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 76 (Duchess) Series Aeroplanes
AD Name AD Number
Control Bearing Assemblies AD/BEECH 76/1
Cowl Flap Hinge Assemblies AD/BEECH 76/2
Elevator Trailing Edge Bond AD/BEECH 76/3
Fuel Tank Outlet Check Valve and Fuel Selector Valves AD/BEECH 76/4
Main Landing Gear Fork Pin AD/BEECH 76/5
Wing Spar Centre Splice Plates AD/BEECH 76/6
Aileron and Rudder Bellcrank Stop Bolt Nuts AD/BEECH 76/7
Rudder and Rudder Trim Tab AD/BEECH 76/8
Engine Mount Assembly AD/BEECH 76/9 Amdt 1
Engine Mount Support Structure AD/BEECH 76/10 Amdt 2
Elevator Down Cable AD/BEECH 76/11
Wing Structural Inspections and Fatigue Life Limitation AD/BEECH 76/12 Amdt 1
Rudder Torque Lower Hinge Adaptor AD/BEECH 76/13
Engine Control Rod Safety Washers AD/BEECH 76/14
Woodward Governor Models L and R 210652 AD/BEECH 76/15
MLG Side Brace Overcentre Travel and Limit Switch AD/BEECH 76/16 Amdt 1
Wing Lower and Upper Splice Plate Bolt Installation AD/BEECH 76/17
MLG A Frame Assembly AD/BEECH 76/18 Amdt 1
Overview
The Airworthiness Directives 2004, enacted under the authority of the Civil Aviation Safety Regulations 1998, represents a significant legislative action by the Civil Aviation Safety Authority to address and rectify issues related to the airworthiness of specific aircraft models, namely the Beechcraft 76 (Duchess) series aeroplanes. The primary problem this legislation aimed to address was the need to ensure that the maintenance and operational standards for these aircraft meet the necessary safety requirements. This was achieved by revoking and remaking existing airworthiness directives, ensuring that they are aligned with the latest safety standards and practices. The policy objective underpinning this action was to enhance aviation safety by maintaining stringent airworthiness standards, thereby protecting the lives of passengers, crew, and the general public. The Civil Aviation Safety Authority, through its delegate David Alan Villiers, undertook this legislative revision to uphold the highest safety benchmarks in the aviation industry.
Scope and Application
The Airworthiness Directives 2004, issued under the authority of the Civil Aviation Safety Authority (CASA) and by the delegate, David Alan Villiers, pertains specifically to the airworthiness of the Beechcraft 76 (Duchess) Series aeroplanes. This legislative instrument revokes the existing airworthiness directives as listed in Schedule 1 and re-makes them as separate instruments, each corresponding to specific aircraft components or systems. The directives address various technical and safety issues such as control bearing assemblies, cowl flap hinge assemblies, elevator trailing edge bonds, and fuel tank outlets, among others. These directives apply to all aircraft operators and maintainers of the specified Beechcraft 76 series aeroplanes within the jurisdiction of CASA, which covers the entire Commonwealth of Australia. There are no stated exclusions or exemptions within the scope of this legislation, and it is enforced uniformly across the country. The re-made directives are intended to ensure compliance with the highest safety standards, thereby enhancing the overall airworthiness of the affected aircraft.
Key Provisions
This legislative instrument, the Airworthiness Directives 2004, serves to revoke and re-make a series of airworthiness directives specifically related to the Beechcraft 76 (Duchess) Series Aeroplanes. This is done under subregulation 39.001 (1) of the Civil Aviation Safety Regulations 1998. The directives being revoked and re-made are listed in Schedule 1 and are being re-made in the exact form as they appear in the latest published edition. The key provisions revolve around specific components and maintenance requirements for the aircraft, such as control bearing assemblies, cowl flap hinge assemblies, and elevator trailing edge bonds, among others.
The obligations and requirements imposed by this legislation on the parties involved, particularly aircraft owners and operators, are stringent. They must adhere to the detailed specifications outlined in each re-made directive. This includes conducting regular inspections, implementing necessary repairs or modifications, and ensuring compliance with any prescribed time frames or operational limitations. The directives mandate that these steps be taken to maintain the airworthiness of the Beechcraft 76 (Duchess) Series Aeroplanes, ensuring that all aspects of the aircraft meet safety standards set by the Civil Aviation Safety Authority (CASA).
Failure to comply with these directives can result in significant legal consequences. The legislation stipulates that breaches may lead to enforcement actions by CASA. In terms of penalties, while the specific fines are not detailed in the provided text, it is known that non-compliance with airworthiness directives can result in substantial penalties under the Civil Aviation Safety Regulations 1998. These penalties could include fines and, in severe cases, criminal charges against the aircraft operator or owner, potentially leading to imprisonment. The exact penalties would depend on the severity of the breach and the specific provisions of the relevant regulations.