AD/SWSA226/11 - Rudder - Inspection

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B07158 Not in force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Fairchild (Swearingen) SA226 and SA227 Series Aeroplanes

 

AD/SWSA226/11 Rudder - Inspection 9/73

Applicability: All model SA226T with S/Nos. T-201 to T-237. Document:  Swearingen SB 27-20-3032.

Compliance: As per the requirement document.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, serve to regulate various aspects of civil aviation within Australia. Within this comprehensive framework, Part 39, specifically addressing the safety of civil aircraft, contains the Airworthiness Directives (AD) aimed at ensuring that aircraft meet the necessary safety standards. AD/SWSA226/11 is one such directive, targeting the Fairchild (Swearingen) SA226 and SA227 series aeroplanes, focusing on rudder inspection for specified models. This directive was introduced to address identified safety issues related to the structural integrity of the rudders on these aircraft models, thereby ensuring ongoing airworthiness and safety compliance. The policy objective behind these regulations is to maintain the highest standards of safety in Australian civil aviation, protecting both passengers and crew. The Civil Aviation Safety Authority (CASA) administers these regulations, issuing specific directives to address safety concerns as they arise. The directive for the Fairchild (Swearingen) SA226 and SA227 series aeroplanes is a response to particular safety issues identified with the rudders of these aircraft models. By mandating inspections according to the requirements outlined in the Swearingen SB 27-20-3032 document, CASA aims to prevent potential safety hazards, thereby reinforcing the overarching goal of the Civil Aviation Regulations 1998 to safeguard the public and maintain the integrity of the civil aviation system in Australia.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, apply to the Fairchild (Swearingen) SA226 and SA227 series aeroplanes, with a focus on Airworthiness Directives concerning these aircraft models. AD/SWSA226/11 mandates that all model SA226T aircraft with serial numbers ranging from T-201 to T-237 must undergo inspections of the rudder as per the specified requirement document, Swearingen SB 27-20-3032. Compliance with these regulations is essential for maintaining airworthiness and ensuring safety standards are met across the Commonwealth of Australia. The geographic reach of these regulations is national, applying uniformly across all states and territories within Australia. The regulations do not explicitly mention any exclusions or exemptions, implying that all specified aircraft must adhere to the stipulated directives without exception. Subordinate instruments may further detail specific compliance requirements and operational guidelines, but these are not outlined in the provided text.

Key Provisions

The Civil Aviation Regulations 1998, particularly in Part 39, contain significant provisions concerning the airworthiness of aircraft. Section 39-105, which pertains to the schedule of airworthiness directives, is a crucial part of this legislation. This section mandates specific inspections and maintenance actions for particular types of aircraft to ensure safety and compliance with aviation standards. For instance, AD/SWSA226/11, which applies to Fairchild (Swearingen) SA226 and SA227 series aeroplanes, specifically addresses the inspection of the rudder (section 9/73). This directive applies to all model SA226T with serial numbers ranging from T-201 to T-237 and requires adherence to the specifications outlined in document Swearingen SB 27-20-3032. Under the Civil Aviation Regulations 1998, the obligations imposed on the parties governed by these provisions are clear and stringent. Operators of the specified aircraft models must ensure that the rudder inspections are conducted as per the detailed requirements in the referenced document. This includes verifying the structural integrity, functionality, and any necessary repairs or replacements. Compliance with these directives is mandatory, and failure to adhere to the prescribed procedures could result in significant safety risks and regulatory penalties. The Civil Aviation Regulations 1998 also outline the potential consequences for non-compliance with the airworthiness directives. Breaches of these provisions can lead to both civil and criminal penalties. Civil penalties may include fines and the potential grounding of the aircraft until compliance is achieved. Furthermore, there are serious criminal implications for individuals or companies that deliberately or negligently fail to meet these safety standards. The maximum penalties can be severe, reflecting the critical importance of adhering to these regulations to maintain the safety of civil aviation. This underscores the necessity for operators to meticulously follow the specified inspection and maintenance procedures to avoid any legal repercussions.

Legal classification tags

Area of Law
Aviation Law
Instrument
Legislative Instrument
Concepts
Definitions & Interpretation
Compliance Obligations
Enforcement Powers
Catchwords
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.