AD/PA-30/18 - Bonding Points - Installation

Overview

The Civil Aviation Regulations 1998, amended by F2006B05660, addresses safety concerns related to bonding points on Piper PA-30 and 39 (Twin Comanche) series aeroplanes. This legislative instrument was enacted by the Commonwealth of Australia to ensure compliance with safety standards in civil aviation, particularly focusing on the installation of bonding points for refuelling equipment and ground connections. The policy objective is to enhance the safety of aviation operations by mandating specific bonding installations that prevent static electricity discharges during refuelling and ground operations. The enactment ensures that all models of the specified aircraft series must adhere to these safety directives immediately upon the release of the legislative instrument.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 under the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, apply to all models of Piper PA-30 and 39 (Twin Comanche) series aeroplanes. The regulation mandates that each fuel filling point must be equipped with a positive method for bonding refuelling equipment to the aeroplane to ensure safety during refuelling operations. Additionally, a clearly identified external bonding point must be present on each main undercarriage assembly or on the nose gear, facilitating the attachment of ground connections. Compliance with these directives is required forthwith, underscoring the importance of immediate action to maintain airworthiness standards. This regulation extends across the Commonwealth of Australia, ensuring consistent safety standards are applied nationally. It is important to note that the regulation does not specify any exclusions, exemptions, or thresholds, thereby applying uniformly to all relevant aircraft within the designated scope.

Key Provisions

The Civil Aviation Regulations 1998, particularly Part 39 - 105, mandate specific safety directives for certain types of aircraft, such as the Piper PA-30 and 39 (Twin Comanche) series aeroplanes, as outlined in AD/PA-30/18. This directive focuses on bonding points for refuelling and ground connections. According to section 1, the requirement is that each fuel filling point must have a positive method for bonding the refuelling equipment to the aeroplane (1/72). Additionally, a clearly identified external bonding point must be present on each main undercarriage assembly or the nose gear, suitable for attaching ground connections (1/72). The obligations imposed by these regulations are straightforward but critical. Aircraft operators must ensure that bonding points are correctly installed and functional at all fuel filling points. This involves not only the installation of the bonding method but also regular checks to confirm that the bonding points remain effective and intact. For the main undercarriage assembly or nose gear, operators must ensure that the external bonding point is clearly marked and suitable for ground connections. This ensures that there is a reliable and safe method for conducting refuelling and other ground operations, reducing the risk of static electricity discharge which could potentially lead to fuel ignition or other hazards. Failure to comply with these directives can lead to significant consequences. The regulations specify that compliance must be achieved forthwith (1/72). This implies that any non-compliance could be subject to enforcement actions by the Civil Aviation Safety Authority (CASA). Potential penalties for non-compliance could include fines, operational restrictions, or even grounding of the aircraft until the bonding points are properly installed and verified. In severe cases, repeated non-compliance or failure to address safety issues promptly could lead to more serious civil or criminal penalties as prescribed by the Civil Aviation Act 1988 and other related legislation. The exact penalties would depend on the severity and impact of the non-compliance, but the regulations are clear in their requirement for immediate and thorough compliance to ensure the safety of the aircraft and its operations.