Airworthiness Directives 2004 - Revocation and Remaking - Embraer EMB-110 (Bandeirante) Series Aeroplanes

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 Airworthiness Directives 2004

 I, DAVID ALAN VILLIERS, delegate of the Civil Aviation Safety

 Authority, acting under subregulation 39.001 (1) of the Civil

 Aviation Safety Regulations 1998:

 (a) revoke the Airworthiness Directives mentioned in

 Schedule 1; and

 (b) make, as separate instruments, each Airworthiness

 Directive mentioned in Schedule 1 and attached.

 

 

 David Villiers

 Delegate of the Civil Aviation Safety Authority

 

  20 December 2004

 Note:   Each attached Airworthiness Directive is being re-made in exactly the

 same form as appears in the latest published edition of the Directive.

 


 Schedule 1 Revocation and Remaking of

 Airworthiness Directives

 Embraer EMB-110 (Bandeirante) Series Aeroplanes

 AD Name AD Number

 Emergency Exit Cover - Modification - CANCELLED AD/EMB-110/1

 Fatigue Life Limits AD/EMB-110/2 Amdt 9

 Propeller Auto Feather System - Relay Installation AD/EMB-110/3

 Wing Structural Fatigue Limitation - CANCELLED AD/EMB-110/4 Amdt 3

 Flight Control Trim System Bearings AD/EMB-110/5 Amdt 4

 Wing Upper Skin - Inspection AD/EMB-110/6

 Fire Detector Cable Terminals - Modification AD/EMB-110/7 Amdt 1

 Flap Actuators AD/EMB-110/8 Amdt 5

 Emergency Exit Lever Cover - Modification AD/EMB-110/9 Amdt 1

 Fuel Tank Alternate Vent - Removal AD/EMB-110/10

 Elevator Trim Tab and Tail Cone Clearance - Inspection AD/EMB-110/11

 Elevator Rear Bellcrank Bolts and Spring Supports - Replacement AD/EMB-110/12

 Rudder Upper Hinge Support AD/EMB-110/13 Amdt 6

 Vertical Stabiliser, Rudder Central Hinge Fitting - Modification AD/EMB-110/14

 Flap Actuators Ball Nut - Inspection AD/EMB-110/15

 Control Column P/N 4A-500-10-01-20 - Inspection AD/EMB-110/16 Amdt 2

 Fire Detector Bracket Assembly P/N 4A-513-21-02 - Modification AD/EMB-110/17

 Tailplane Deicer System - Modification AD/EMB-110/18

 Fire Extinguishing System - Wire Disconnection AD/EMB-110/19

 Primary Flight Control Cables AD/EMB-110/20 Amdt 1

 Fuel Filter Drain Hose - Replacement AD/EMB-110/21

 Rudder Pedal Assembly, Main Bearing Attachment - Inspection and Modification AD/EMB-110/22

