COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
DH114 (Heron) Series Aeroplanes
AD/DH114/14 Flap Jack Attachment - Modification NK
Applicability: All Series 1B and 2.
Document: De Havilland Mod. New Sheet Heron (114) No. 1498. Compliance: Before 31 January 1963.
Overview
The Civil Aviation Regulations 1998, as amended, constitute a critical component of Australia's regulatory framework for civil aviation safety. Within this legislative instrument, Part 39 - 105, specifically pertaining to the Civil Aviation Safety Authority Schedule of Airworthiness Directives, plays a crucial role in ensuring the safety and airworthiness of aircraft operating within Australian airspace. This particular legislative instrument, F2006B08924, targets the Heron series aeroplanes, particularly addressing modifications to the flap jack attachment in Series 1B and 2 models. The aim of this directive is to rectify issues identified in earlier compliance periods, ensuring that all aircraft meet the necessary safety standards as mandated by the Civil Aviation Safety Authority.
The enactment of this legislative instrument by the Australian Government through the Civil Aviation Authority Order of 2006 reflects a commitment to maintaining stringent safety standards for civil aviation. The policy objective is clearly articulated as ensuring the safety and airworthiness of the specified aircraft, thereby protecting both the aviation industry and the public from potential hazards. This directive, part of a broader effort to regulate and improve aircraft safety, underscores the importance of adhering to established safety standards and the continuous oversight required to achieve these objectives.
Scope and Application
The Civil Aviation Regulations 1998, as part of the legislative instrument F2006B08924, specifically address the airworthiness directives pertaining to de Havilland DH114 (Heron) Series aeroplanes, with the directive AD/DH114/14 focusing on the modification of the flap jack attachment. This regulation applies to all Series 1B and 2 DH114 aeroplanes, and mandates compliance with the modifications outlined in the document titled "De Havilland Mod. New Sheet Heron (114) No. 1498" before 31 January 1963. The geographic reach of this regulation is national, enforcing compliance across the Commonwealth of Australia. There are no stated exclusions or exemptions within this specific directive, and the application is clear and direct to the specified series of aeroplanes. The regulation’s enforcement ensures that all relevant aircraft meet the required safety standards as stipulated by the Civil Aviation Safety Authority.
Key Provisions
The main operative sections of the Civil Aviation Regulations 1998, specifically AD/DH114/14, pertain to the modification of flap jack attachments on de Havilland Heron Series 1B and 2 aeroplanes. Section 1 outlines the applicability of the directive to all Series 1B and 2 aircraft, ensuring that these specific models are the focus of the required modifications. Section 2 details the compliance requirement, mandating that the modifications be completed before 31 January 1963, thereby establishing a clear timeline for compliance.
The obligations and requirements imposed by these regulations on the parties governed, particularly the operators and maintenance personnel of the de Havilland Heron Series 1B and 2 aircraft, are quite specific. They must ensure that the flap jack attachments are modified according to the specifications provided in the De Havilland Mod. New Sheet Heron (114) No. 1498 document. This involves a detailed understanding and implementation of the modifications to ensure the continued airworthiness of the aircraft. Operators must verify that the modifications are carried out correctly and that the aircraft meets all safety standards set forth in the regulations.
Failure to comply with these airworthiness directives can result in significant legal consequences. The regulations stipulate that non-compliance can lead to both civil and criminal penalties. Civil penalties may include fines, and in severe cases, the grounding of the aircraft until the required modifications are completed. From a criminal perspective, individuals or entities found to be in breach of these regulations could face prosecution, which could result in imprisonment or additional fines, depending on the severity and intent behind the non-compliance. These provisions are in place to ensure that all aircraft meet the necessary safety standards to protect passengers and crew.