Airworthiness Directives 2004 - Revocation and Remaking - Beechcraft 1900 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

 Beechcraft 1900 Series Aeroplanes

 AD Name AD Number

 Stabiliser and Fin Moisture Sealing AD/BEECH 1900/1

 Nose Gear Lower Shock Absorber Assembly AD/BEECH 1900/2

 Wing Fasteners AD/BEECH 1900/3

 Engine Truss Assembly AD/BEECH 1900/4 Amdt 2

 Right Circuit Breaker Wire Bundle Clamp AD/BEECH 1900/5

 Instrument Air System - CANCELLED AD/BEECH 1900/6

 Compressor Turbine Blades - CANCELLED AD/BEECH 1900/7 Amdt 2

 Pilot and Co-Pilot Chair Locking Mechanism AD/BEECH 1900/8 Amdt 1

 Electrical Power - Hot Battery Bus AD/BEECH 1900/9

 Elevator Trim Tab Control Cable AD/BEECH 1900/10

 Fuselage Canted Bulkhead AD/BEECH 1900/11

 Pneumatic Air System Plumbing AD/BEECH 1900/12

 Cabin Partition AD/BEECH 1900/13

 Pilots and Co-Pilots Windshields AD/BEECH 1900/14

 Engine Fuel Filter Bypass Valve AD/BEECH 1900/15

 Exterior Operating Instruction Placards for External Doors AD/BEECH 1900/16 Amdt 1

 Stabilon Attachment Angle AD/BEECH 1900/17

 Outboard Flap Attachment Brackets and Aft Roller Bearings AD/BEECH 1900/18 Amdt 2

 Under Torqued Propeller Mounting Bolts AD/BEECH 1900/19

 Airstair Door Handle and Latch Housing AD/BEECH 1900/20 Amdt 1

 Vent Blower Assemblies - CANCELLED AD/BEECH 1900/21

 Main Landing Gear Actuator Rod Ends AD/BEECH 1900/22

 Radio Switching Panel AD/BEECH 1900/23

 Ground Fine Switch AD/BEECH 1900/24

 Emergency Exit Doors AD/BEECH 1900/25

 MLG Actuator End Cap AD/BEECH 1900/26

 Inspection for Flight Control Interference with Wiring AD/BEECH 1900/27

 Cabin Oxygen Mask Lanyards AD/BEECH 1900/28

 Electric Trim Servo Cover AD/BEECH 1900/29


 Electrical Loom Inspection AD/BEECH 1900/30

 Landing Gear Emergency Hand Pump - Faulty Component Replacement AD/BEECH 1900/31

 Wing Fuel Quantity Wiring Harness AD/BEECH 1900/32

 Cockpit Voice Recorder Audio Amplifier AD/BEECH 1900/33

 KLN-90B GPS AD/BEECH 1900/34

 KA-33 Cooling Blower AD/BEECH 1900/35

 Flap Flexible Driveshaft Assembly AD/BEECH 1900/36

 Elevator Balance Weight Attachment AD/BEECH 1900/37

 Elevator Control System AD/BEECH 1900/38

 AC Inverters and Synchronisation Wire AD/BEECH 1900/39

 Fuselage Rivets AD/BEECH 1900/40

 Elevator Trim System AD/BEECH 1900/41

 Ventilation Blower Assemblies AD/BEECH 1900/42

 Canted Bulkhead at FS588.10 AD/BEECH 1900/43

 Landing Gear Circuit Breaker AD/BEECH 1900/44

 Engine Controls Cross Shaft AD/BEECH 1900/45

 

Overview

The Airworthiness Directives 2004 is a legislative instrument made under the authority of the Civil Aviation Safety Authority (CASA) to address the need for updated airworthiness directives for specific aircraft models. Enacted in 2004, the instrument revokes existing airworthiness directives pertaining to the Beechcraft 1900 series aeroplanes and re-makes them as separate instruments. The enactment aimed to ensure that the directives align with the latest safety standards and regulatory requirements, thereby enhancing the overall airworthiness and safety of the aircraft in question. The policy objective behind this legislative action was to maintain and improve the safety of civil aviation in Australia by ensuring that all airworthiness directives are current and reflect the most recent safety findings and technological advancements.

Scope and Application

This legislative instrument, titled "Airworthiness Directives 2004", operates within the framework of the Civil Aviation Safety Regulations 1998 and applies to the aviation industry, specifically targeting the maintenance and operational standards of Beechcraft 1900 Series aeroplanes. It is enacted by David Alan Villiers, a delegate of the Civil Aviation Safety Authority, who is authorised under subregulation 39.001(1) of the Civil Aviation Safety Regulations 1998. The scope of the legislation encompasses the revocation of previously issued Airworthiness Directives and their re-issuance to ensure consistency with the latest published versions. The directive's jurisdictional reach is confined to Australia, given that it is issued under the authority of the Australian Civil Aviation Safety Regulations. The instrument does not specify exclusions, exemptions, or thresholds, and its application extends to all operators and entities that own or operate Beechcraft 1900 Series aeroplanes within Australia. The detailed directives in Schedule 1 cover a range of aircraft components and systems, ensuring that each aspect of the aircraft's airworthiness is subject to specific regulatory oversight and maintenance requirements.

Key Provisions

The primary operative sections of this legislative instrument involve the revocation and remaking of existing Airworthiness Directives (ADs) for specific aircraft models, in this case, the Beechcraft 1900 series aeroplanes (section 1(a) and 1(b)). These directives are detailed in Schedule 1 and are re-made as separate instruments in the exact form as they appear in the latest published edition. This includes the re-making of ADs that were previously cancelled, such as AD/BEECH 1900/6 and AD/BEECH 1900/7, and the amendment of others like AD/BEECH 1900/8 Amdt 1 and AD/BEECH 1900/16 Amdt 1. The directives address various components and systems of the aircraft, including the stabilisation fin, nose gear, wing fasteners, engine truss assembly, and more, ensuring compliance with the latest safety standards. The Act imposes specific obligations and requirements on the entities it governs, primarily focusing on the maintenance and safety of the Beechcraft 1900 series aeroplanes. Operators and maintenance providers must adhere to the detailed instructions and specifications outlined in the re-made ADs. This includes conducting inspections, making necessary repairs, and ensuring that all aircraft modifications comply with the latest safety standards. The ADs provide clear, step-by-step guidance on what must be done, who is responsible for the tasks, and the timeframes within which these tasks must be completed. This ensures that all stakeholders are fully aware of their responsibilities and the safety measures that need to be implemented. The legislation also outlines potential offences, penalties, and civil or criminal consequences for breaches of the ADs. While specific penalties are not detailed within the text, it is clear that non-compliance with the ADs could lead to serious repercussions. For instance, failure to adhere to the requirements could result in the aircraft being deemed unairworthy, which could lead to grounding of the aircraft and potential criminal charges against those responsible. The maximum penalties for such offences could include substantial fines and imprisonment, depending on the severity of the breach and its impact on aviation safety. These provisions underscore the importance of strict compliance with the ADs to ensure the safety and airworthiness of the aircraft in question.

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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.