COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 60 (Duke) Series Aeroplanes
AD/BEECH 60/27
Amdt 1
Strobe Light Bounding Straps 11/74
Applicability: All model A60 & B60, S/Nos. P-223 thru P-307, P-309 and P-310, fitted with Grimes P/N 30-0467-1 or Grimes P/N 30-0467-3 strobe light assemblies.
Requirement: Action in accordance with Beechcraft SI No. 0655-362, Rev. 1. Compliance: Within 100 hours’ time in service after 31 January 1975.
Overview
The Civil Aviation Regulations 1998 (Cth), enacted by the Commonwealth of Australia, forms a critical component of the regulatory framework governing aviation safety in Australia. These regulations, overseen by the Civil Aviation Safety Authority (CASA), aim to ensure that all civil aviation activities within Australia are conducted in a manner that mitigates risks to public safety and property. The specific focus of Part 39 - 105, which pertains to Airworthiness Directives, is to mandate safety measures and compliance standards for specific aircraft types, thereby addressing any identified safety issues and maintaining high standards of airworthiness. The legislative intent is clear: to enhance aviation safety by ensuring that all aircraft, and their components, meet stringent regulatory standards.
One such directive under this part is AD/BEECH 60/27, which was introduced to address a specific safety concern related to the strobe light bounding straps on Beechcraft 60 (Duke) Series Aeroplanes. This directive applies to all model A60 and B60 aircraft with specified serial numbers, fitted with certain Grimes P/N strobe light assemblies. The directive mandates corrective actions in line with Beechcraft Service Instruction No. 0655-362, Revision 1, and requires compliance within 100 hours of time in service after 31 January 1975. This legislative measure underscores the commitment of the Australian government, through CASA, to continually address and rectify safety issues in the aviation sector, ensuring the highest level of safety for all aviation activities.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning Airworthiness Directives for Beechcraft 60 (Duke) Series Aeroplanes, applies to all model A60 and B60 aircraft, specifically those with serial numbers ranging from P-223 through P-307, P-309, and P-310, that are equipped with Grimes Part Numbers 30-0467-1 or 30-0467-3 strobe light assemblies. This directive is administered by the Civil Aviation Safety Authority and is applicable within the Commonwealth of Australia, enforcing compliance with aviation safety standards set forth by the regulatory body. The directive mandates that compliance with the specified action, in accordance with Beechcraft Service Instruction No. 0655-362, Revision 1, must be achieved within 100 hours of time in service after 31 January 1975. This ensures that the affected aircraft meet the necessary safety standards to maintain airworthiness and operational integrity.
Key Provisions
The Civil Aviation Regulations 1998, under PART 39 - 105, include specific Airworthiness Directives (AD) aimed at ensuring the safety and compliance of aircraft operations. One such directive, AD/BEECH 60/27 Amendment 1, pertains to the strobe light bounding straps on Beechcraft 60 (Duke) Series Aeroplanes, specifically models A60 and B60 with serial numbers P-223 through P-307, P-309, and P-310, that are equipped with Grimes P/N 30-0467-1 or Grimes P/N 30-0467-3 strobe light assemblies. This directive requires actions in accordance with Beechcraft Service Information (SI) No. 0655-362, Revision 1, and compliance must be achieved within 100 hours of time in service following 31 January 1975.
Under the Civil Aviation Regulations, the specified Beechcraft 60 (Duke) Series Aeroplanes must adhere to the requirements outlined in the AD/BEECH 60/27 Amendment 1. This includes the implementation of modifications or actions specified in the referenced Beechcraft Service Information No. 0655-362, Revision 1. The directive mandates that these changes must be completed within the stipulated timeframe of 100 hours of time in service after the effective date of 31 January 1975. This ensures that the aircraft's strobe light assemblies meet the necessary safety standards and function correctly, thus enhancing overall aviation safety.
Entities and individuals governed by the Civil Aviation Regulations, particularly those operating the specified Beechcraft 60 (Duke) Series Aeroplanes, are obligated to ensure that the required modifications to the strobe light bounding straps are carried out in accordance with the specified service information. This involves a thorough review and implementation of the technical directives provided by Beechcraft to guarantee compliance. Operators must also maintain records and documentation of the actions taken to comply with the AD/BEECH 60/27 Amendment 1, ensuring that the aircraft remains airworthy and meets the regulatory standards set forth by the Civil Aviation Safety Authority.
Failure to comply with the requirements of AD/BEECH 60/27 Amendment 1 can result in serious consequences. The Civil Aviation Regulations outline potential civil and criminal penalties for non-compliance, which may include fines and imprisonment. The specific penalties are not detailed within the directive itself but are governed by the broader provisions of the Civil Aviation Act 1988 and related regulations. Non-compliance with airworthiness directives is taken seriously, as it directly impacts the safety and reliability of aircraft operations, potentially leading to severe repercussions for the entities involved.