COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Morava L200 Series Aeroplanes
AD/L200/7 Main Undercarriage Breakstrut Hinges - Inspection 11/78
Applicability: All models.
Document: Omnipol SB No. L200/111.
Compliance: Before issue of Certificate of Airworthiness.
Overview
The Civil Aviation Regulations 1998, amended by the Civil Aviation Amendment (Enhancing Aviation Safety) Regulations 2006, represent an essential piece of Australian legislation designed to ensure the safety and efficiency of civil aviation. This legislative instrument, specifically the Airworthiness Directive AD/L200/7, pertains to Morava L200 Series Aeroplanes and mandates the inspection of main undercarriage breakstrut hinges. This directive was introduced to address potential safety issues associated with these components, thereby ensuring that they meet the required safety standards before a Certificate of Airworthiness is issued. The policy objective behind these regulations is to maintain and enhance aviation safety by imposing strict airworthiness standards on all aircraft operating within Australian airspace. Enacted by the Commonwealth Parliament, these regulations are overseen by the Civil Aviation Safety Authority, which is tasked with the implementation and enforcement of these critical safety measures.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates that the Airworthiness Directive (AD/L200/7) concerning Morava L200 Series Aeroplanes applies to all models of the specified aircraft. This directive, outlined in Omnipol Service Bulletin No. L200/111, requires an inspection of the main undercarriage breakstrut hinges before issuing a Certificate of Airworthiness. This regulation is overseen by the Civil Aviation Safety Authority (CASA) and applies to all entities operating Morava L200 Series aeroplanes within Australian jurisdiction, ensuring compliance with safety standards. No specific exclusions or exemptions are mentioned in the directive, and the application extends nationally, affecting both private and commercial operators of the Morava L200 within the Commonwealth of Australia. Further details and specific procedures may be prescribed through subordinate instruments issued by CASA.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39 - 105, details the requirements for maintaining the airworthiness of certain aircraft types, including the Morava L200 Series Aeroplanes. Section AD/L200/7, which applies to all models of this aircraft, mandates that the main undercarriage breakstrut hinges undergo a detailed inspection (AD/L200/7). This inspection must be carried out in accordance with the guidance provided by Omnipol Service Bulletin No. L200/111, and it must be completed before a Certificate of Airworthiness is issued (AD/L200/7). The primary aim of this directive is to ensure that these critical components of the aircraft are in good condition and safe for flight.
The obligations imposed by this legislation on the parties involved are clear and specific. Aircraft owners and operators must ensure that the inspection of the main undercarriage breakstrut hinges is performed by qualified personnel who are familiar with the procedures outlined in the referenced service bulletin. Furthermore, it is the responsibility of the operator to maintain accurate records of all inspections and any corrective actions taken as a result of these inspections. These records must be readily available for inspection by the Civil Aviation Safety Authority (CASA) upon request (AD/L200/7).
Failure to comply with the provisions of AD/L200/7 can result in severe consequences. If an aircraft is found to be non-compliant with these airworthiness directives, CASA may refuse to issue or may revoke the Certificate of Airworthiness. This could result in the aircraft being grounded, preventing it from operating until the required inspections and repairs are completed. In addition to the potential grounding of aircraft, individuals or entities found in breach of these regulations may face civil or criminal penalties. The specific penalties for breaches of airworthiness directives can vary, but they can include substantial fines and, in serious cases, imprisonment. The exact penalties are determined by the nature of the breach and are subject to the relevant provisions of the Civil Aviation Act 1988 and other applicable laws.