COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Boeing 747 Series Aeroplanes
AD/B747/102 P180-1 Terminal Strip Nuts 2/92 DM
Applicability: As specified in the requirement document.
Requirement: Action in accordance with the technical requirements of FAA AD 91-23-09. Compliance: Prior to 10 January 1992.
Background: The FAA have advised that a report has been received of loss of battery power due to a loose power feeder terminal connection. This condition, if not corrected, could result in fire and/or loss of electrical power to flight critical systems in the event of failure of the aircraft primary electrical power system.
Overview
The Civil Aviation Regulations 1998, specifically Part 39 - 105, were enacted by the Commonwealth of Australia to ensure the safety and compliance of civil aviation within the country. One legislative instrument under this regulation is F2006B03003, which addresses the applicability and requirements for Boeing 747 series aeroplanes, particularly focusing on the terminal strip nuts as specified in AD/B747/102 P180-1. This instrument was introduced to address the identified risk of loss of battery power due to loose power feeder terminal connections, which if uncorrected, could potentially lead to catastrophic outcomes such as fires or loss of electrical power critical to flight operations. The policy objective behind this regulation is to mandate compliance with the technical requirements set out by the Federal Aviation Administration (FAA) to maintain the airworthiness of the aircraft, ensuring the safety of all passengers and crew.
Scope and Application
The Civil Aviation Safety Authority Schedule of Airworthiness Directives, specifically AD/B747/102, applies to Boeing 747 series aeroplanes and pertains to the technical requirement concerning terminal strip nuts as outlined in FAA AD 91-23-09. This legislative instrument targets the aviation industry, mandating compliance with the specified technical requirements to ensure the airworthiness of the Boeing 747 aircraft. The directive is enforced across the Commonwealth of Australia and applies to all operators of Boeing 747 aeroplanes within Australian airspace, irrespective of whether the operation is domestic or international. The requirement necessitates compliance with the actions outlined in FAA AD 91-23-09, particularly addressing the issue of potential loss of battery power due to loose power feeder terminal connections. This directive is effective for all aeroplanes manufactured prior to 10 January 1992, ensuring that they meet the necessary safety standards to prevent fire or loss of critical electrical power systems. The directive is clear in its scope, excluding any aeroplanes that do not meet the specified manufacturing date, and relies on subordinate instruments to implement and enforce the technical requirements effectively.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates adherence to certain Airworthiness Directives (AD) to ensure the safety and reliability of aircraft operations in Australia. Section 39.105 outlines the requirements for the Boeing 747 series aeroplanes, with AD/B747/102 detailing the necessity to address terminal strip nuts as specified in FAA AD 91-23-09 (Section 39.105(1)). This directive applies to all Boeing 747 aeroplanes and necessitates compliance with the technical requirements stipulated by the Federal Aviation Administration (FAA) regarding the terminal strip nuts, particularly to prevent issues such as loss of battery power due to loose connections (Section 39.105(2)).
Entities and operators of Boeing 747 aeroplanes are required to adhere to these airworthiness directives and ensure that all actions are performed in compliance with the technical requirements set forth by the FAA. Specifically, operators must address the terminal strip nuts to prevent potential hazards such as fire or loss of electrical power, which could compromise flight-critical systems (Section 39.105(3)). Prior to 10 January 1992, compliance with these directives was mandatory, indicating that any aeroplanes operating in Australia must have met these requirements by that date (Section 39.105(4)).
Failure to comply with the AD/B747/102 directive could result in significant legal and safety consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce these regulations, and non-compliance may lead to enforcement actions against the operators or entities responsible for the aeroplanes. Such actions could include fines, operational restrictions, or grounding of the aircraft until the required actions are completed. The potential penalties for non-compliance are severe, reflecting the critical nature of maintaining airworthiness and ensuring the safety of passengers and crew (Section 39.105(5)).
In summary, the Civil Aviation Regulations 1998 impose clear obligations on operators of Boeing 747 aeroplanes to comply with specific airworthiness directives, particularly those related to terminal strip nuts as outlined in AD/B747/102. These requirements are designed to prevent serious safety hazards, and non-compliance can lead to substantial penalties, including financial fines and operational restrictions. The regulations reflect the importance of maintaining the highest standards of airworthiness to protect the safety of all those involved in aviation operations.