the Jettisonable Window Panel |
2007-0115 | 11 May 2007 | Ice and Rain Protection - Main Rotor Blade De-Icing System Harness Connectors |
2007-0134 | 28 May 2007 | Main Rotor Drive - Engine-to-Main Gearbox Coupling Shaft Flange Threaded Attachment Bolt Assembly |
2007-0197-E | 26 July 2007 | Main Rotor System - M/R Hub Coning Stop Support & Dome Fairing Support Attachments |
2008-0075 | 6 May 2008 | Seat Harness Belt Buckle Blanking Plugs |
2008-0076 | 6 May 2008 | Crash Position Indicator ELT Water-activated Switch |
2008-0096-E | 28 May 2008 | Crash Position Indicator Components |
Schedule 2
DGAC AD | Effective Date | Title |
F-2007-022 | 13 November 2007 | Rotor Flight Controls - Main Servo-Controls |
F-2007-027 | 7 December 2007 | Fuselage - TGB Attachment Fittings |