AD/AMD 10/23 - Fire Extinguishing System Non-Return Valves

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


AIRWORTHINESS DIRECTIVE


For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

 

AMD Falcon 10 Series Aeroplanes

 

AD/AMD 10/23 Fire Extinguishing System Non-Return Valves


8/2001

TX

 

Applicability: Dassault Falcon 10 series aircraft.

 

Requirement: Inspect the engine fire extinguishing system non-return valves in accordance with Dassault Aviation Service Bulletin F10-A291. Replace any non-return valves found to be defective.

 

Note: DGAC Telex AD T2001-219-025(B) refers.

 

Compliance: Before further flight after the effective date of this Airworthiness Directive.

 

This Airworthiness Directive becomes effective on 15 June 2001.

 

Background:  This Airworthiness Directive is prompted by advice that, during engine fire bottle replacement, the fire extinguishing system non-return valves were found to be defective. In the event of an engine fire, the fire extinguishing agent would remain trapped in the system pipes and the fire would not be controlled.


 

Eugene Paul Holzapfel

Delegate of the Civil Aviation Safety Authority 13 June 2001

 

 

 

 

 

 

 

 

 

 

 

 


The above AD is notified in the Commonwealth of Australia Gazette on .15 June 2001.

 

 


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Overview

The Civil Aviation Regulations 1998 (CAR 1998) were enacted to ensure the safety of civil aviation in Australia, providing the framework for the regulation of aircraft and related activities. The 1998 Regulations were a consolidation of previous legislation and amendments, aiming to streamline and modernise the regulatory environment for aviation safety. Among the various parts of these regulations, Part 39 specifically addresses airworthiness, with Section 105 detailing the process for issuing Airworthiness Directives (ADs). The Civil Aviation Safety Authority (CASA), as the delegate of the Commonwealth Government, issues these directives to address safety issues and ensure compliance with safety standards. The policy objective is to maintain the highest level of safety in civil aviation by mandating specific actions to correct identified unsafe conditions. One such Airworthiness Directive, AD/AMD 10/23, issued under the authority of CASA, pertains to the inspection and replacement of non-return valves in the engine fire extinguishing systems of Dassault Falcon 10 series aircraft. This directive was introduced following reports of defective non-return valves that could trap fire extinguishing agents in the system pipes, thereby failing to control engine fires effectively. The directive mandates that these valves be inspected and replaced if defective, in accordance with specific service bulletins, before further flights after its effective date of 15 June 2001. This measure ensures that the safety of aircraft operations is maintained by addressing a specific identified risk.

Scope and Application

This Airworthiness Directive (AD) issued under the Civil Aviation Regulations 1998 applies specifically to Dassault Falcon 10 series aircraft. It mandates the inspection and replacement of engine fire extinguishing system non-return valves to address a safety concern where such valves have been found to be defective during engine fire bottle replacement. This defect could lead to the fire extinguishing agent being trapped in the system pipes, thereby preventing effective control of an engine fire. The directive requires compliance by ensuring the specified inspections and replacements are carried out in accordance with Dassault Aviation Service Bulletin F10-A291 before any further flight after the directive’s effective date of 15 June 2001. This AD is issued by the Civil Aviation Safety Authority (CASA) delegate, and its application extends to all Dassault Falcon 10 series aircraft operating within the Commonwealth of Australia. No specific exclusions, exemptions, or thresholds are mentioned in this directive, meaning it applies broadly to all relevant aircraft without exception.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 - 105, mandate the creation and enforcement of Airworthiness Directives (ADs) to ensure the safety of aircraft. Section 39.1(1) provides the authority for the Civil Aviation Safety Authority (CASA) delegate to issue these directives when an unsafe condition is identified. In this case, AD/AMD 10/23 pertains specifically to the Dassault Falcon 10 series aeroplanes and mandates inspections and repairs of the engine fire extinguishing system non-return valves. This AD, signed by the CASA delegate on 13 June 2001, aims to address a defect that could potentially lead to engine fires not being controlled effectively. The AD requires the inspection and replacement of non-return valves in the engine fire extinguishing system of Dassault Falcon 10 series aircraft in accordance with Dassault Aviation Service Bulletin F10-A291. The directive stipulates that these actions must be carried out before the aircraft can be flown further after the effective date of the AD, which is 15 June 2001. The directive references DGAC Telex AD T2001-219-025(B), indicating that this requirement is part of a broader communication and enforcement effort. Operators and owners of Dassault Falcon 10 series aircraft are obligated to comply with this AD to ensure the airworthiness and safety of their aircraft. This includes conducting the specified inspections and making necessary repairs to the non-return valves to prevent the fire extinguishing agent from becoming trapped in the system pipes, which could otherwise result in uncontrolled engine fires. Failure to comply with these requirements could lead to serious safety issues and potential regulatory consequences. Non-compliance with the AD may result in the aircraft being grounded until the required inspections and repairs are completed. Additionally, there may be civil and criminal penalties for failure to adhere to ADs. The specific consequences and penalties are detailed in the Civil Aviation Act 1988 and the Civil Aviation Regulations 1998, which could include fines and imprisonment for serious breaches. The exact penalties are not specified in the AD itself but are governed by the broader regulatory framework.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.