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-205/34
Amdt 1
Wing Rear Spar - Inspection 3/84
Applicability: All models S205-18/F, S205-20F; S205-18/R, S205-20/R, S205-22/R, S208, S208A.
Requirement: SIAI-Marchetti S.B. No. 205B57.
Compliance: Unless already accomplished, before further flight and thereafter at intervals not exceeding 50 hours time in service.
Background: a. The manufacturer has received reports of cracking in the wing rear spar at the locations described above.
b. This Directive has been amended to reflect the revised Aircraft Applicability and Requirement Document reissue.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, were introduced to ensure the safe and efficient operation of civil aviation in Australia. One part of this comprehensive regulatory framework is the Schedule of Airworthiness Directives, which includes AD/SM-205/34 Amendment 1, specifically concerning SIAI Marchetti S205 and S208 Series Aeroplanes. This directive was introduced to address the identified problem of cracking in the wing rear spar of certain SIAI Marchetti models, as reported by the manufacturer. The policy objective is to enhance aviation safety by ensuring that operators of these aircraft conduct mandatory inspections to prevent potential structural failures, thereby maintaining the airworthiness of the affected aeroplanes.
The directive mandates that specific SIAI Marchetti models undergo inspections of the wing rear spar before further flight and at intervals not exceeding 50 hours of time in service. This requirement is crucial for ensuring the safety and integrity of the aircraft in question, reflecting the Civil Aviation Safety Authority's commitment to mitigating risks associated with known structural issues. The directive was amended to reflect updates to the Aircraft Applicability and Requirement Document, ensuring that the regulatory requirements remain current and effective in addressing safety concerns.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, applies to a defined range of SIAI Marchetti S205 and S208 series aeroplanes, namely the models S205-18/F, S205-20F; S205-18/R, S205-20/R, S205-22/R, S208, S208A. This regulatory directive is applicable across the Commonwealth of Australia, thereby ensuring a uniform approach to airworthiness standards and safety across all states and territories. The directive mandates specific compliance requirements regarding the inspection of the wing rear spar to address reports of cracking, as detailed in the SIAI-Marchetti S.B. No. 205B57. Aircraft operators must conduct these inspections before further flight and at intervals not exceeding 50 hours of time in service to maintain compliance. The regulation extends its applicability through subordinate instruments, which may provide further detail or amendments to the initial directive as circumstances or technological advancements dictate.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 – 105, includes a schedule of airworthiness directives that are critical for ensuring the safety of aircraft operations. One such directive, AD/SM-205/34 Amendment 1, pertains to the inspection of the wing rear spar for SIAI Marchetti S205 and S208 series aeroplanes (Section 105). This directive applies to all models S205-18/F, S205-20F; S205-18/R, S205-20/R, S205-22/R, S208, S208A, as outlined in Section 3/84. The requirement for compliance is detailed in SIAI-Marchetti S.B. No. 205B57, which mandates that the inspection must be carried out unless it has already been completed, before the aeroplane can be flown further, and at intervals not exceeding 50 hours of time in service.
The obligations imposed by this directive are clear and straightforward. Operators of the specified SIAI Marchetti aeroplanes must ensure that the wing rear spar inspection is performed in accordance with the specified SIAI-Marchetti S.B. No. 205B57. This means that before any further flight of these aeroplanes, the inspection must be conducted, and subsequently, it must be repeated at intervals not exceeding 50 hours of time in service. This ongoing requirement ensures that any potential issues, such as cracking in the wing rear spar, are identified and addressed promptly to maintain airworthiness.
Failure to comply with the airworthiness directives set out in the Civil Aviation Regulations can lead to significant consequences. Section 105 of the Regulations outlines the potential for both civil and criminal penalties for non-compliance. The specific penalties are not detailed in the excerpt but typically include fines and imprisonment for breaches of civil aviation safety regulations. Operators found in breach of these requirements could face severe penalties, reflecting the high priority placed on ensuring the safety of all civil aviation operations within Australia. The seriousness of these potential consequences underscores the importance of adhering to the airworthiness directives as mandated by the Civil Aviation Regulations.