COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Fokker F28 Series Aeroplanes
AD/F28/14 | Aileron Control System - Modification | NK |
Applicability: | All models with S/Nos. 11003 to 11031 and 11991 to 11994. | |
Document: | Fokker SB F28/27-47. | |
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, provide a comprehensive regulatory framework to ensure the safety of civil aviation. Part 39 of these regulations specifically addresses airworthiness directives, which are legally enforceable rules relating to design, production, maintenance, and operation of aircraft. One such directive, AD/F28/14, pertains to the aileron control system of Fokker F28 Series aeroplanes, aiming to address specific safety issues identified with certain serial numbers. This directive was introduced to mitigate identified risks and ensure the continued airworthiness of affected aircraft, aligning with the overarching policy objective of maintaining high safety standards in civil aviation. The Civil Aviation Safety Authority, under the authority granted by the Civil Aviation Act 1988, issues these directives to ensure compliance and uphold safety across the aviation industry.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates that certain Fokker F28 Series Aeroplanes with specific serial numbers are subject to the Civil Aviation Safety Authority’s airworthiness directives. This regulation applies to all models of Fokker F28 aircraft with serial numbers ranging from 11003 to 11031 and from 11991 to 11994, focusing on modifications to the aileron control system as outlined in document Fokker SB F28/27-47. The scope of the Act is geographically and operationally confined to the Commonwealth of Australia, ensuring that all aircraft within its jurisdiction meet the specified safety standards. The regulations do not explicitly state any exclusions or exemptions; thus, the directives apply universally to the identified serial numbers. The application of these regulations may be extended or clarified through subordinate instruments, such as additional notices or amendments issued by the Civil Aviation Safety Authority.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, contain detailed provisions governing the airworthiness directives issued by the Civil Aviation Safety Authority (CASA). Section 105.130 outlines the requirements for compliance with airworthiness directives, which are mandatory for the continued airworthiness of aircraft. In this context, AD/F28/14 pertains to the Fokker F28 Series Aeroplanes and mandates modifications to the aileron control system for specific serial numbers, namely those ranging from 11003 to 11031 and 11991 to 11994 (Section 105.130(1)). The directive requires these aircraft to undergo a detailed inspection and, if necessary, modification of the aileron control system to ensure compliance with safety standards (Section 105.130(2)).
Operators and owners of the specified Fokker F28 aircraft must adhere to the requirements set forth in AD/F28/14. This includes ensuring that the aircraft are inspected and modified according to the detailed specifications provided in the accompanying document, Fokker SB F28/27-47. Operators must maintain records of the modifications performed and keep these records readily available for inspection by CASA officers (Section 105.135). Furthermore, any repairs or maintenance work must be carried out by personnel who are qualified and certified according to the regulations, ensuring that the modifications are performed to the required safety standards (Section 105.135(3)).
Failure to comply with the airworthiness directive AD/F28/14 can result in significant legal consequences. Operators who do not adhere to the directive may face enforcement actions under Section 105.130(4), which can include fines and penalties. The maximum penalty for non-compliance can amount to substantial financial sanctions, reflecting the seriousness of ensuring aircraft safety. Additionally, CASA has the authority to ground non-compliant aircraft, which can result in significant operational disruptions and financial losses for the operators (Section 105.130(5)). In severe cases, repeated non-compliance or safety violations can lead to more severe penalties, including potential criminal charges for those responsible (Section 105.130(6)).