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 German Luftfahrt-Bundesamt (LBA) has issued AD’s listed Appendix 1 and Transport Canada Aviation (TCA) has issued AD’s listed in Appendix 2 of this Explanatory Statement affecting Eurocopter BO 105 helicopters. Germany was originally the state of design which was handed to Canada for this helicopter model. CASA has assessed the listed AD’s and has issued Australian AD/BO 105/25 which will become effective on 25 October 2007.
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 Best Practice Regulation has determined that ADs do not require a Regulatory Impact Statement.
The AD has been made by the Manager, Systems in the Airworthiness Engineering Branch, on behalf of CASA, in accordance with subsection 84A (2) of the Act.
Appendix 1
LBA AD | Effective Date | Title |
75-103 | 21 May 1975 | Quadruple Nuts – Main Rotor Head |
75-106/2 | 16 June 1975 | Hose Assemblies |
75-170/2 | 17 September 1975 | Quadruple Nuts and Bolts – Main Rotor Head |
75-171 | 5 August 1975 | Power Supply System Connector Plugs |
75-191/2 | 1 October 1975 | Load hook Release Wiring |
75-238 | 27 October 1975 | Right Outboard Engine Mount Flange |
76-136/2 | 5 October 1978 | Gearbox Supports – Service Life |
76-255/2 | 4 October 1976 | Dual Hydraulic Booster |
76-256/3 | 19 February 1980 | Rotor Brake |
77-306 | 12 December 1977 | Input Shaft and Ram Air Ventilation |
78-257 | 18 October 1978 | Dual Hydraulic System Selector Valves |
78-295/2 | 21 January 1980 | Tail Rotor Blades and Tail Rotor Heads |
79-135 | 20 March 1979 | Main Rotor Transmission Bearings |
79-136 | 14 March 1979 | Exhaust Pipe Clamps |
79-137 | 16 March 1979 | Drive Shaft Fairing – Asbestos Cloth |
79-234 | 17 May 1979 | Tail Rotor Control Linkage |
79-235/2 | 18 October 1979 | Dual Hydraulic Booster System |
79-444 | 17 October 1979 | Engine Cowling Fire Protection Paint |
80-95/2 | 11 June 1980 | Bendix Drive Shaft |
80-208 | 27 August 1980 | Main Gearbox Freewheel Shaft |
83-124/2 | 30 October 1984 | Tandem Hydraulic Units |
84-128 | 6 August 1984 | Tail Rotor Blades |
84-177/2 | 14 January 1984 | Cargo Hook |
84-178 | 5 November 1984 | Vertical Fin |
85-50 | 18 February 1985 | Control Rods |
Appendix 2.
TCA AD | Effective Date | Title |
CF-91-41 | 1 February 1992 | Torque Indication Hose |
CF-93-06 | 30 April 1993 | Continuous Ignition System |