COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piper PA-32 (Cherokee Six) Series Aeroplanes
AD/PA-32/56 Steering System - Modification 5/78
Applicability: All models PA-32-260 and PA-32-300 with S/Nos. 32-7400001 to 32-7400050, 32- 7440001 to 32-7440086, 32-7440088 to 32-7440160.
Document: 1. Piper SB No. 428; or
2. FAA AD 74-18-13 Amendment 39-1939.
Compliance: Unless already accomplished, within 100 hours time in service after 30 April 1978.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, aim to ensure the safe and efficient operation of civil aviation within Australian airspace. These regulations provide a comprehensive framework for all aspects of civil aviation, including aircraft operations, airworthiness, and maintenance standards. One such specific directive is Part 39 - 105, which includes Airworthiness Directives (AD) for various aircraft models, including the Piper PA-32 (Cherokee Six) Series Aeroplanes. The AD/PA-32/56 pertains to a modification of the steering system for certain models of the Piper PA-32 series, identified by specific serial numbers. The directive was introduced to address safety concerns related to the steering system of these aircraft, ensuring compliance with safety standards to mitigate risks associated with potential failures in the steering mechanism. The objective is to mandate compliance within a specified timeframe, thereby enhancing the overall safety of the aircraft in operation.
Scope and Application
The Civil Aviation Regulations 1998, under PART 39 - 105, specifically addresses the safety and airworthiness of aircraft through the application of directives such as AD/PA-32/56. This directive applies to all Piper PA-32-260 and PA-32-300 models with serial numbers falling within specified ranges, mandating a modification to the steering system to ensure compliance with safety standards. The directive is mandatory for aircraft operators and must be adhered to within 100 hours of time in service following 30 April 1978, unless the required modification has already been performed. The geographic reach of this regulation is national, as it falls under the Commonwealth of Australia's jurisdiction. This directive does not explicitly exclude any specific entities or industries, meaning it applies broadly to all relevant aircraft within the defined serial number ranges. The directive is supported by specific documentation, including Piper SB No. 428 and FAA AD 74-18-13 Amendment 39-1939, which provide detailed instructions and specifications for the required modifications.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, includes provisions related to the Piper PA-32 (Cherokee Six) Series Aeroplanes, which detail the requirements for modifications to the steering system as outlined in AD/PA-32/56 (section 39-105). This directive applies to all models PA-32-260 and PA-32-300 with specific serial numbers, as listed in the regulations (section 39-105). The compliance documentation that must be referenced includes either Piper Service Bulletin No. 428 or FAA AD 74-18-13 Amendment 39-1939 (section 39-105). The directive mandates that the specified modification to the steering system must be completed unless it has already been carried out, and it must be done within 100 hours of time in service after 30 April 1978 (section 39-105).
The Act imposes specific obligations on the operators of the affected aircraft. Operators are required to ensure that the steering system modifications are carried out in accordance with the directive, using either Piper Service Bulletin No. 428 or the FAA AD 74-18-13 Amendment 39-1939 as the reference document. Operators must also ensure that the modifications are completed within the stipulated timeframe of 100 hours of time in service after the date specified, which is 30 April 1978 (section 39-105). The directive aims to enhance the safety of the aircraft by addressing potential issues with the steering system.
Failure to comply with the requirements set out in the AD/PA-32/56 directive may result in civil or criminal consequences. The specific consequences and penalties are not detailed in the provided text but are typically outlined in other sections of the Civil Aviation Regulations 1998. Generally, non-compliance with Civil Aviation Regulations can lead to enforcement actions, including fines, suspension or revocation of aircraft operating certificates, and potential criminal charges if the non-compliance results in an aviation accident or incident. The exact penalties would depend on the severity of the breach and would be determined in accordance with the broader provisions of the Civil Aviation Act 1988 and associated regulations.