AD/B737/285 Amdt 1 - State of Design Airworthiness Directives

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

Legislation au F2006L02526 Not 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 United States FAA has issued ADs listed in Schedule 1 affecting Boeing model 737-100 and 737-200 series aircraft.  The United States is the State of Design for these types.  Since the issue of AD/B737/285 CASA has identified additional applicable FAA ADs, CASA has assessed the individual ADs and has issued Australian AD/B737/285 Amdt 1, which will become effective on 31 August 2006.  This AD, which requires compliance with all applicable FAA ADs listed in Schedule 1, cancels and replaces the previous issue.

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

FAA AD Number

Effective Date

Title

79-26-02

31 December 1979

Ground Proximity Warning System Flap Position Switches

83-01-05 R2

4 August 1986

Engine Starter Operation Indication

85-02-03

1 March 1985

Runaway Stabiliser Trim

89-22-04

23 October 1989

Fuselage Inspection

92-08-06

29 May 1992

Sperry SP177 Autopilot Flight Control Computers and Mode Control Panels

96-23-04

19 December 1996

Static Inverters

2001-16-11

25 September 2001

Carriage Spindles

2001-24-33

16 January 2002

Auxiliary Power Unit Generator Power Feeder Wire Bundle

 

 

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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.