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 18 Series Aeroplanes
AD Name AD Number
Starter Solenoid and Main Bus Lead Wire - Inspection AD/BEECH 18/1
Landing Gear Retracting Mechanism - Inspection AD/BEECH 18/2
Fuel Tank Gasket - CANCELLED AD/BEECH 18/3
Horizontal Stabiliser Spar - Inspection AD/BEECH 18/4 Amdt 1
Wing Centre Section Spar Chafing - Inspection AD/BEECH 18/5
Centre Section Truss - CANCELLED AD/BEECH 18/6
Control Wheel Shaft - Modification AD/BEECH 18/7
Undercarriage Limit Switch - Inspection AD/BEECH 18/8
Centre Spar and Landing Gear - CANCELLED AD/BEECH 18/9
Lower Outer Wing Root Fittings - CANCELLED AD/BEECH 18/10
Mainplane Lower Main Spar Tube - CANCELLED AD/BEECH 18/11 Amdt 1
Centre Section Lower Main Spar - CANCELLED AD/BEECH 18/12
Centre Section Truss Clusters - CANCELLED AD/BEECH 18/13
Outer Mainplane - CANCELLED AD/BEECH 18/14 Amdt 3
Wing Centre Section - CANCELLED AD/BEECH 18/15 Amdt 10
Front Seat Restraint Installations - Modification AD/BEECH 18/16
Aircraft Modification, Inspection and Retirement AD/BEECH 18/17 Amdt 4
Control Columns and Elevator Control Arm Assembly - Inspection AD/BEECH 18/18 Amdt 1
Goodyear Fuel Cells - Inspection AD/BEECH 18/19
Lower Rudder Torque Tube - Inspection AD/BEECH 18/20
Main Landing Gear Walking Beam Upper Attach Bolt - Inspection and AD/BEECH 18/21
Main Landing Gear Drag Legs, Drag Leg Bolts and Retract Slide Assemblies - AD/BEECH 18/22
Pilot Seats - Reinforcement AD/BEECH 18/23
Overview
The Airworthiness Directives 2004 are a legislative instrument enacted under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998 by David Alan Villiers, a delegate of the Civil Aviation Safety Authority (CASA). This instrument revokes and remakes various airworthiness directives pertaining to the Beechcraft 18 series aeroplanes, ensuring the aircraft maintain compliance with safety standards. The primary objective of this legislation is to address identified issues and safety concerns related to specific components of the Beechcraft 18 aeroplanes. Each directive is remade to reflect the latest safety requirements, thereby maintaining the airworthiness of these aircraft and ensuring they meet current regulatory standards.
Scope and Application
The Airworthiness Directives 2004, under the delegation of David Alan Villiers as a delegate of the Civil Aviation Safety Authority, pertains to the revocation and remaking of specific airworthiness directives for Beechcraft 18 Series Aeroplanes. These directives apply to aircraft operators and maintenance personnel involved in the operation and maintenance of the specified Beechcraft 18 Series Aeroplanes. The geographic and jurisdictional reach of these directives is nationwide, aligning with the Commonwealth's overarching jurisdiction in civil aviation safety. The legislative instrument includes a schedule that lists the specific airworthiness directives to be revoked or remade, such as inspections and modifications of various aircraft components. Subordinate instruments may further extend or restrict the application of these directives, ensuring compliance with the latest safety standards. Any exclusions or exemptions are not explicitly stated in the provided text, suggesting that the directives apply comprehensively to the specified aircraft and components.
Key Provisions
The Airworthiness Directives 2004, under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998, primarily involve the revocation of several existing Airworthiness Directives related to Beechcraft 18 Series Aeroplanes and their re-enactment as separate instruments. This legislative instrument, signed by David Alan Villiers as the delegate of the Civil Aviation Safety Authority, outlines specific airworthiness directives that need to be revoked or re-made (sections 1 and 2). These directives include inspections, modifications, and retirement procedures pertinent to various parts of the aircraft, such as the starter solenoid, landing gear, fuel tank gasket, horizontal stabiliser spar, wing centre section, control wheel shaft, undercarriage limit switch, centre spar, lower outer wing root fittings, mainplane lower main spar, centre section truss, outer mainplane, front seat restraint installations, control columns, elevator control arm assembly, Goodyear fuel cells, lower rudder torque tube, main landing gear components, and pilot seats.
The obligations imposed by this Act are centred around ensuring the safety and airworthiness of the Beechcraft 18 Series Aeroplanes. Operators and owners of these aircraft must adhere to the specific requirements outlined in the re-made directives, which include regular inspections, necessary modifications, and retirement of certain parts when required. Compliance with these directives is mandatory to maintain the aircraft's airworthiness certification and ensure safe operation. This includes conducting inspections at specified intervals, implementing modifications where necessary, and following procedures for the retirement of parts that no longer meet airworthiness standards.
Failure to comply with the provisions of these Airworthiness Directives can result in significant legal consequences. The Civil Aviation Safety Regulations 1998 outline potential offences and penalties for non-compliance. Civil penalties may include fines, while criminal penalties can lead to imprisonment. The specific maximum penalties are determined by the severity of the breach and the impact on aviation safety. Operators and owners must ensure that they understand and adhere to the requirements set forth in the directives to avoid these penalties and maintain the safety and airworthiness of their aircraft.