AD/SM-205/4 - Fuselage - Reinforcement

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B07062 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-205/4 Fuselage - Reinforcement 3/71

Applicability: All S205 series with S/Nos. 001 to 4-173 except 103, 109, 217, 348, 351, 369, 4-101,

4103, 4-121, 4-127, 4-137, 4-144, 4-149, 4-150, 4-151, 4-152, 4-153, 4-168 and 4-

172.

 

Document:  SIAI Marchetti SB 205B20. Compliance: Before 31 March 1971.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Safety Authority (CASA) issued Airworthiness Directive AD/SM-205/4 in 1998 to address specific structural integrity concerns related to the fuselage of the SIAI Marchetti S205 and S208 series aeroplanes. The directive targets certain serial numbers within the specified range, excluding those listed as exempt, to ensure compliance with safety standards by a specified date. The objective of this legislation is to mitigate potential safety risks by mandating reinforcement measures for the fuselage of affected aircraft, thereby enhancing overall aviation safety. This legislative instrument is part of the Civil Aviation Regulations 1998, enacted by the Australian Parliament to regulate civil aviation safety and establish standards for aircraft airworthiness. The directive aims to ensure that the specified aeroplanes meet safety requirements by reinforcing their fuselages, thus addressing a particular safety gap identified by CASA. The policy objective is to maintain and improve the safety of civil aviation through stringent compliance measures.

Scope and Application

The Civil Aviation Safety Authority (CASA) has issued an Airworthiness Directive (AD) under the Civil Aviation Regulations 1998, specifically targeting the SIAI Marchetti S205 and S208 series aeroplanes. This directive mandates reinforcement of the fuselage for certain aircraft serial numbers, namely all S205 series aircraft with serial numbers ranging from 001 to 4-173, with specified exceptions for serial numbers including 103, 109, 217, 348, 351, 369, 4-101, 4-103, 4-121, 4-127, 4-137, 4-144, 4-149, 4-150, 4-151, 4-152, 4-153, 4-168, and 4-172. This directive applies to aircraft operators and owners who must ensure compliance with the specified reinforcement measures before 31 March 1971. The directive is part of the broader framework of civil aviation regulations administered by CASA and is applicable across the Commonwealth of Australia, ensuring uniform safety standards in the aviation industry. This AD extends its reach to any person or entity operating the specified SIAI Marchetti aircraft within Australian jurisdiction, underscoring the importance of adhering to these safety directives to maintain airworthiness and public safety.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39, Section 105, mandate certain airworthiness directives to ensure the safety of aircraft, including the SIAI Marchetti S205 and S208 series aeroplanes. AD/SM-205/4 pertains to the reinforcement of the fuselage of S205 series aeroplanes with specific serial numbers. These serial numbers are listed in the applicability clause, excluding certain identified numbers such as 103, 109, 217, and others up to 4-172. This directive requires compliance with the document SIAI Marchetti SB 205B20 and must be completed before 31 March 1971. Operators and owners of the affected S205 series aeroplanes are obligated to ensure that the required fuselage reinforcement is carried out as per the specified document. This includes performing the necessary structural modifications to meet the airworthiness standards set forth by the Civil Aviation Safety Authority (CASA). The directive requires detailed documentation of the reinforcement process to verify compliance and to ensure that the modifications do not compromise the structural integrity or operational safety of the aircraft. Failure to comply with the airworthiness directive AD/SM-205/4 can lead to serious consequences. The Civil Aviation Regulations 1998 impose civil penalties for non-compliance, which can include substantial fines. Additionally, continued operation of an aircraft that does not meet the specified airworthiness standards can result in the aircraft being grounded, thereby preventing its operation until the required modifications are completed. The severity of the penalties underscores the importance of adhering to the directive to maintain the highest safety standards in civil aviation. Furthermore, in cases where non-compliance leads to safety incidents or accidents, the operators and owners may face criminal charges. The potential criminal consequences include imprisonment, reflecting the gravity of neglecting safety directives that are critical for the protection of lives and property. Therefore, it is imperative that all stakeholders involved with the affected aircraft meticulously follow the requirements of AD/SM-205/4 to avoid legal repercussions and to uphold the safety standards mandated by the Civil Aviation Regulations 1998.

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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.