Airworthiness Directives 2004 - Revocation and Remaking - Beechcraft 56TC (Turbo Baron) Series Aeroplanes

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Legislation au F2006B07748 In force Legislative Instrument

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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

 Beechcraft 56TC (Turbo Baron) Series Aeroplanes

 AD Name AD Number

 Rudder Spar and Hinges AD/BEECH 56/1 Amdt 2

 Elevator Trim Tab System AD/BEECH 56/2 Amdt 2

 Cabin Door Latch AD/BEECH 56/3

 Nacelle Side Brace Ribs AD/BEECH 56/4

 Pneumatic Pressure Regulator AD/BEECH 56/5

 Centre Section Rear Spar Jack Pad AD/BEECH 56/6

 Control Wheel Adaptor AD/BEECH 56/7 Amdt 2

 Engine Mount Bolt Nuts AD/BEECH 56/8

 Fuel Vent Heater Wiring AD/BEECH 56/9

 Front Seat Restraint Installations AD/BEECH 56/10

 Main Undercarriage Up-Lock - CANCELLED AD/BEECH 56/11 Amdt 1

 Flap Bracket AD/BEECH 56/12

 Wing Front Spar - CANCELLED AD/BEECH 56/13 Amdt 1

 Second Row Seats AD/BEECH 56/14

 Fuel System - Placards AD/BEECH 56/15

 Wing Strobe Lights AD/BEECH 56/16

 Goodyear Fuel Cells AD/BEECH 56/17

 Flight Controls AD/BEECH 56/18

 Fuselage Bulkheads FS 257.6 and FS 271.92 AD/BEECH 56/19

 Elevator Control Push Rods AD/BEECH 56/20

 Control Surface Trim Tab Systems AD/BEECH 56/21

 Wing Main Spar Centre Section AD/BEECH 56/22 Amdt 2

 Elevators AD/BEECH 56/23 Amdt 1

 Nose Baggage Door Secondary Latch AD/BEECH 56/24

 Fuel Boost Pumps AD/BEECH 56/25 Amdt 2

 Emergency Exits - Placards and Markings AD/BEECH 56/26

 Rudder Pedal Arms AD/BEECH 56/27 Amdt 2

 Hawker De Havilland Restraint System AD/BEECH 56/28

 Elevator Control Fittings AD/BEECH 56/29

 Elevator Trim Tab Actuator AD/BEECH 56/30

 Wing Bolt, Nut and Fitting AD/BEECH 56/31 Amdt 2

 Flap Flex Shaft Assembly AD/BEECH 56/32

 Electroluminescent Panel Retaining Screw AD/BEECH 56/33

 

Overview

The Airworthiness Directives 2004, enacted by David Alan Villiers as the delegate of the Civil Aviation Safety Authority, aims to address the need for updated and accurate airworthiness directives for specific aircraft models. This legislative instrument revokes and re-makes various airworthiness directives related to Beechcraft 56TC (Turbo Baron) Series Aeroplanes to ensure that the latest safety standards and requirements are reflected. Each directive is remade in the same form as it appears in the latest published edition. The objective of these directives is to maintain the airworthiness of the aircraft by specifying the requirements for continued airworthiness in relation to design, construction, maintenance, and operation of the affected aircraft, thereby ensuring the safety of aviation operations.

Scope and Application

The Airworthiness Directives 2004, made under the authority of the Civil Aviation Safety Regulations 1998, apply to specific components and systems of Beechcraft 56TC (Turbo Baron) series aeroplanes. The legislation is concerned with ensuring the airworthiness of these aircraft through the revocation of existing directives and the re-making of updated versions. This directive applies to all aircraft operators, maintenance personnel, and entities involved in the manufacture or maintenance of the specified components. The geographic reach of this legislation is nationwide, as it pertains to civil aviation within Australia, falling under the jurisdiction of the Commonwealth. The legislation does not specify any exclusions or exemptions, meaning that all affected aircraft and components must comply with the updated directives. The application of the Act can be extended or restricted through subordinate instruments, which would detail specific conditions or modifications to the directives as necessary.

Key Provisions

The Airworthiness Directives 2004 (F2006B07748) outlines specific provisions for the management and compliance of airworthiness directives for various aircraft components and systems. Section 2 revokes certain existing Airworthiness Directives related to the Beechcraft 56TC (Turbo Baron) Series Aeroplanes, as detailed in Schedule 1, while section 3 re-makes these directives as separate instruments. Each directive is being re-made to match the latest published editions, ensuring that the directives remain current and relevant. These directives cover a range of components and systems, such as the rudder spar and hinges (AD/BEECH 56/1), elevator trim tab system (AD/BEECH 56/2), and cabin door latch (AD/BEECH 56/3), among others. The obligations imposed by these directives are stringent and focused on ensuring the safety and airworthiness of the specified aircraft. Operators and owners must adhere to the specific requirements and modifications outlined in each directive, which may include inspections, repairs, replacements, or alterations to aircraft components. These obligations are designed to address potential safety hazards, correct deficiencies, and ensure compliance with safety standards set by the Civil Aviation Safety Authority (CASA). Each directive provides detailed instructions and timelines for compliance, and failure to meet these requirements can result in severe consequences. The Airworthiness Directives 2004 also establishes penalties and consequences for non-compliance. Section 4 of the legislative instrument indicates that breaches of these directives can result in both civil and criminal penalties. The maximum penalties are significant and reflect the serious nature of non-compliance with airworthiness standards. Civil penalties can include substantial fines, while criminal penalties may involve imprisonment. These measures underscore the importance of strict adherence to the directives and highlight the potential legal repercussions for operators and owners who fail to comply with the mandated safety requirements. Ensuring compliance is not only a legal obligation but also a critical step in maintaining the safety and integrity of aviation operations.

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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.