AD/EMB-145/1 - State of Design ADs

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

Legislation au F2008L02101 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 Brazilian ANAC and its predecessor the DAC have issued the ADs listed in Schedule 1 affecting Embraer EMB-145 series aircraft.  Brazil is the State of Design for these types.  CASA has assessed the individual ADs and has issued Australian AD/EMB-145/1, which will become effective on 20 June 2008.  This AD requires compliance with all applicable ANAC and DAC 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, Systems and New Technologies in the Airworthiness Engineering Branch, on behalf of CASA, in accordance with subsection 84A (2) of the Act.


Schedule 1

 

Brazilian AD Number

Issue Date

Title

97-07-02R1

15 January 1998

Pilot Valve Harness Tube

97-07-12R2

11 February 2003

Dynamic Pressure Tubing of Main Pitot System

97-09-02

12 September 1997

Trust Reverser Lock Door Bracket

97-09-04

25 September 1997

Generator Cables and Hydraulic Hoses Chaffing

97-10-02

13 October 1997

MLG Shock Absorber Plain Bearing

97-10-04R1

21 July 2005

Spoilers and Speed Brake Actuators

98-01-03

15 January 1998

Hydraulic Line Tube

98-01-04

15 January 1998

Horizontal Stabilizer Anti-Icing Valve System

98-05-01R1

08 July 1999

Nose Landing Gear

98-05-02

28 May 1998

Servo and Elevator Tab Fitting Bolts

98-07-01

06 July 1998

Hydraulic Accumulators

98-09-01R1

15 March 1999

Main Landing Gear Manoeuvring Actuator

98-11-01R1

08.May.2000

Engine Bleed Line

98-12-01R1

26 May 1999

Honeywell Primus 1000 Automatic Flight Controls

1999-01-02R1

15 March 1999

Reinforcement of Wing Rib 15

1999-04-01R2

30 May 2000

Engine Bleed Air Check Valve

1999-06-01R2

19 July1999

VSI Oscillation and IAS Fluctuations

1999-09-01R2

01 May 2000

Elevator Tabs

E1999-10-01

20 October 1999

Flight Director/Autopilot

1999-12-01

03 January 2000

Placard with New Oil Pressure Limit

2000-04-01R2

28 May 2001

Engine Bleed Air Valve

E2000-05-01

25 May 2000

Spring Tab and Servo Tab Hinge Fitting

2000-06-01

03 July 2000

Lamp/Smoke Detector Cover Joints

2000-07-01

20 August 2000

Brake Control Unit

E2000-09-01

01 September 2000

GAMAH Couplings at the Fuel System Tubes

2000-09-02

16 October .2000

Engine Maximum Oil Pressure Limit

2000-10-02R2

22 February 2002

Strap Configuration of Connectors Pins IC-600

2001-01-01R1

27 March 2001

Pitch Trim Command

2001-02-01

21 February 2001

Engine Fire Extinguishing System Tubing

2001-04-01

23 Apr 2001

Engines and APU Fire Extinguisher Bottles

2001-04-02R3

13 July 2007

In-Flight APU Starts

2001-04-03

09 May 2001

EICAS and FADEC Software Versions

2001-05-01R2

22 April 2003

TAT # 2 Relay Oxidation

2001-06-03R2

24 June 2002

Stabilizer Bonding Jumpers

2001-09-01R2

08 January 2003

Engines and APU Fire Extinguishing Bottles

2001-09-03

02 October 2001

Engine Air Bleed Tube

2001-09-04

10 October 2001

ATS Output Shaft

2001-12-02R1

30 September 2005

RVSM Operation

2001-12-03R1

04 February 2002

Trunnion Fitting Web

2001-12-04R2

27 May 2002

Horizontal Stabilizer Control Unit

2002-01-01R3

08 November 2002

Elevator Control System

2002-03-01R3

06 December 2004

Nose Landing Gear Wheel Nuts

2002-05-01R2

06 January 2003

APU Exhaust Silencer

2002-06-01R1

08 November 2002

Pitot 1 and 2 Circuit Drain Valves

Brazilian AD Number

Issue Date

Title

E2002-08-01

28 August 2002

Main Landing Gear Trailing Arm Cardan

2002-10-03R2

05 January 2005

Connections of FADEC Interface Resistor Modules

2002-12-01R1

20 July 2004

Corrosion on the MLG Leg Strut Bushing Housings

E2002-12-03

20 December 2002

Electromechanical Elevators Gust Lock System

2003-01-02R1

12 March 2003

Glide Slope Antenna and Electrical Connectors

2003-03-01R1

14 October 2004

Pitch Trim System Failures

2003-06-01R1

28 July 2004

Pressure Refuelling

2003-07-01R1

23 December 2003

Air Turbine Starter

2004-01-01

27 January 2004

Additional Indication Device to the Clear Ice System

2004-01-02R2

29 November 2004

Modification of the TAT Sensor Heating System

2004-01-03

29 January 2004

Replacement of the Hydraulic Pump

2004-01-05R1

01 June 2004

Tail Boom Strobe Light Electrical Harness

2004-01-07R2

22 December 2005

Rudder II Control Rods

2004-05-02

02 June 2004

PSU Printed Circuit Board

2004-05-03R1

16 September 2005

Passenger Seat Tracks Attachment Screws

2004-10-01

30 October 2004

Engine Fire Handle Internal Circuit

2004-11-01

28 November 2004

Failure of HSCU Channels

2004-12-02R1

29 June 2005

Backup Pressure Relief Valve

2004-12-03R1

27 July 2006

Digital Flight Data Recorder (DFDR)

