AD/CESSNA 310/34 - Main Landing Gear Trunnion - Inspection

Overview

The Civil Aviation Regulations 1998, as amended by the legislative instrument F2006B08161, were enacted to establish a comprehensive regulatory framework governing civil aviation in Australia, addressing gaps and ensuring the safety and efficiency of the aviation sector. This particular amendment, introduced by the Commonwealth of Australia, targets specific maintenance and operational standards for aircraft, aiming to enhance the safety and reliability of aviation operations. The regulation focuses on the Cessna 310 series aeroplanes, specifically mandating inspections of the main landing gear trunnion for model 310Q with serial numbers ranging from 1038 to 1145. The policy objective is to mitigate risks associated with structural integrity and ensure compliance with established safety directives, thereby safeguarding passengers and crew.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the safety standards and directives for various aircraft models, including the Cessna 310 Series aeroplanes. In this context, the legislation applies to all model 310Q aeroplanes with serial numbers ranging from 1038 to 1145. The regulations mandate that these aircraft must adhere to the Airworthiness Directives concerning the inspection of the main landing gear trunnion, as detailed in the requirement document Cessna SL No. M 74-14. Compliance with these directives is essential for ensuring the continued airworthiness and safety of the specified aircraft models. The regulations extend to the entire Commonwealth of Australia, applying to all operators and owners of the affected Cessna 310Q aircraft within the national jurisdiction. There are no exclusions or exemptions mentioned within the specified scope of the legislation, and the directives are to be strictly followed as per the requirements outlined in the accompanying document.

Key Provisions

The Civil Aviation Regulations 1998, particularly Part 39 - 105, contains specific directives concerning the airworthiness of aircraft, including the Cessna 310 Series Aeroplanes. Section AD/CESSNA 310/34 mandates an inspection of the main landing gear trunnion for all model 310Q Cessna aircraft with serial numbers ranging from 1038 to 1145. This inspection directive is applicable to ensure the continued safety and airworthiness of these specific aircraft models, as outlined in document Cessna SL No. M 74-14. Compliance with this directive must be achieved in accordance with the specified requirements outlined in the aforementioned document. The obligations imposed by these regulations are quite clear and centre around ensuring that the specified aircraft undergo a thorough inspection of their main landing gear trunnions. This is essential to maintain the structural integrity and safety of the aircraft. Operators and owners of the affected Cessna 310Q aircraft are required to follow the detailed inspection procedures provided in document Cessna SL No. M 74-14. These procedures must be adhered to meticulously to ensure that any potential issues with the main landing gear trunnion are identified and addressed promptly. Failure to comply with the airworthiness directives stipulated in the Civil Aviation Regulations 1998 can lead to serious consequences. Non-compliance with Section AD/CESSNA 310/34 could result in the aircraft being deemed unfit to fly, which poses significant safety risks. The regulations do not explicitly state penalties within this particular section, but non-compliance with civil aviation regulations generally can lead to severe penalties, including fines, suspension or revocation of aircraft operating certificates, and potential criminal charges. The severity of these penalties underscores the importance of adhering to the inspection requirements set forth by the Civil Aviation Safety Authority.