COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Eurocopter BO 105 Series Helicopters
AD/BO 105/6 Fuel Filter Drain Valve 9/86 DM
Applicability: All model BO 105 helicopters fitted with engine fuel filter drain valve P/No P101- 228.
Requirement: Action in accordance with MBB Alert Service Bulletin ASB BO 105-60-101.
Note: German AD 86-148 MBB Refers.
Compliance: Corrective action 1 of Requirement Document:
Before further flight after 22 August 1986. Corrective action 2 of Requirement Document:
At each daily inspection after 22 August 1986.
Corrective action 3 of Requirement Document:
This action may be carried out before further flight after 22 August 1986 in which case corrective actions 1 and 2 need not be complied with.
Note: Corrective action in accordance with action 3 is an interim measure until manufacturer can supply improved drain valves.
Background: Draining the fuel filters at preflight checks may loosen the handle of the shutoff plunger and under adverse conditions may cause the drain valve to disintegrate.
Overview
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, addresses safety directives concerning airworthiness, particularly focusing on the Eurocopter BO 105 Series Helicopters. This legislation was enacted to ensure the safety and reliability of aircraft in operation, addressing issues such as the risk of fuel filter drain valve disintegration that could potentially compromise flight safety. The Civil Aviation Safety Authority (CASA) oversees these regulations, aiming to mandate corrective actions that align with international safety standards and manufacturer directives. By implementing these airworthiness directives, CASA seeks to prevent mechanical failures and ensure the continued safe operation of aircraft within Australian airspace.
The legislation requires specific actions regarding the fuel filter drain valve on BO 105 helicopters, mandating that corrective measures be taken in accordance with MBB Alert Service Bulletin ASB BO 105-60-101. The primary objective is to mitigate the risk of valve disintegration by ensuring that the drain valves are either properly secured or replaced with improved versions. This directive ensures that all affected helicopters adhere to stringent safety protocols, thereby safeguarding against potential mechanical failures that could endanger flight operations.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandate airworthiness directives for various aircraft types, including the Eurocopter BO 105 Series Helicopters. This particular directive, AD/BO 105/6, targets all BO 105 helicopters equipped with engine fuel filter drain valve P/No P101-228. The directive was issued in response to a potential safety issue identified by the manufacturer, MBB, which noted that draining the fuel filters during preflight checks could lead to the handle of the shutoff plunger loosening, potentially causing the drain valve to disintegrate under adverse conditions. The regulation requires compliance with MBB Alert Service Bulletin ASB BO 105-60-101, which provides specific corrective actions to mitigate the identified risk. These actions must be completed before further flight after 22 August 1986 and at each daily inspection thereafter, with an interim measure allowing for a different corrective action if improved drain valves are not yet available. This directive applies nationally within the Commonwealth of Australia, under the jurisdiction of the Civil Aviation Safety Authority, and does not specify any exclusions or exemptions. The regulatory framework may be further elaborated or modified through subordinate instruments as necessary.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, impose requirements and obligations on the operation of certain aircraft, including the Eurocopter BO 105 series helicopters. The section in question, AD/BO 105/6, pertains to the fuel filter drain valve, P/No P101-228, and outlines mandatory actions to ensure safety and compliance. According to the legislation, all model BO 105 helicopters fitted with the specified fuel filter drain valve must adhere to the requirements set forth in MBB Alert Service Bulletin ASB BO 105-60-101. This directive references German AD 86-148 MBB, indicating that the measures are based on international safety standards.
The key provisions of this directive require corrective actions to be implemented before further flights after 22 August 1986. Specifically, corrective action 1 must be completed before the first flight following the date mentioned, while corrective actions 2 and 3 must be undertaken at each daily inspection thereafter. Corrective action 1 involves taking steps to ensure the integrity of the fuel filter drain valve, while corrective action 2 mandates regular inspections. Corrective action 3 provides an interim measure allowing for the replacement of the drain valve before further flight, which can be done instead of actions 1 and 2. However, corrective action 3 is only applicable until the manufacturer supplies improved drain valves.
Failure to comply with the requirements set out in the Civil Aviation Regulations 1998 can result in significant legal and safety consequences. Non-compliance with the airworthiness directives could lead to the aircraft being deemed unfit for flight, which in turn could result in serious safety risks. Additionally, operators and owners of non-compliant aircraft may face civil penalties, including fines and potential prosecution under the Civil Aviation Act 1988. The exact penalties for non-compliance can vary but may include substantial financial penalties and, in severe cases, criminal charges. It is imperative for all parties governed by these regulations to adhere to the outlined requirements to maintain the safety and airworthiness of the aircraft.