COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
SIAI Marchetti S205 and S208 Series Aeroplanes
AD/SM-205/20 Main and Nose Landing Gear Torque
Link Pins and Bolts - Modification Applicability: All 205 series with S/Nos. 001 to 003, 101 to 399 and 4-101 to 4-212. Document: SIAI Marchetti SB 205B35.
Compliance: With 100 hours time in service after 31 July 1972.
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Overview
The Civil Aviation Regulations 1998, under PART 39 - 105, specifically address the airworthiness of aircraft to ensure safety and compliance with civil aviation standards. This legislation was enacted by the Parliament of Australia and aims to maintain high safety standards in the aviation industry by setting forth regulations on the maintenance and modification of aircraft. The objective is to ensure that all aircraft, including the SIAI Marchetti S205 and S208 Series Aeroplanes, meet the required safety criteria. One such regulation, AD/SM-205/20, pertains to the modification of main and nose landing gear torque link pins and bolts for the specified series of aircraft, ensuring their structural integrity and operational safety within specified time frames after manufacture. This legislative instrument is critical for the oversight and maintenance of aircraft safety standards, thereby protecting the public and maintaining the integrity of the aviation industry.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, applies to the SIAI Marchetti S205 and S208 series aeroplanes, mandating compliance with AD/SM-205/20. This directive concerns the modification of the main and nose landing gear torque link pins and bolts. It is applicable to all SIAI Marchetti S205 series aeroplanes with serial numbers ranging from 001 to 003, 101 to 399, and 4-101 to 4-212. Compliance is required for aircraft that have accumulated 100 hours of time in service post 31 July 1972. The regulations extend to the Commonwealth jurisdiction, overseen by the Civil Aviation Safety Authority (CASA), ensuring a standardised approach to aviation safety across Australia. There are no specific exclusions, exemptions, or thresholds stated in this directive, implying that all eligible aircraft must comply without exception. This legislative instrument is a crucial component in maintaining the safety standards of the specified aircraft within the national aviation framework.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes a Schedule of Airworthiness Directives that governs the maintenance and operational standards for certain aircraft. Within this Schedule, AD/SM-205/20 pertains to the SIAI Marchetti S205 and S208 series aeroplanes and mandates modifications to the main and nose landing gear torque link pins and bolts. This directive applies to all 205 series aircraft with serial numbers ranging from 001 to 003, 101 to 399, and 4-101 to 4-212. Compliance with this directive is required within 100 hours of time in service after 31 July 1972, as stipulated in SIAI Marchetti SB 205B35.
Under this regulation, the primary requirement is that the specified aircraft must undergo modifications to their main and nose landing gear torque link pins and bolts. These modifications are essential to ensure the continued airworthiness of the aircraft and to comply with the safety standards set forth by the Civil Aviation Safety Authority (CASA). Operators of these aircraft must ensure that the modifications are completed within the specified timeframe to maintain compliance with the regulations.
Operators and owners of the affected aircraft bear significant responsibilities under this directive. They must ensure that the modifications are carried out by appropriately qualified personnel and that all work is thoroughly documented. This documentation must be maintained and made available for inspection by CASA upon request. Failure to comply with these requirements can result in severe consequences, including potential grounding of the aircraft, fines, and other penalties.
In terms of enforcement, the Civil Aviation Regulations 1998 provide for both civil and criminal penalties for non-compliance with airworthiness directives. Civil penalties may include fines up to the statutory maximum, which can be substantial depending on the severity and frequency of the violation. Criminal penalties can also be imposed, including fines and imprisonment, for serious breaches that endanger safety. CASA has the authority to take enforcement actions such as grounding aircraft, suspending air operator certificates, and initiating legal proceedings against non-compliant parties. Therefore, it is imperative for operators and owners to adhere strictly to the requirements of AD/SM-205/20 to avoid these adverse consequences.