COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Oxygen Systems
AD/OXY/5 Scott Oxygen Mask Connectors 4/86
Applicability: Scott Aviation oxygen connectors P/Nos 289-56 and 289-56-1.
Note: The constant flow oxygen mask to which the affected connectors may be fitted include, but are not necessarily limited to the following Scott part numbers:
289-127, 289-127-2, 289-127-4, 289-128, 289-128-2, 289-360, 289-395, 289-701-23,
289-701-24, 289-701-223, 289-601-6, 289-601-13, 289-601-17, 289-601-206, 289-
601-213, 289-601-217.
Requirement: Action in accordance with Scott Aviation Service Bulletin 289-35-10. Compliance: Within 30 days after 30 April 1986.
Note: FAA AD 85-26-03 Amdt. 39-5182 refers.
Background: To prevent the blockage of oxygen flow due to incompletely drilled oxygen connectors.
Overview
The Civil Aviation Regulations 1998, as amended, is a comprehensive set of rules enacted by the Parliament of Australia to ensure the safety and efficiency of civil aviation within the country. Specifically, Part 39 - 107 of the Regulations pertains to the Civil Aviation Safety Authority's schedule of airworthiness directives, which includes directives related to oxygen systems on aircraft. One such directive, AD/OXY/5, mandates action on Scott Aviation oxygen connectors P/Nos 289-56 and 289-56-1, requiring compliance with Scott Aviation Service Bulletin 289-35-10 to prevent oxygen flow blockages caused by incompletely drilled connectors. This directive aims to address a safety gap by ensuring that oxygen connectors meet specific standards to maintain uninterrupted oxygen flow, thus enhancing the safety of in-flight oxygen systems. The enactment of these regulations and directives underscores the Civil Aviation Safety Authority's commitment to stringent safety measures and the mitigation of aviation risks.
Scope and Application
The Civil Aviation Safety Authority's (CASA) Airworthiness Directives, specifically AD/OXY/5 concerning Scott oxygen mask connectors, apply to the Scott Aviation oxygen connectors with part numbers 289-56 and 289-56-1. These directives are pertinent to the safety of constant flow oxygen masks, which may include various Scott part numbers such as 289-127, 289-127-2, and others listed in the directive. This regulation applies to all aircraft operators within the Commonwealth of Australia, ensuring adherence to safety standards within the aviation industry. Compliance with these directives is mandatory, requiring corrective actions in accordance with the Scott Aviation Service Bulletin 289-35-10, to be completed within 30 days after 30 April 1986. The directive aims to prevent the blockage of oxygen flow due to incompletely drilled oxygen connectors, thereby maintaining the integrity of oxygen supply systems in aircraft.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39, Section 107, mandates the Airworthiness Directives concerning oxygen systems, with AD/OXY/5 focusing on Scott Oxygen Mask Connectors. The directive applies to Scott Aviation oxygen connectors with part numbers 289-56 and 289-56-1. It specifically addresses the need to address the risk of oxygen flow blockages due to incompletely drilled connectors. These connectors may be used in various Scott Aviation oxygen masks, including but not limited to part numbers 289-127, 289-127-2, and others as listed. The directive requires operators to follow the action specified in Scott Aviation Service Bulletin 289-35-10. Compliance with this directive must be achieved within 30 days following 30 April 1986.
Entities governed by these regulations are obliged to ensure that the specified Scott Aviation oxygen connectors are in compliance with the requirements set out in Service Bulletin 289-35-10. This involves taking the necessary steps to prevent oxygen flow blockages by ensuring that the connectors are correctly and fully drilled. These obligations extend to all aircraft operators, maintenance organisations, and other relevant entities that must adhere to the directives to maintain the safety and airworthiness of aircraft. Non-compliance with these directives could result in compromised safety and potential regulatory penalties.
Failure to comply with the provisions of AD/OXY/5 may lead to enforcement actions by the Civil Aviation Safety Authority (CASA). The consequences of non-compliance can include enforcement notices, fines, and potential grounding of aircraft until the necessary actions are taken to ensure compliance. While the specific penalties are not detailed in the text, non-compliance with airworthiness directives generally carries significant legal and financial repercussions. It is critical for all affected parties to adhere to these directives to avoid any adverse outcomes.