AD/OH-58/1 - State of Design Airworthiness Directives

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

Legislation au F2008L02965 In force Legislative Instrument

Legislation content

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 US FAA have issued the ADs listed in Schedule 1 affecting Bell OH-58A (Bell 206A-1) series helicopters.  The USA is the State of Design for this type.  CASA has assessed the individual ADs and has issued Australian AD/OH-58/1, which will become effective on 28 August 2008.  This AD requires compliance with all applicable FAA 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 Best Practice Regulation has determined that ADs do not require a Regulatory Impact Statement.

 

The AD has been made by the Manager, Airframes in the Airworthiness Engineering Branch, on behalf of CASA, in accordance with subsection 84A (2) of the Act.


Schedule 1

 

FAA AD Number

Effective Date

Title

2005-21-03

21 November 2005

Tail Rotor Blade Root Doubler

2003-13-14

12 August 2003

Chip Detector

90-21-03

14 August 1991

Tail Rotor Blade Assembly

81-18-01 R1

15 January 2002

Trunnion

78-11-02 R1

15 December 1988

Rotor Blade Straps

76-15-03

29 July 1976

Main Rotor Blade Tension-Torsion Strap

76-04-09

30 March 1976

Main Rotor Hub Yokes

75-18-07

19 September 1975

Rotor Blade Pillow Block Assemblies

75-06-03

20 October 1975

Pitch Link Assembly

74-24-01

15 November 1974

Main Rotor Blade Grips

73-19-08

15 September 1973

Strap Fittings and Pins

72-19-01

15 September 1972

Main Rotor Retention Straps

71-08-03

18 November 1971

Particle Separation Kit

 

Interactions

Authorises

All Versions

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.