AD/BO 105/25 - State of Design Airworthiness Directives

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

Legislation au F2007L03985 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 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

 

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