AD/BELL 205/36 - Fuel Boost Pumps - Inspection

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, form a comprehensive framework for the regulation of civil aviation within Australia. This legislation aims to ensure the safety and efficiency of air operations, including the establishment of standards for airworthiness, licensing, and operations of aircraft. One of the critical components of these regulations is the system of Airworthiness Directives (ADs), which address specific safety concerns by mandating corrective actions for particular types of aircraft. The 1998 Regulations were introduced to consolidate and update existing aviation laws, addressing gaps in safety standards and providing a more streamlined regulatory environment. The policy objective underpinning these regulations is to maintain and enhance the high level of safety in civil aviation through rigorous oversight and proactive management of safety risks.

Scope and Application

The Civil Aviation Regulations 1998, specifically within Part 39 - 105, govern the safety directives applicable to civil aviation in Australia, ensuring that aircraft, such as the Bell Helicopter Textron 205 series helicopters, meet stringent safety standards. This particular legislative instrument, AD/BELL 205/36, pertains to model 205A-1 helicopters with serial numbers prior to 30233, mandating a specific inspection of fuel boost pumps. This directive applies to all entities operating these helicopters and aims to enhance aviation safety by addressing potential issues identified in the fuel boost pumps. The regulation has a clear timeframe for compliance, requiring inspections to be completed within 100 hours of the helicopter's time in service following 30 November 1976, as detailed in Bell SB No. 205-76-14. The scope of this regulation is national, extending across the Commonwealth of Australia, and it does not currently include any exclusions, exemptions, or thresholds beyond those specified. Subordinate instruments may further define or refine the application of these directives.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39, Section 105, outlines the Airworthiness Directives (AD) issued by the Civil Aviation Safety Authority (CASA) for the Bell Helicopter Textron 205 Series Helicopters. Section AD/BELL 205/36 mandates an inspection of the fuel boost pumps on all model 205A-1 helicopters with serial numbers (S/Nos.) prior to 30233. This directive is applicable as of 11/76 and requires compliance within 100 hours of time in service after 30 November 1976. The directive references Bell Service Bulletin No. 205-76-14 as the document detailing the necessary inspection procedures. Under the Civil Aviation Regulations 1998, the primary obligation for operators of the specified Bell Helicopter Textron 205 Series helicopters is to conduct a thorough inspection of the fuel boost pumps as mandated by AD/BELL 205/36. This inspection must be performed within 100 hours of time in service after the specified date of 30 November 1976, to ensure that the aircraft remains airworthy. Operators must follow the detailed procedures outlined in Bell Service Bulletin No. 205-76-14 to carry out the inspection, ensuring that any issues are identified and rectified in a timely manner. Failure to comply with the requirements set forth in AD/BELL 205/36 can result in serious consequences. The regulations impose both civil and criminal penalties for non-compliance. Under Section 91 of the Civil Aviation Act 1988, any person who fails to comply with an Airworthiness Directive can be subject to a civil penalty of up to $21,000 for each flight in contravention. Additionally, under Section 97 of the same Act, non-compliance may also be subject to criminal prosecution, which could result in fines of up to $210,000 and/or imprisonment for up to two years for individuals, and up to $1,050,000 for bodies corporate. These stringent penalties underscore the importance of adhering to the AD and ensuring the ongoing airworthiness of the aircraft.