COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 400 Series Aeroplanes
AD/BEECH 400/1 Aft Fuel Tank Vent 12/92 DM
Applicability: Model 400A serial number RK-1 to RK-28 inclusive.
Requirement: Unless previously carried out action in accordance with the Accomplishment Instructions contained in Beechcraft mandatory service bulletin No 2445.
Note: FAA AD 92-16-14 amdt 39-8323 refers.
Compliance: Prior to 25 September 1992.
Background: To prevent a potential fire or explosive situation a one time inspection of the aft fuselage vent system to ensure aluminium honeycomb material is installed, is required.
Overview
The Civil Aviation Regulations 1998, specifically Part 39 - 105, address the safety concerns related to the airworthiness of Beechcraft 400 Series aeroplanes through the issuance of Airworthiness Directives (ADs). This legislation was enacted to ensure that aircraft meet specific safety standards, thereby reducing the risk of accidents and ensuring the safety of passengers and crew. The objective of AD/BEECH 400/1, which pertains to the aft fuel tank vent of Beechcraft 400A models with serial numbers RK-1 to RK-28, is to prevent potential fire or explosive situations by mandating a one-time inspection of the aft fuselage vent system to ensure the correct installation of aluminium honeycomb material. This directive aligns with the broader policy objective of maintaining high safety standards in civil aviation by addressing specific design and maintenance issues that could compromise aircraft safety. The regulations are enforced by the Civil Aviation Safety Authority, which is tasked with ensuring compliance with these safety directives.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertain to the Civil Aviation Safety Authority’s Schedule of Airworthiness Directives, which includes the AD/BEECH 400/1 concerning the aft fuel tank vent of Beechcraft 400 Series aeroplanes. This regulation applies to Model 400A aeroplanes with serial numbers ranging from RK-1 to RK-28 inclusive, and mandates a one-time inspection of the aft fuselage vent system to ensure that aluminium honeycomb material is correctly installed. This directive aims to prevent potential fire or explosive situations and requires compliance prior to 25 September 1992, unless the action has already been completed as per the Accomplishment Instructions in Beechcraft mandatory service bulletin No 2445. The regulation aligns with FAA AD 92-16-14 Amendment 39-8323, thereby extending its jurisdictional reach to align with international standards. The scope of this Act is limited to the specified Beechcraft 400A models and does not explicitly mention any exclusions or exemptions beyond the conditions outlined in the directive. The regulation's application may also be influenced by subordinate instruments, which could provide further clarification or additional requirements.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, contain the Airworthiness Directive (AD) pertaining to Beechcraft 400 Series Aeroplanes. Section AD/BEECH 400/1 focuses on the aft fuel tank vent, providing a detailed requirement for a specific model range. The directive applies to Model 400A aeroplanes with serial numbers RK-1 to RK-28 inclusive, unless an earlier inspection and corrective action have been performed in line with the Accomplishment Instructions in Beechcraft mandatory service bulletin No 2445. The directive references FAA AD 92-16-14 amendment 39-8323, indicating alignment with international safety standards.
Under this directive, operators and owners of the specified Beechcraft 400A aeroplanes must ensure a one-time inspection of the aft fuselage vent system. The primary objective of this inspection is to confirm that the aluminium honeycomb material is correctly installed, thereby preventing potential fire or explosive situations. Compliance with this directive must be achieved before 25 September 1992, underscoring the urgency and importance of this safety measure.
The obligations imposed by this Act are clear and specific. Operators and owners must conduct the inspection as mandated, ensuring the installation of the correct materials in the aft fuselage vent system. Failure to comply with these requirements could result in safety hazards, potentially leading to catastrophic outcomes. Therefore, adherence to the inspection and corrective action protocols is not only a regulatory requirement but also a critical safety measure.
In the event of non-compliance with the AD/BEECH 400/1 directive, several potential consequences may arise. While the specific penalties or consequences are not detailed in the text, breaches of safety regulations under the Civil Aviation Regulations 1998 can lead to significant legal ramifications. These may include fines, operational restrictions, or even the grounding of the affected aircraft. The seriousness of these potential penalties highlights the importance of strict adherence to the directive’s requirements.