COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
SIAI Marchetti 260 Series Aeroplanes
AD/SM-260/8A Control Surface Hinge Bracket Attaching Holes - Inspection
11/76
Applicability: All models F260 and F260B with S/Nos. 101 to 125, 2-26 to 2-61, 3-76, 3-77, 3-78,
3-80, 3-84, 502 10-09 and 20-01.
Requirement: 1. Inspect all Control Surface Hinge Bracket Attachments in accordance with SIAI Marchetti SB No. 260B16.
2. Modify all Control Surface Hinge Bracket Attachments in accordance with the applicable SIAI Marchetti Service Bulletins (See note).
Note: SIAI Marchetti SBs Nos. 260B21 to 260B27 detail modifications to be incorporated at the specific attachments.
Compliance: For para 1 - Within 100 hours time in service after 31 August 1976 and thereafter at intervals not exceeding 200 hours time in service until modified.
For para 2 - Within 1000 hours time in service after 31 December 1976.
Overview
The Civil Aviation Regulations 1998, administered by the Civil Aviation Safety Authority (CASA), were enacted to ensure the safety and efficiency of civil aviation within Australia. These regulations address gaps in aviation safety and operational standards, providing a comprehensive framework for the maintenance and operation of aircraft. Specifically, Part 39 - 105 of the Civil Aviation Regulations focuses on airworthiness directives, which are crucial for maintaining the safety of aircraft in service. The Airworthiness Directive (AD) AD/SM-260/8A for SIAI Marchetti 260 Series Aeroplanes, for example, mandates inspections and modifications to control surface hinge bracket attachments to prevent potential failures and ensure continued safe operation. The policy objective of these regulations is to uphold the highest standards of aviation safety, thereby protecting the public and maintaining the integrity of the Australian civil aviation system.
Scope and Application
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, mandates the application of Airworthiness Directives (AD) concerning SIAI Marchetti 260 Series Aeroplanes. This legislation applies to all models F260 and F260B with specific serial numbers, thereby targeting particular aircraft within the Australian aviation sector. The directive requires compliance with inspection and modification protocols of Control Surface Hinge Bracket Attachments, ensuring the airworthiness of these aeroplanes. The geographical scope of this Act is national, encompassing all regions within Australia where these aircraft are operated. The AD provides specific timelines for compliance, requiring inspections within 100 hours of service post-August 31, 1976, and subsequent inspections at intervals not exceeding 200 hours until modifications are made. Modifications are required within 1000 hours of service post-December 31, 1976. This AD is an integral part of the Civil Aviation Regulations, extending its reach through subordinate instruments such as Service Bulletins issued by SIAI Marchetti, which detail specific modifications to be incorporated.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39, Section 105, mandate specific requirements for the airworthiness of certain aircraft models. The regulation in focus is AD/SM-260/8A, which pertains to SIAI Marchetti 260 Series Aeroplanes. The directive (AD/SM-260/8A) targets all F260 and F260B models with serial numbers ranging from 101 to 125, 2-26 to 2-61, 3-76 to 3-84, 502 10-09, and 20-01. The primary requirement (Section 1) is to inspect all Control Surface Hinge Bracket Attachments in accordance with SIAI Marchetti Service Bulletin No. 260B16. Additionally, all Control Surface Hinge Bracket Attachments must be modified in line with the relevant SIAI Marchetti Service Bulletins, particularly those numbered 260B21 to 260B27, which detail specific modifications.
These regulations impose clear obligations on the operators of the affected aircraft. Operators must ensure that inspections are conducted within 100 hours of time in service after 31 August 1976, and subsequently, at intervals not exceeding 200 hours until modifications are completed. For the modifications themselves, they must be performed within 1000 hours of time in service after 31 December 1976. Compliance with these requirements is critical for maintaining the airworthiness of the aircraft, ensuring safety and adherence to regulatory standards.
Failure to comply with the AD/SM-260/8A directive may result in serious consequences. The Civil Aviation Regulations 1998 do not explicitly detail specific penalties or consequences for non-compliance with this directive in the provided text. However, non-compliance with airworthiness directives generally can lead to severe civil or criminal penalties under the Civil Aviation Act 1988. This could include substantial fines, potential grounding of the aircraft, and legal action against the operators or responsible parties. The exact penalties would depend on the specific circumstances of the non-compliance and the discretion of the Civil Aviation Safety Authority.