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-205/27 Flap Control Arms P/Nos. 205-6-052-1,
-03, -101 and -103 - Inspection
7/77
Applicability: All models 205.
Requirement: Visually inspect the reference P/No. flap control arms for cracks with the aid of a 10X glass or an approved dye penetrant technique.
Note: RAI AD No. 77-91/S205-41 and SIAI MARCHETTI SB No. 205B47 refer to
this inspection.
Compliance: Within 100 hours time in service after 31 July 1977.
Overview
The Civil Aviation Regulations 1998, as amended, encompass a comprehensive framework for ensuring the safety of civil aviation in Australia. This legislation, enacted by the Parliament of Australia, is overseen by the Civil Aviation Safety Authority (CASA) and is intended to fill critical gaps in the regulation of civil aviation, ensuring that all aircraft operations meet the highest standards of safety. The Regulations are designed to safeguard the public by enforcing stringent safety requirements on aircraft, personnel, and operations within Australia's airspace. A specific example of this commitment to safety is found in Part 39 - 105, which outlines Airworthiness Directives for specific aircraft models, such as the SIAI Marchetti S205 and S208 Series Aeroplanes. These directives mandate regular inspections of critical components, such as flap control arms, to prevent potential failures and ensure the continued airworthiness of these aircraft. The policy objective is clear: to maintain and enhance the safety of civil aviation by imposing detailed regulatory requirements and ensuring compliance through rigorous oversight.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, applies to all models 205 of the SIAI Marchetti S205 and S208 series aeroplanes. This regulation mandates a visual inspection of the specified flap control arms, with reference parts numbers 205-6-052-1, -03, -101, and -103, for any cracks. The inspection must be conducted with the aid of a 10X magnifying glass or an approved dye penetrant technique. This requirement is to ensure the continued airworthiness of these aircraft and is referenced in RAI AD No. 77-91/S205-41 and SIAI Marchetti Service Bulletin No. 205B47. The compliance must be achieved within 100 hours of time in service after 31 July 1977. The geographic reach of this regulation is national, applying throughout Australia under the oversight of the Commonwealth of Australia's Civil Aviation Safety Authority. The regulation does not explicitly state any exclusions or thresholds beyond the specified models and parts. However, it may be extended or restricted through subordinate instruments issued by the Civil Aviation Safety Authority.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, detail the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, which includes AD/SM-205/27 concerning SIAI Marchetti S205 and S208 series aeroplanes. This particular directive mandates that flap control arms P/Nos. 205-6-052-1, -03, -101, and -103 must be visually inspected for cracks. This inspection should be conducted with the aid of a 10X magnifying glass or an approved dye penetrant technique. The directive references RAI AD No. 77-91/S205-41 and SIAI Marchetti Service Bulletin No. 205B47 for additional guidance on this inspection.
Operators and owners of the affected aircraft must adhere to this directive by ensuring the flap control arms are inspected within 100 hours of time in service after 31 July 1977. This requirement is critical to maintaining the airworthiness of the aircraft and ensuring the safety of all passengers and crew. The inspection must be performed meticulously, with attention to detail to detect any potential cracks that could compromise the structural integrity of the flap control arms.
Failure to comply with the provisions outlined in AD/SM-205/27 can lead to significant consequences. Operators and owners may face enforcement actions by CASA, which could include fines, penalties, or even grounding of the aircraft until compliance is achieved. The specific penalties are detailed in the Civil Aviation Regulations 1998, but generally, non-compliance with airworthiness directives can result in substantial financial penalties and reputational damage. Therefore, it is imperative for operators and owners to prioritise these inspections and ensure that they are conducted in accordance with the stipulated timeframes and techniques.
Additionally, repeated non-compliance or failure to address identified issues can lead to more severe penalties, including potential criminal charges against responsible individuals. The severity of the consequences underscores the importance of adhering to the directives issued by CASA. Ensuring that all inspections are carried out as required not only maintains the safety of the aircraft but also safeguards the interests of all parties involved in aviation operations.