AD/BEECH 55/12 Amdt 1 - Operating Restriction Placard

Overview

The Civil Aviation Regulations 1998, specifically Part 39, Section 105, was enacted to ensure the safety of civil aviation within Australia, addressing issues related to the airworthiness of aircraft and the safety protocols that must be followed. This regulation was introduced to provide comprehensive guidelines and directives to maintain high standards of safety in the aviation industry, ensuring that aircraft meet specific airworthiness criteria. The regulations were established by the Parliament of Australia, with the overarching policy objective of protecting public safety by enforcing stringent safety measures and operational standards on aircraft and aviation operations within the country. One of the specific amendments to these regulations is AD/BEECH 55/12, which applies to Beechcraft 55, 58, and 95-55 (Baron) series aeroplanes. This amendment mandates the installation of placards on the fuel selector panels of these aircraft to highlight critical operational restrictions. For aircraft equipped with auxiliary fuel tanks, a placard must be installed indicating that the use of auxiliary fuel tanks and crossfeed is only permissible during level flight. Additionally, for aircraft not fitted with baffled fuel cells, another placard must be installed to prohibit turning-type take-offs or take-offs immediately following fast taxi turns. These placards are essential for ensuring that pilots adhere to the necessary safety protocols, thereby mitigating potential risks associated with improper fuel management and operational procedures.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, governs the airworthiness directives for certain aircraft, including the Beechcraft 55, 58, and 95-55 (Baron) series aeroplanes, through the Airworthiness Directive AD/BEECH 55/12 Amendment 1. This regulation applies to specific models of the Beechcraft series, namely 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, and D-55A. The directive mandates that for aircraft equipped with auxiliary fuel tanks, a placard must be installed on the leading edge of the fuel selector panel indicating the restriction of using the auxiliary fuel tanks and crossfeed in level flight only. Additionally, for aircraft not fitted with baffled fuel cells, a placard must be placed on the leading edge of the fuel selector panel prohibiting turning type take-offs or take-offs immediately following fast taxi turns. Compliance with these placard installations is required for aircraft manufactured before 1 September 1971. The regulation operates under the jurisdiction of the Commonwealth of Australia and is enforced by the Civil Aviation Safety Authority, ensuring adherence to safety standards across the nation.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39, specifically in Section 39-105, detail the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives for Beechcraft 55, 58, and 95-55 (Baron) series aeroplanes. This directive, known as AD/BEECH 55/12 Amendment 1, pertains to the installation of specific placards on these aircraft models to ensure safety during operation. The directive applies to models 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, and D-55A. Under Section 39-105, the directive mandates two key placard installations. Firstly, for aircraft equipped with auxiliary fuel tanks, a placard must be affixed to the leading edge of the fuel selector panel. The placard should bear the warning: "USE AUXILIARY FUEL TANKS AND CROSSFEED IN LEVEL FLIGHT ONLY." Secondly, for aircraft without baffled fuel cells, another placard must be placed on the leading edge of the fuel selector panel, stating: "TURNING TYPE TAKE-OFFS OR TAKE-OFFS IMMEDIATELY FOLLOWING FAST TAXI TURN ARE PROHIBITED." These placards are intended to highlight operational restrictions and enhance safety during flight. Operators and owners of the specified Beechcraft models must ensure compliance with these requirements before 1 September 1971. Failure to install the required placards as mandated by Section 39-105 may result in non-compliance with aviation safety standards. It is the responsibility of the aircraft operators to adhere to these directives to maintain airworthiness and ensure safe operations. Failure to comply with the provisions outlined in Section 39-105 of the Civil Aviation Regulations 1998 can lead to significant consequences. Operators who do not install the required placards on their Beechcraft 55, 58, and 95-55 series aeroplanes may face enforcement actions from CASA. While the specific penalties are not detailed in the legislative instrument provided, non-compliance with airworthiness directives generally can result in civil penalties, including fines, and potential criminal charges if the non-compliance leads to safety incidents. The severity of the penalties depends on the nature and extent of the non-compliance and any resultant harm. It is essential for operators to diligently adhere to these directives to avoid adverse outcomes.