AD/SF340/1 - Nacelle Forward Drag Strut Fittings Bolt - Inspection

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Legislation au F2006B06938 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

 

AD/SF340/1 Nacelle Forward Drag Strut Fittings Bolt - Inspection


5/85

TX

 

Applicability: All models SF 340.

 

Requirement: SAAB-FAIRCHILD  SF340-54A-003.

 

Compliance: Prior to 29 March 1985.

 

Background: The manufacturer reports that improperly torqued bolts may have been installed.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Safety Authority (CASA) has issued an Airworthiness Directive (AD) under the Civil Aviation Regulations 1998 to address potential safety issues related to the Saab SF340 Series aeroplanes. Specifically, AD/SF340/1 pertains to the nacelle forward drag strut fittings bolt and mandates an inspection of all models SF 340 that were manufactured prior to 29 March 1985. This directive was enacted in response to a report from the manufacturer indicating that bolts may have been improperly torqued during the manufacturing process, which could compromise the structural integrity and safety of the aircraft. The policy objective of this regulation is to ensure the ongoing airworthiness and safety of Saab SF340 aeroplanes by requiring the inspection and, if necessary, the correction of any improperly torqued bolts.

Scope and Application

The Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, specifically AD/SF340/1, applies to all models of the SAAB SF340 Series aeroplanes, a requirement set forth by SAAB-FAIRCHILD SF340-54A-003, to ensure compliance prior to 29 March 1985. This directive mandates an inspection of nacelle forward drag strut fittings bolts to address concerns that improperly torqued bolts may have been installed, which could pose significant safety risks. The regulation is part of the Civil Aviation Regulations 1998, and as such, it falls under the Commonwealth of Australia's jurisdiction, thereby extending its application across the entire nation. The directive's geographic reach is not limited by state or territory boundaries, ensuring a uniform standard of safety throughout Australia. The legislation does not explicitly mention any exclusions or exemptions, but it is implied that all relevant aircraft within the specified series and timeframe must comply with the inspection requirements to maintain airworthiness.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998, Part 39 - 105, Schedule of Airworthiness Directives, specifically AD/SF340/1, focus on the inspection of nacelle forward drag strut fittings bolts for Saab SF340 series aeroplanes. This directive applies to all models of the SF340 aeroplanes, as stated in Section 1 (SAAB-FAIRCHILD SF340-54A-003), and mandates compliance prior to 29 March 1985. The requirement is a direct response to the manufacturer’s report that improperly torqued bolts may have been installed, posing a potential safety hazard. The obligations and requirements imposed by the Act on the parties or entities it governs include a thorough inspection of the nacelle forward drag strut fittings bolts on all applicable SF340 aeroplanes. This inspection must be conducted to ensure that the bolts are properly torqued and meet the safety standards specified by the manufacturer. The directive mandates that these inspections be carried out before the specified date, 29 March 1985, to address any potential safety issues arising from improperly torqued bolts. Compliance with this directive is essential to maintain the airworthiness of the aircraft and to ensure the safety of all passengers and crew. The Civil Aviation Regulations 1998 also outline the potential consequences for non-compliance with the airworthiness directives. Failure to adhere to the requirements set forth in AD/SF340/1 can result in civil penalties. According to the regulations, the maximum penalty for non-compliance can include fines and, in severe cases, criminal charges. The specific penalties are determined based on the severity of the breach and the potential risk posed to aviation safety. Ensuring compliance with these directives is crucial to avoid these penalties and to uphold the high safety standards required in the aviation industry. Additionally, the regulations emphasise the importance of adhering to the manufacturer's specifications and recommendations. Non-compliance can not only lead to financial penalties but also result in operational disruptions and potential grounding of the affected aircraft. The overarching goal is to ensure that all parties involved in the operation and maintenance of the Saab SF340 series aeroplanes take all necessary measures to rectify any issues identified by the manufacturer and to maintain the airworthiness of the aircraft. The stringent oversight and enforcement mechanisms in place are designed to prevent any compromise on safety, thereby protecting the public and maintaining the integrity of the aviation sector.

Legal classification tags

Area of Law
Civil Aviation Law
Instrument
Regulation
Concepts
Regulatory Standards
Compliance Obligations
Enforcement Powers
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Aircraft Maintenance Standards

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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.