AD/SM-205/11A - Flap Lock Mechanism - Modification

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Legislation au F2006B07033 In force Legislative Instrument

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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-205/11A Flap Lock Mechanism - Modification 2/72

Applicability: All S205 Series.

 

Document: 1. SIAI Marchetti SB 205B25; or

 

2. FAA AD 70-20-1; or

 

3. AD/SM-205/11.

 

Compliance: Before 29 February 1972.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, amended in 2006, were enacted by the Australian Parliament to ensure the safety and efficiency of civil aviation in Australia. These regulations cover various aspects of aviation operations, including airworthiness standards. Part 39, specifically, outlines the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, ensuring that aircraft meet specific safety standards. The policy objective of these regulations is to maintain high safety standards in civil aviation to protect passengers, crew, and the general public. One example of these regulations in action is the AD/SM-205/11A concerning the flap lock mechanism modification for SIAI Marchetti S205 and S208 Series Aeroplanes. This directive aims to address the potential safety issues associated with the flap lock mechanism, ensuring compliance before 29 February 1972, and mandates specific modifications to enhance aircraft safety. The legislation is designed to be enforced by CASA to uphold the overarching policy of ensuring that all aircraft operating within Australian airspace meet stringent safety standards.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to the SIAI Marchetti S205 and S208 Series Aeroplanes, detailing the Airworthiness Directives (AD) issued by the Civil Aviation Safety Authority (CASA). This legislation mandates compliance with AD/SM-205/11A concerning the flap lock mechanism modification, which is imperative for all S205 Series aircraft. This directive applies to aircraft identified as SIAI Marchetti SB 205B25, in accordance with the Federal Aviation Administration's (FAA) AD 70-20-1, and the prior AD/SM-205/11 issued before 29 February 1972. The regulations extend across the Commonwealth of Australia, ensuring that all operators of the specified aircraft types within the Australian jurisdiction adhere to the outlined safety directives to maintain airworthiness standards. The Act does not explicitly state any exclusions or exemptions but implicitly requires compliance with the specified modifications and standards. The scope of the regulation can be further detailed and expanded through subordinate instruments issued by CASA.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39, particularly Section 105, govern the authority of the Civil Aviation Safety Authority (CASA) to issue airworthiness directives for specific aircraft models, such as the SIAI Marchetti S205 and S208 series aeroplanes. Section 105 mandates that any modification to the flap lock mechanism of these aircraft must adhere to the specifications outlined in the directive AD/SM-205/11A. This directive is critical for maintaining the safety and airworthiness of the aircraft, ensuring that any modifications are performed in accordance with the standards set forth by CASA. The directive applies to all S205 series aeroplanes, and compliance must be achieved before 29 February 1972. The obligations imposed by this Act on the operators and maintainers of the SIAI Marchetti S205 and S208 series aeroplanes are stringent. Operators must ensure that all modifications to the flap lock mechanism are carried out following the detailed instructions provided in the relevant documents, which include the SIAI Marchetti SB 205B25, the FAA AD 70-20-1, and the AD/SM-205/11 directive. This means that maintenance personnel must be trained and certified to perform these modifications, and records of all modifications must be kept and maintained for regulatory review. Additionally, operators must ensure that any non-compliance with these directives is rectified promptly to maintain the safety standards required by CASA. Failure to comply with the provisions of the Civil Aviation Regulations 1998, specifically Section 105 and the related airworthiness directives, can lead to severe consequences. Civil penalties can be imposed for non-compliance, which may include fines up to the statutory maximum as prescribed by the Civil Aviation Act 1988. In more severe cases, CASA can take action that may result in the grounding of the aircraft, suspension of airworthiness certificates, or even the revocation of operating permits. Additionally, criminal charges can be brought against individuals or corporations responsible for non-compliance, potentially leading to imprisonment, further fines, or both. It is imperative that all parties governed by these regulations adhere to the directives to avoid these serious repercussions.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.