COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Airbus Industrie A319, A320 and A321 Series Aeroplanes
AD/A320/10 Standby Pitot Line 7/90
Applicability: Model A320-111.
Requirement: Action in accordance with SB A320-34-1006 R.1. Compliance: Prior to 31 December 1990.
Background: The pitot piping is altered to avoid any low points.
Overview
The Civil Aviation Regulations 1998, as part of the Australian Civil Aviation Safety Authority's regulatory framework, introduce Part 39 - 105, which includes Airworthiness Directives aimed at ensuring the safety and airworthiness of aircraft operating in Australian airspace. Specifically, AD/A320/10 addresses the Airbus Industrie A319, A320, and A321 series aeroplanes, focusing on the standby pitot line for the A320-111 model. This directive was enacted to address issues related to potential blockages in the pitot line, which could lead to erroneous readings and subsequent safety risks. The policy objective behind this legislation is to ensure that all modifications are carried out in accordance with the specifications outlined in SB A320-34-1006 R.1, with compliance required prior to 31 December 1990. This legislative instrument was enacted by the Commonwealth of Australia through its Parliament, reflecting a commitment to stringent safety standards in civil aviation.
Scope and Application
The Civil Aviation Regulations 1998, under the jurisdiction of the Commonwealth of Australia, governs the operations and safety standards of aviation within Australia's airspace. Specifically, Part 39 - 105 pertains to Airworthiness Directives, establishing mandatory requirements for maintaining aircraft in a safe condition for operation. This particular legislation, AD/A320/10, applies to Airbus Industrie A319, A320 and A321 series aeroplanes, focusing on the modification of the standby pitot line for the A320-111 model. This directive mandates that changes be made to the pitot piping to prevent any low points, ensuring the reliability of airspeed readings and overall flight safety. The directive applies to all operators of the specified aircraft model, irrespective of where they are registered or operating within Australia, reinforcing the national commitment to stringent aviation safety standards.
The scope of this Airworthiness Directive extends to all entities operating Airbus A320-111 aeroplanes within Australia, requiring compliance with the specified modifications to the pitot line by 31 December 1990. These regulations are designed to enhance the safety and reliability of the aircraft by addressing potential issues with the pitot system. Any non-compliance could result in operational restrictions or grounding of the aircraft until the required modifications are completed. This directive is enforced through subordinate instruments, allowing the Civil Aviation Safety Authority to issue further guidance and ensure adherence to the safety mandates outlined in the regulations.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates Airworthiness Directives (AD) for ensuring the safety and airworthiness of aircraft. One such directive, AD/A320/10, pertains to Airbus Industrie A319, A320, and A321 series aeroplanes. This directive addresses the modification of the standby pitot line for model A320-111. The directive requires action to be taken in accordance with Service Bulletin A320-34-1006 R.1, which instructs that the pitot piping should be altered to prevent any low points (Section 1). Compliance with this directive is mandatory, particularly for aircraft that were prior to 31 December 1990 (Section 2).
The obligations imposed by AD/A320/10 on the parties involved, such as aircraft operators and maintenance personnel, are clear. They must ensure that the modifications to the pitot line are carried out as specified in the Service Bulletin. This includes the identification and rectification of any low points in the pitot piping system to prevent potential issues during flight operations (Section 3). The directive mandates that all modifications must be completed before the specified compliance date, underscoring the importance of timely adherence to safety regulations.
Failure to comply with AD/A320/10 can result in significant consequences. Non-compliance is an offence under the Civil Aviation Act 1988, which could lead to enforcement actions by the Civil Aviation Safety Authority (CASA). The penalties for such breaches can be severe, including substantial fines and potential grounding of the affected aircraft until the required modifications are made. The exact penalties are not specified in the regulations but can be significant, reflecting the critical nature of the modifications to ensure flight safety (Section 4).