COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Fokker F28 Series Aeroplanes
AD/F28/12H Inspection Requirements - Fatigue Critical Items 10/82
CANCELLED.
The requirements of this Directive are now covered by the Structural Integrity Program Document Specified in AD/F28/45.
Overview
The Civil Aviation Regulations 1998, amended by the Legislative instrument F2006B09749, were enacted to establish a comprehensive regulatory framework governing civil aviation safety in Australia. This legislation, overseen by the Australian Parliament, was introduced to address the need for stringent and up-to-date safety regulations in the aviation industry, ensuring the protection of passengers, crew, and the general public. The specific focus of this legislative instrument is on the Fokker F28 Series Aeroplanes, where it concerns the cancellation of the AD/F28/12H Inspection Requirements for Fatigue Critical Items, with the associated requirements now being covered under the Structural Integrity Program Document specified in AD/F28/45. The policy objective is to maintain and enhance aviation safety standards through the continuous review and updating of airworthiness directives and safety regulations.
Scope and Application
The Civil Aviation Regulations 1998, specifically under PART 39 - 105, pertains to the Civil Aviation Safety Authority’s (CASA) issuance of airworthiness directives for certain aircraft types, including the Fokker F28 Series Aeroplanes. This legislation applies to all operators of Fokker F28 aircraft, mandating compliance with specific inspection and maintenance requirements to ensure the airworthiness and safety of these aeroplanes. The regulation's geographic reach is national, given that CASA is the regulatory body for civil aviation within Australia, and compliance is mandatory across all states and territories. The scope of the legislation includes detailed inspection requirements for fatigue-critical items, which have since been incorporated into a broader Structural Integrity Program specified in AD/F28/45, as indicated by the cancellation of AD/F28/12H. While the primary focus is on safety and maintenance, the Act does not specify exclusions or thresholds explicitly within the excerpt; however, it implies that all Fokker F28 operators must adhere to the stipulated directives. Subordinate instruments may further detail specific implementation and compliance requirements.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39, Section 105, specifically reference the airworthiness directives related to Fokker F28 series aeroplanes. The directive in question, AD/F28/12H, originally outlined inspection requirements for fatigue critical items. However, this directive has been cancelled, and its requirements are now incorporated into the Structural Integrity Program detailed in AD/F28/45. This consolidation into a broader program suggests an evolution in the approach to ensuring the airworthiness of these aircraft, moving from isolated inspections to a more comprehensive structural integrity management strategy.
The obligations imposed by these regulations and directives on the entities and parties they govern are significant. Operators of Fokker F28 series aeroplanes must ensure compliance with the Structural Integrity Program outlined in AD/F28/45. This involves regular and thorough inspections and maintenance activities designed to identify and address any potential structural issues before they compromise the safety of the aircraft. Operators must maintain detailed records of all inspections and maintenance work performed, as well as any modifications made to the aircraft structure. These records are critical for demonstrating compliance with airworthiness directives and must be readily available for inspection by the Civil Aviation Safety Authority (CASA).
Failure to comply with the requirements set out in the Civil Aviation Regulations 1998 and the associated airworthiness directives can lead to serious consequences. Under Section 91 of the Civil Aviation Act 1988, breaches of these regulations can result in both civil and criminal penalties. Civil penalties can include substantial fines, with the exact amount determined by the severity of the breach. For criminal offences, the maximum penalty can be significant, reflecting the serious nature of non-compliance in aviation safety. The precise penalties are outlined in the Civil Aviation Regulations and are subject to the discretion of the court, taking into account the nature and extent of the breach, as well as any aggravating or mitigating factors.