2005-04-02

30 April 2005

Steering System Logic

2005-04-03

30 April 2005

APU Firewall

2005-08-04R1

27 July 2006

Pitot Heating Relay

2005-08-05

06 September 2005

APU Compartment Drain System

2005-10-04

17 November 2005

Aileron Dumper Rod Ends

2006-01-01R1

23 May 2006

Passenger Seat Tracks

2006-02-01

24 February 2006

Takeoff Warnings

2006-02-03R2

08 October 2006

Electrical Bonding of the Fuel Tubings

2006-05-01

23 May 2006

Windshield Temperature Controller Power Cable Terminals

2006-07-01

31 July 2006

Cable Guard Pins of Aileron System

2007-05-01R1

04 July 2007

Rework of the Forward Fuselage Structure

2007-07-01

21 August 2007

MRBR Temporary Revision 10-5

2007-07-02

21 August 2007

MRBR Temporary Revision 10-6

2007-07-03

21 August 2007

APU Firewall

 

Overview

The Civil Aviation Act 1988 was enacted to regulate civil aviation in Australia and ensure the safety of air navigation. The Act empowers the Governor-General to make regulations for the purposes of the Act, including the issuance of airworthiness directives (ADs) by the Civil Aviation Safety Authority (CASA) to address safety issues with aircraft and aeronautical products. This legislative framework aligns with international standards set by the Convention on International Civil Aviation, ensuring that Australia meets its obligations in maintaining the continuing airworthiness of aircraft registered within its jurisdiction. CASA issues ADs based on assessments of information provided by the aircraft's State of Design, ensuring that Australian aviation safety standards are consistent with international best practices. The Civil Aviation Safety Regulations 1998 further detail the process by which CASA can issue ADs, making them legislative instruments subject to the provisions of the Legislative Instruments Act 2003. The ADs issued under this framework are a direct response to identified safety concerns, and in the case of AD/EMB-145/1, they mandate compliance with ADs issued by the Brazilian ANAC and DAC for Embraer EMB-145 series aircraft, reflecting Australia's commitment to international civil aviation safety standards. This regulatory approach ensures that all aircraft registered in Australia meet stringent safety requirements, thereby protecting public safety and maintaining the integrity of Australia's aviation system.

Scope and Application

The Civil Aviation Act 1988 and the Civil Aviation Safety Regulations 1998 establish a framework for ensuring the safety of air navigation, with a particular focus on the continuing airworthiness of aircraft. Under these legislative instruments, the Civil Aviation Safety Authority (CASA) is empowered to issue airworthiness directives (ADs) to mandate safety measures for specific types of aircraft or aeronautical products. This authority stems from section 98 of the Civil Aviation Act 1988 and regulation 39.001 of the Civil Aviation Safety Regulations 1998. ADs serve as a common mechanism for states to communicate airworthiness information, particularly when a State of Design issues such directives, necessitating their assessment and possible adoption by the State of Registry, in this case CASA. The ADs issued for Embraer EMB-145 series aircraft, originating from Brazil as the State of Design, are an example of how these regulations operate to harmonise international civil aviation safety standards. The ADs in question have been adopted by CASA and are intended to ensure compliance with Brazilian safety directives, reflecting Australia's commitment to international agreements under the Convention on International Civil Aviation. This legislative process does not require public consultation or the preparation of a Regulatory Impact Statement, given the technical nature of airworthiness directives and their alignment with international obligations. The ADs are issued by CASA under the authority granted by the Act and are considered legislative instruments, subject to disallowance under the Acts Interpretation Act 1901.

Key Provisions

The Civil Aviation Act 1988 and the Civil Aviation Safety Regulations 1998 together provide the legal framework for issuing airworthiness directives (ADs) to ensure the continuing airworthiness of aircraft. Under section 98 of the Civil Aviation Act 1988, the Governor-General may make regulations for the purposes of the Act, which in this context, is to ensure the safety of air navigation. Regulation 39.001 of the Civil Aviation Safety Regulations 1998 empowers the Civil Aviation Safety Authority (CASA) to issue ADs for kinds of aircraft or aeronautical products. These ADs are considered legislative instruments under section 6 of the Legislative Instruments Act 2003 and are disallowable instruments under section 46A of the Acts Interpretation Act 1901. The obligations imposed by the ADs are primarily on the State of Registry, which in the case of Australia is CASA. CASA must assess the airworthiness directives issued by the State of Design and, if appropriate, issue an Australian AD to mandate the requirements of the State of Design. This ensures that aircraft registered in Australia comply with international airworthiness standards. Annex 8 to the Convention on International Civil Aviation further underscores the responsibility of the State of Design to provide necessary information for continuing airworthiness and the role of the State of Registry in developing or adopting requirements to ensure the continuing airworthiness of aircraft. Failure to comply with an AD can have significant consequences. Under the Civil Aviation Act 1988, non-compliance with an airworthiness directive can result in both civil and criminal penalties. Civil penalties can include fines and other monetary penalties, while criminal penalties can include imprisonment. The exact penalties depend on the severity of the non-compliance and the discretion of the court. Additionally, failure to comply with an AD can result in the grounding of an aircraft, which can have severe operational and financial implications for the operator. Therefore, it is crucial for aircraft operators and owners to adhere strictly to the requirements set forth in these airworthiness directives to maintain the safety and airworthiness of their aircraft.

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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.