Airworthiness Directives 2004 - Revocation and Remaking - Beechcraft 95 (Travelair) Series Aeroplanes

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Legislation au F2006B07754 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 95 (Travelair) Series Aeroplanes

 AD Name AD Number

 Plastic Control Wheel AD/BEECH 95/1 Amdt 2

 Main Landing Gear Indicators - CANCELLED AD/BEECH 95/2

 Main Undercarriage Up Lock - CANCELLED AD/BEECH 95/3 Amdt 3

 Ground Outside Air Temperature Indicator AD/BEECH 95/4

 Elevator Trim Tab System AD/BEECH 95/5 Amdt 2

 Starter Vibrator Wiring AD/BEECH 95/6

 Operating Restriction Placard AD/BEECH 95/7

 Pneumatic Pressure Regulator AD/BEECH 95/8

 Control Wheel Adaptor AD/BEECH 95/9 Amdt 2

 Engine Mount Bolt Nuts AD/BEECH 95/10

 Front Seat Restraint Installations AD/BEECH 95/11

 Flap Bracket AD/BEECH 95/12

 Wing Front Spar - CANCELLED AD/BEECH 95/13 Amdt 1

 Second Row Seats AD/BEECH 95/14

 Fuel System Placards AD/BEECH 95/15

 Increased Fuel Sump Capacity - CANCELLED AD/BEECH 95/16

 Tachometer and Manifold Pressure Indicators - Calibration and Engine  AD/BEECH 95/17

 Front Seat Restraint Installation AD/BEECH 95/18

 Goodyear Fuel Cells AD/BEECH 95/19

 Hatshelf Soundproofing Blanket AD/BEECH 95/20

 Fuselage Bulkheads FS 257.6 & FS 271.92 AD/BEECH 95/21

 Elevator Control Push Rods AD/BEECH 95/22

 Control Surface Trim Tab Systems AD/BEECH 95/23

 Nose Baggage Door Secondary Latch AD/BEECH 95/24

 Emergency Exits - Placards and Markings AD/BEECH 95/25

 Wing Attach Fittings, Bolts and Nuts AD/BEECH 95/26 Amdt 1

 Sponge Filled Fuel Reservoir Tanks AD/BEECH 95/27 Amdt 1

 Elevator Control Fittings AD/BEECH 95/28

 Wing Main Spar Centre Section AD/BEECH 95/29

 Elevator Trim Tab Actuator AD/BEECH 95/30

 Interior Door Handles AD/BEECH 95/31

 Flap Flex Shaft Assembly AD/BEECH 95/32

 

Overview

The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Authority, represents an effort to streamline and update the regulatory framework governing aircraft maintenance and safety standards in Australia. Enacted in 2004 by David Alan Villiers, as a delegate of the Civil Aviation Safety Authority, the legislation aimed to address gaps in the existing regulatory environment by revoking and re-making a series of airworthiness directives specific to the Beechcraft 95 (Travelair) series aeroplanes. This legislative instrument was designed to ensure that the airworthiness directives are consistent with the latest published standards, thereby enhancing the overall safety and reliability of these aircraft. While the specific objectives of the directives are not outlined in the text, the overarching policy goal appears to be maintaining high safety standards within the civil aviation sector.

Scope and Application

The Airworthiness Directives 2004 legislative instrument operates within the Commonwealth of Australia, under the authority of the Civil Aviation Safety Authority (CASA). This instrument pertains specifically to the airworthiness directives that apply to the Beechcraft 95 (Travelair) Series Aeroplanes. It revokes and re-makes a series of airworthiness directives, each identified by an AD number and name, which are listed in Schedule 1. These directives cover a range of technical and safety-related issues such as control systems, structural components, and placards, ensuring the aircraft meet specific safety standards. The application of these directives is mandatory for all aircraft operators and maintenance personnel involved with the specified Beechcraft 95 (Travelair) Series Aeroplanes. The instrument does not specify exclusions or exemptions but implies that its provisions apply universally to the listed aircraft and associated components. The application and enforcement of these directives are extended through subordinate instruments that may provide further details on compliance and implementation.

Key Provisions

The legislative instrument F2006B07754, issued by David Alan Villiers as a delegate of the Civil Aviation Safety Authority (CASA), primarily focuses on the revocation and remaking of certain Airworthiness Directives (ADs) for Beechcraft 95 (Travelair) Series Aeroplanes. This instrument operates under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. Specifically, section 3(a) of the instrument revokes the listed ADs, while section 3(b) re-makes each of these ADs as separate instruments. These ADs pertain to various components and systems of the aircraft, including the plastic control wheel, main landing gear indicators, main undercarriage up lock, ground outside air temperature indicator, and more. Each AD is re-made in the exact form as it appears in the latest published edition. The obligations imposed by this legislative instrument on the parties or entities it governs are primarily concerned with compliance with the re-made ADs. Operators and owners of Beechcraft 95 (Travelair) Series Aeroplanes must adhere to these directives, which mandate specific maintenance, inspection, and repair actions for the listed aircraft components and systems. These ADs aim to ensure the airworthiness and safety of the aircraft, and compliance is crucial to maintaining the safety standards set by CASA. Failure to comply with these ADs could result in non-compliance with aviation safety regulations, potentially leading to operational restrictions or grounding of the aircraft. The instrument also outlines the consequences for non-compliance with the re-made ADs. Section 4 details the potential offences, penalties, and civil or criminal consequences for breaches. Under the Civil Aviation Act 1988, non-compliance with ADs can result in civil penalties, including fines. The maximum penalties for such offences are substantial, reflecting the importance of airworthiness and safety in aviation. Additionally, serious non-compliance could lead to criminal charges, resulting in more severe penalties, including imprisonment. Ensuring adherence to these ADs is not only a regulatory requirement but also a critical aspect of maintaining the safety and airworthiness of Beechcraft 95 (Travelair) Series Aeroplanes.

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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.