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-205/16 Fuel Quantity Transmitter Scupper - Inspection
and Modification
2/72
Applicability: Model S205 with S/Nos. 001 to 003, 101 to 399 and 3-101 to 4-258; Model S208
with S/Nos. 001 to 003, 1-03 to 2-19 and 3-100.
Document: SIAI Marchetti SB 205B29.
Compliance: Inspect within 5 hours time in service after 29 February 1972 and thereafter at intervals not exceeding 50 hours time in service until modified.
Modify within 500 hours time in service after 29 February 1972.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, serve as a comprehensive framework governing civil aviation safety within the country. These regulations are designed to address the critical need for maintaining high safety standards in the aviation industry, ensuring the safety of passengers, crew, and the general public. One specific legislative instrument under this act is the Airworthiness Directive (AD) for SIAI Marchetti S205 and S208 Series Aeroplanes, identified as AD/SM-205/16. This directive was introduced to address issues related to the fuel quantity transmitter scupper, necessitating specific inspection and modification procedures to maintain the airworthiness of these aircraft models.
The Airworthiness Directive AD/SM-205/16 sets forth mandatory requirements for the inspection and modification of the fuel quantity transmitter scupper on designated SIAI Marchetti S205 and S208 series aeroplanes. The directive applies to specific serial numbers of these models and mandates that inspections must be conducted within a certain timeframe after 29 February 1972, with further inspections at intervals not exceeding 50 hours of time in service until the required modifications are made. Modifications must be completed within 500 hours of time in service following the specified date. This legislative instrument aims to ensure that these aircraft remain compliant with safety standards, thereby enhancing overall aviation safety.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the Civil Aviation Safety Authority's (CASA) issuance of Airworthiness Directives (ADs) for aircraft types. This includes SIAI Marchetti S205 and S208 series aeroplanes, which are subject to AD/SM-205/16, focusing on the fuel quantity transmitter scupper. The directive applies to specific serial numbers of the mentioned aircraft models, ensuring safety and compliance with operational standards. The regulation mandates inspections and modifications within specified timeframes post-service commencement, thereby ensuring the airworthiness and safety of the aircraft in question.
The scope of the AD is geographically and operationally confined to the Commonwealth of Australia, regulating the maintenance and inspection requirements for the specified aircraft within its jurisdiction. There are no stated exclusions or exemptions within the directive itself, though broader legislative or regulatory frameworks may offer additional context or exceptions. The applicability and enforcement of these regulations are extended through subordinate instruments issued by CASA, which can provide further detail or amendments to the directives.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandate the maintenance and inspection of SIAI Marchetti S205 and S208 Series Aeroplanes through Airworthiness Directives. According to AD/SM-205/16, section 2/72 pertains to the fuel quantity transmitter scupper, requiring a comprehensive inspection and modification procedure for certain model numbers (sections 1 and 2). For model S205, the applicable serial numbers range from 001 to 003, 101 to 399, and 3-101 to 4-258. For model S208, the applicable serial numbers are 001 to 003, 1-03 to 2-19, and 3-100.
Operators and owners of the specified aircraft must comply with the inspection and modification requirements outlined in the directive. According to section 2/72, the fuel quantity transmitter scupper must be inspected within 5 hours of time in service following 29 February 1972. After the initial inspection, the inspection must occur at intervals not exceeding 50 hours of time in service until the modification is completed. Additionally, the modification itself must be completed within 500 hours of time in service after 29 February 1972. The directive references SIAI Marchetti SB 205B29 as the document containing the necessary compliance details.
The regulations impose significant obligations on the parties involved. Operators and owners must ensure that inspections are conducted as per the specified intervals to maintain the airworthiness of the aircraft. Failure to comply with these inspection and modification requirements can lead to serious consequences. The Civil Aviation Regulations 1998 outline penalties for non-compliance, which may include substantial fines and potential grounding of the aircraft. The maximum penalties are not explicitly stated in the text but are generally severe, reflecting the critical nature of adhering to airworthiness directives.
In summary, the key provisions of the Civil Aviation Regulations 1998, particularly Part 39 - 105, mandate strict inspection and modification procedures for SIAI Marchetti S205 and S208 Series Aeroplanes. Operators and owners must adhere to these requirements to ensure the continued safety and airworthiness of the aircraft. Non-compliance with these directives can result in significant civil and criminal consequences, underscoring the importance of strict adherence to the outlined procedures.