 Trim Tab Control Systems - Inspection and Modification AD/EMB-110/23

 Control Wheel Spindle AD/EMB-110/24 Amdt 1

 Main Landing Gear Torque Link Key AD/EMB-110/25 Amdt 3

 Elevator and Rudder Trim Actuators AD/EMB-110/26 Amdt 1

 Fuselage Structure Horizontal Stabiliser Front Attachment AD/EMB-110/27 Amdt 3

 Control Surfaces - Static Balance AD/EMB-110/28 Amdt 2

 Flight Control Trim Tab Hinge Pins - Inspection and Replacement AD/EMB-110/29


 Flap Control and Protection Unit - Modification AD/EMB-110/30 Amdt 1

 Cracking of Horizontal Stabiliser Attachment Fittings AD/EMB-110/31 Amdt 7

 Elevator Front Spar - Inspection and Modification AD/EMB-110/32 Amdt 1

 Fuselage and Empennage - Inspection - CANCELLED AD/EMB-110/33

 Elevator Control Rods - Inspection and Replacement AD/EMB-110/34 Amdt 1

 Electrical Power - Generator Ground Point - Rework AD/EMB-110/35

 Elevator Trim Tab Actuation - Dual Control Rod Installation AD/EMB-110/36 Amdt 1

 Elevator Trim - CANCELLED AD/EMB-110/37

 Main Landing Gear Axle AD/EMB-110/38 Amdt 2

 Trim Tab Actuator Attachments AD/EMB-110/39 Amdt 2

 Flap Control Switch AD/EMB-110/40 Amdt 2

 Engine Electrical Connectors AD/EMB-110/41

 Undercarriage Wiring Inspection AD/EMB-110/42

 Elevator Balance Weight Arm AD/EMB-110/43 Amdt 2

 Elevator Trim Actuator Support AD/EMB-110/44 Amdt 3

 Rudder Tab System AD/EMB-110/45

 Rudder Trim Tab Actuator System AD/EMB-110/46

 Door Locking Mechanism AD/EMB-110/47 Amdt 2

 Aileron Spar AD/EMB-110/48 Amdt 1

 Nose Landing Gear Downlock Spring AD/EMB-110/49

 Automatic Propeller Feathering System AD/EMB-110/50

 Generator Control Unit Overvoltage Protection Circuit AD/EMB-110/51

 Rear Door Operating Mechanism AD/EMB-110/52

 Nose Landing Gear Rotating Cylinder Assembly AD/EMB-110/53 Amdt 1

 

Overview

The Airworthiness Directives 2004 is a legislative instrument that was enacted in 2004 by the delegate of the Civil Aviation Safety Authority under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The primary purpose of this legislation was to revoke existing Airworthiness Directives concerning the Embraer EMB-110 (Bandeirante) Series Aeroplanes and to re-issue them in an updated form. This re-issuance aimed to ensure the continued safety and airworthiness of these aircraft by incorporating the latest safety standards and modifications. The policy objective behind these directives is to maintain and enhance the safety of civil aviation by providing specific instructions and requirements for the operation and maintenance of the specified aircraft models. The Civil Aviation Safety Authority, through its delegate, took action under the authority granted by the Civil Aviation Safety Regulations 1998 to ensure that the safety directives remain current and effective. This legislative instrument specifically addresses the need to update and reissue Airworthiness Directives to reflect any changes in operational procedures, maintenance requirements, or safety concerns identified after the original directives were issued. The re-made directives are intended to provide clear and detailed instructions to aircraft operators and maintenance personnel to ensure that the Embraer EMB-110 series aeroplanes continue to meet the necessary safety standards.

Scope and Application

The Airworthiness Directives 2004, issued by David Alan Villiers as the delegate of the Civil Aviation Safety Authority (CASA) under the Civil Aviation Safety Regulations 1998, applies to the specific modifications and safety requirements of Embraer EMB-110 (Bandeirante) Series Aeroplanes operating within Australia. These directives mandate the compliance of all aircraft operators and maintenance personnel with the detailed specifications outlined in the individual Airworthiness Directives, which address various aspects of aircraft structure, systems, and components. The geographic and jurisdictional reach of these directives is limited to Australia, encompassing both Commonwealth and state jurisdictions, as they pertain to aircraft registered and operated within the country. The application of these directives is comprehensive, covering all relevant aircraft models and their respective modifications, without stated exclusions or exemptions. The authority to further extend or restrict the application of these directives is vested in subordinate instruments, ensuring that the directives remain adaptable to evolving safety standards and technological advancements in aviation.

Key Provisions

The Airworthiness Directives 2004 document, as issued by David Alan Villiers, a delegate of the Civil Aviation Safety Authority, primarily revolves around the revocation of specific Airworthiness Directives and their re-making as separate instruments, as per subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. The document references Schedule 1, which lists the specific directives that are to be revoked and remade. Each directive is re-made in the same form as the latest published edition (section 1). This action is significant as it ensures that the directives remain current and effective in maintaining airworthiness standards for the specified Embraer EMB-110 (Bandeirante) series aeroplanes. The obligations and requirements imposed by this Act are quite specific and pertain to the maintenance and inspection of various components of the Embraer EMB-110 (Bandeirante) aeroplanes. The directives cover a broad range of areas including emergency exits, fatigue life limits, propeller systems, structural components, flight control systems, and electrical systems. Each directive mandates specific actions such as modifications, inspections, replacements, and reworks to ensure the continued airworthiness of these aircraft. Compliance with these directives is crucial for operators and maintenance personnel to adhere to the highest safety standards and to prevent potential hazards. In terms of consequences for non-compliance, the Act does not explicitly state the penalties or consequences for breaching the directives within the provided text. However, given the critical nature of airworthiness directives, non-compliance could potentially lead to severe outcomes including grounding of the aircraft, enforcement actions by the Civil Aviation Safety Authority, and in severe cases, criminal charges. The exact penalties would depend on the specific breach and could range from fines to imprisonment, depending on the severity and impact of the non-compliance on aviation safety.

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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.