AD/SF340/74 - Cargo Compartment Fire Detectors

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Legislation au F2006B07004 In force Legislative Instrument

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 



SAAB SF340 Series Aeroplanes

 

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 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.

 

AD/SF340/74 Cargo Compartment Fire Detectors 3/2000

Applicability: Model SF340A aeroplanes, serial number (S/N) 004 through 159 and Model 340B aeroplanes, S/N 160 through 459.

 

Requirement: Replace cargo compartment smoke detectors manufactured by Fenwall with smoke detectors, part number CGAB1201-01, manufactured by Cerberus SA in accordance with SAAB Aircraft AB Mandatory Service Bulletin SAAB 340-26-023 dated

21 December 1999.

 

Note: LFV AD 1-151 refers.

 

Compliance: Before 28 December 2001.

 

This Airworthiness Directive becomes effective on 23 March 2000.

 

Background: The Luftfartsverket, the Swedish Civil Aviation Administration, has advised that field experience has demonstrated that smoke detectors, located in the cargo compartment, manufactured by Fenwall exhibit poor reliability, resulting in false warning occurring during high humidity environmental conditions.

 

This Directive mandates the replacement of the current cargo compartment smoke detectors with new units that have increased reliability and decreased maintenance.


 

Eugene Paul Holzapfel

Delegate of the Civil Aviation Safety Authority 10 February 2000

 

 

 

 

 

 

 

 

 


The above AD is notified in the Commonwealth of Australia Gazette on 23 February 2000.

 

 

 

 

Overview

The Civil Aviation Regulations 1998, under Part 39 - 105 of the Civil Aviation Safety Authority Schedule of Airworthiness Directives, introduces a specific Airworthiness Directive concerning the Saab SF340 Series aeroplanes. Enacted by the Commonwealth of Australia, this legislation was introduced to address the safety concerns identified by the Swedish Civil Aviation Administration regarding the reliability of cargo compartment smoke detectors manufactured by Fenwall. The directive mandates the replacement of these detectors with more reliable units manufactured by Cerberus SA, thereby aiming to rectify the unsafe conditions that could potentially lead to false warnings, particularly under high humidity conditions. The Civil Aviation Safety Authority, through its delegate Eugene Paul Holzapfel, issued this directive to ensure the continued airworthiness and safety of the affected aircraft models, requiring compliance by a specified date to mitigate any potential risks.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39, mandates that certain actions be taken to maintain the airworthiness of specified aircraft models. This particular Airworthiness Directive (AD) applies to Saab SF340 Series aeroplanes, specifically Model SF340A aeroplanes with serial numbers (S/N) ranging from 004 to 159 and Model SF340B aeroplanes with serial numbers from 160 to 459. The AD requires the replacement of cargo compartment smoke detectors originally manufactured by Fenwall with new smoke detectors, part number CGAB1201-01, manufactured by Cerberus SA, following instructions set out in SAAB Aircraft AB Mandatory Service Bulletin SAAB 340-26-023 dated 21 December 1999. The requirement must be met before 28 December 2001, with the directive becoming effective from 23 March 2000. This action is necessary due to the identified poor reliability of the original smoke detectors, particularly in high humidity conditions, which can lead to false warnings. The AD is applicable within the jurisdiction of the Commonwealth of Australia and is overseen by the Civil Aviation Safety Authority.

Key Provisions

The Civil Aviation Regulations 1998, particularly Part 39 - 105, establish a comprehensive framework for ensuring the airworthiness of aircraft in Australia. Section 39.1(1) empowers the Civil Aviation Safety Authority (CASA) to issue Airworthiness Directives (ADs) to address identified safety issues. The AD in question, AD/SF340/74, pertains specifically to Saab SF340 series aeroplanes, namely SF340A aeroplanes with serial numbers (S/N) 004 through 159, and SF340B aeroplanes with S/N 160 through 459. The directive mandates the replacement of cargo compartment smoke detectors manufactured by Fenwall with those manufactured by Cerberus SA, part number CGAB1201-01, as outlined in SAAB Aircraft AB Mandatory Service Bulletin SAAB 340-26-023 dated 21 December 1999. This replacement is necessary to mitigate the risk of false warnings due to poor reliability of the original detectors, particularly under high humidity conditions, as reported by the Swedish Civil Aviation Administration. The AD imposes specific obligations on the operators and owners of the affected aircraft. These parties must ensure that the required modifications are carried out before 28 December 2001, as stipulated in the compliance section of the directive. The modifications must be executed in accordance with the instructions provided by SAAB Aircraft AB, and the directive itself becomes effective from 23 March 2000. The directive references LFV AD 1-151, indicating that this requirement is aligned with international standards and recommendations. Compliance with the AD is mandatory, and failure to adhere to these specifications could result in serious safety implications. Failure to comply with the requirements of the AD can lead to significant consequences. The AD explicitly states that the action must be taken before the specified compliance date. Non-compliance may result in the aircraft being deemed unairworthy, which can lead to grounding of the aircraft and potential enforcement actions by CASA. The Civil Aviation Regulations 1998 do not explicitly outline the penalties for non-compliance in this specific context, but generally, failure to adhere to ADs can result in severe penalties, including fines and potential criminal charges. The specific penalties can vary based on the severity of the non-compliance and any resulting safety incidents. Operators and owners are therefore strongly encouraged to ensure strict adherence to the directive to avoid these adverse outcomes.

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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.