AD/SF340/95 - Windshield Wiper Arm - 2

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Safety 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 CASR 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.


 

SAAB SF340 Series Aeroplanes

 

AD/SF340/95 Windshield Wiper Arm - 2 13/2003

 

Applicability: Model SF340A aircraft, serial numbers 004 through 159.

 

Model 340B aircraft, serial numbers 160 through 459.

 

Requirement: Action in accordance with SAAB Service Bulletin 340-30-088.

 

Note: LFV AD 1-193 refers.

 

Compliance: Before 30 June 2004.

 

This Airworthiness Directive becomes effective on 25 December 2003.

 

Background: An incident of windshield wiper blade separation has occurred.


David Villiers

Delegate of the Civil Aviation Safety Authority 12 November 2003

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

The above AD is notified in the Commonwealth of Australia Gazette on 3 December 2003.

 


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Overview

The Civil Aviation Safety Regulations 1998 (CASR) were enacted by the Australian Parliament to ensure the safety and efficiency of civil aviation in Australia. These regulations are administered by the Civil Aviation Safety Authority (CASA), which is tasked with ensuring compliance with the regulations through the issuance of various directives. One such directive, AD/SF340/95, was introduced on 25 December 2003 to address an unsafe condition identified in the SAAB SF340 series aeroplanes, specifically regarding the separation of windshield wiper blades. The directive applies to Model SF340A aircraft with serial numbers 004 through 159, and Model 340B aircraft with serial numbers 160 through 459. The policy objective behind this AD is to mandate corrective action as specified in SAAB Service Bulletin 340-30-088, ensuring that the identified unsafe condition is rectified before 30 June 2004 to maintain the airworthiness of the aircraft.

Scope and Application

The Airworthiness Directive (AD) issued under the Civil Aviation Safety Regulations 1998 applies specifically to Saab SF340 Series aeroplanes, encompassing model SF340A aircraft with serial numbers ranging from 004 to 159 and model 340B aircraft with serial numbers from 160 to 459. This AD mandates compliance with the instructions detailed in SAAB Service Bulletin 340-30-088 to address a specific unsafe condition identified with the windshield wiper arm. The requirement to take action is imperative for ensuring the continued airworthiness of these aircraft, and must be completed before 30 June 2004. This directive applies on a national level, as it is issued by the Civil Aviation Safety Authority, a Commonwealth authority, and aims to maintain safety standards within Australia’s civil aviation sector. The directive does not explicitly mention any exclusions or exemptions, implying that all specified aircraft must comply with the outlined requirements.

Key Provisions

The Airworthiness Directive (AD) issued under subregulation 39.1 (1) of the Civil Aviation Safety Regulations 1998 (CASR) applies to specific models of Saab SF340 aircraft. Specifically, it concerns Model SF340A aircraft with serial numbers ranging from 004 to 159 and Model 340B aircraft with serial numbers ranging from 160 to 459. The directive was issued to address an incident involving the separation of a windshield wiper blade, as detailed in the background section (section 1). The AD mandates that the action outlined in the requirement section must be implemented, which involves following the instructions provided in Saab Service Bulletin 340-30-088 (section 2). This action must be taken by the specified compliance date, which is before 30 June 2004 (section 3). The AD imposes certain obligations on the parties or entities governed by it. Aircraft operators and owners must ensure that the specified action, as detailed in the requirement section, is carried out on their Saab SF340 aircraft within the stipulated timeframe (section 2). This involves adhering to the instructions provided in Saab Service Bulletin 340-30-088, which likely includes detailed steps for inspecting, repairing, or replacing the windshield wiper arm to prevent further separation incidents. The directive also requires that the action be completed before the compliance date of 30 June 2004, ensuring that the safety measures are implemented promptly. The AD does not explicitly state any offences, penalties, or civil/criminal consequences for non-compliance. However, failure to adhere to ADs can lead to serious safety issues and may result in enforcement actions by the Civil Aviation Safety Authority (CASA). Potential consequences could include grounding of the aircraft until the required actions are taken, fines, and other regulatory penalties. While the specific penalties are not detailed in this AD, CASA has the authority to take action under the Civil Aviation Act 1988 and related regulations to ensure compliance with airworthiness directives.

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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.