AD/BEECH 200/41 Amdt 2 - Fuel Boost Pumps

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, serve to regulate the safety and airworthiness of civil aviation operations within the country. Specifically, Part 39 - 105 of these regulations provides for the issuance of Airworthiness Directives to ensure aircraft meet safety standards. The Civil Aviation Safety Authority (CASA) is the enacting body responsible for these directives. This particular Airworthiness Directive, AD/BEECH 200/41 Amendment 2, addresses a critical safety issue concerning the fuel boost pumps in Beechcraft 200 (Super King Air) series aeroplanes. The directive was introduced to address the problem of leaking fuel boost pumps, which could compromise the safety of the aircraft. The policy objective is to mandate regular inspections and modifications to prevent fuel leaks, thereby enhancing the overall safety of the aircraft and protecting the lives of passengers and crew.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, govern the airworthiness directives for various aircraft, including the Beechcraft 200 (Super King Air) series aeroplanes as detailed in AD/BEECH 200/41 Amendment 2. This legislation applies to certain Beechcraft 200 series aeroplanes, including Super King Air 200, B200, B200C, B200CT, 200T, and B200T models with specific serial numbers and fuel boost pump serial number date codes. The application of these regulations is mandatory for any of the specified aircraft that are equipped with Airborne fuel boost pumps having particular serial number date codes and repair station nameplate dates. The compliance requirements mandate an initial inspection and necessary modifications within a specified timeframe and before further flights or installations, as stipulated by the manufacturer’s service bulletin. This Act extends its reach to ensure the safety and airworthiness of the mentioned aircraft, encompassing the entire Commonwealth of Australia. No exclusions or exemptions are noted within the provided text, although the scope and enforcement may be further detailed or modified through subordinate instruments.

Key Provisions

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, includes the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives. One such directive, AD/BEECH 200/41 Amendment 2, concerns the fuel boost pumps on Beechcraft 200 (Super King Air) series aeroplanes. This directive applies to aircraft equipped with specific Airborne fuel boost pumps that have serial number date codes ranging from 5H through 12H, IJ through 12J, and all Airborne overhauled boost pumps dated between 5-81 and 12-83 (Section 9/86). The directive specifies particular serial numbers and models of Super King Air 200 and B200, B200C, B200CT, 200T, and B200T series aeroplanes that are subject to these requirements. The main requirement outlined in this directive is to perform an initial inspection in accordance with Step 1 and subsequent modifications as per Steps 3 and 4 of the Requirement Document (Beechcraft SB No. 2156). Furthermore, any leaking boost pumps must be replaced following Step 2 of the Requirement Document, and any affected pumps held as spares must be inspected in line with the same document (Section 9/86). Compliance must be achieved within 100 hours of time in service after 30 September 1986 or before 31 March 1987, whichever comes first (Section 9/86). The modifications must also be completed before further flight after the initial inspection and before the installation of any affected pumps in an aircraft after 30 September 1986. It is important to note that compliance with previous versions of this directive does not suffice, and a new certification is required. The obligations imposed by this directive are stringent and clear. Operators of the specified Beechcraft 200 series aeroplanes must ensure that all fuel boost pumps meeting the criteria set out in the directive are inspected and modified as required. This includes conducting the initial inspection within the specified timeframe and replacing any leaking pumps immediately. Additionally, operators must ensure that any affected pumps held as spares are also inspected according to the Requirement Document. These obligations are designed to maintain the safety and airworthiness of the aircraft, ensuring that they meet the required standards set forth by CASA. Failure to comply with the provisions of this directive can lead to serious consequences. While the specific penalties for non-compliance are not detailed in the text, under the Civil Aviation Regulations 1998, breaches of airworthiness directives can result in significant penalties. These may include fines, suspension or revocation of the aircraft's certificate of airworthiness, and potential criminal charges for operators or maintenance personnel found guilty of neglecting their obligations. The seriousness of these consequences underscores the importance of adhering to the requirements set out in the directive to ensure the safety and compliance of the affected aircraft.