AD/BEECH 200/3 Amdt 1 - Propeller Secondary Low Pitch Stop System

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, were amended by Legislative Instrument F2006B03686 to address specific safety concerns in civil aviation, particularly focusing on the airworthiness of aircraft. This legislative instrument introduces an airworthiness directive (AD) specifically for Beechcraft 200 (Super King Air) Series aeroplanes, mandating compliance with a prescribed modification to the propeller secondary low pitch stop system. The objective of this amendment is to ensure the safety and reliability of these aircraft models, specifically those with serial numbers BB-2, BB-6 to BB-162, by enforcing a compliance timeline within 100 hours of time in service following 31 May 1977. Additionally, it requires an amendment to the Flight Manual post-installation of the modification, ensuring all operational personnel are aware of the changes and can safely operate the aircraft. The AD/BEECH 200/3 Amendment 1, introduced under this legislative instrument, aligns with Beechcraft Service Instruction No 0808-247, Revision 1, and is designed to rectify identified safety issues by modifying the propeller system. This amendment was enacted by the relevant legislative authority to ensure that all specified aircraft meet the stringent safety standards set forth by the Civil Aviation Safety Authority, thereby mitigating potential risks associated with the identified deficiencies.

Scope and Application

The Civil Aviation Safety Authority Schedule of Airworthiness Directives, specifically AD/BEECH 200/3 Amendment 1, pertains to the propeller secondary low pitch stop system of Beechcraft 200 (Super King Air) Series aeroplanes, specifically models 200 with serial numbers ranging from BB-2 to BB-162. The directive mandates compliance with Beechcraft Service Instruction No 0808-247, Revision 1, within 100 hours of time in service following 31 May 1977. The directive applies to the aircraft models mentioned and requires a flight manual amendment after the modification is incorporated. The regulation is part of the Civil Aviation Regulations 1998, administered under the Commonwealth of Australia, thereby ensuring that the specified modifications are uniformly implemented across the national airspace. No exclusions or exemptions are explicitly stated in the directive, implying that all affected aircraft must comply with the prescribed action and timeframe.

Key Provisions

The Civil Aviation Regulations 1998, particularly Part 39 - 105, mandate the safety standards for aircraft operating within Australian airspace. Under this regulation, the Airworthiness Directives (AD) are crucial for ensuring that specific types of aircraft meet certain safety criteria. For instance, AD/BEECH 200/3 Amendment 1 pertains to the Beechcraft 200 (Super King Air) series aeroplanes, specifically addressing the propeller secondary low pitch stop system. This directive applies to models 200, with serial numbers ranging from BB-2 to BB-162, excluding BB-5 (section 5/77). Compliance with these directives is mandatory and requires adherence to the specified modifications as outlined in Beechcraft Service Information (SI) No 0808-247, Revision 1. For the affected Beechcraft 200 models, this means that any modifications or repairs related to the propeller secondary low pitch stop system must be completed within 100 hours of the aircraft being in service after 31 May 1977. Additionally, it is essential to update the Flight Manual to reflect any changes made in accordance with this directive to ensure that pilots are fully aware of the updated operational procedures and safety requirements. Failure to comply with the Airworthiness Directives can lead to significant legal and operational repercussions. The regulations impose strict obligations on aircraft owners, operators, and maintenance personnel to ensure that all safety directives are followed. Non-compliance can result in the aircraft being deemed unairworthy, which could lead to grounding and potential grounding of the aircraft until the necessary modifications are made. Additionally, there may be civil and criminal penalties imposed for non-compliance, which can include fines and imprisonment, depending on the severity of the breach. The exact penalties are determined by the relevant aviation authorities and may vary based on the specific circumstances of the case.