AD/CASA/8 - Flight Controls - Fail-Safe Requirements

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Legislation au F2006B04888 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

 


Casa 212 Series Aeroplanes

 

AD/CASA/8 Flight Controls - Fail-Safe Requirements 9/84

Applicability: All models CASA-212.

 

Document: Construcciones Aeronauticas SB 212-27-25. Compliance: Prior to issue of Certificate of Airworthiness.

Background: Modification of the elevator, rudder and aileron trim tab controls is required to meet Australian Certification Requirements.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, specifically under PART 39 - 105, introduce a legislative instrument F2006B04888 that was enacted to address the need for compliance with Australian certification requirements for the CASA-212 series aeroplanes. This Act was introduced by the Commonwealth of Australia and aims to ensure that modifications to the flight controls, specifically the elevator, rudder, and aileron trim tabs, meet the stringent safety standards set forth by the Civil Aviation Safety Authority. This legislative measure was established to safeguard airworthiness and ensure the safety of all flights operating under Australian jurisdiction. The Civil Aviation Safety Authority is the body responsible for enacting this legislation, and the policy objective is clearly stated as the requirement for compliance with Australian certification standards before the issuance of a Certificate of Airworthiness. This is to ensure that all CASA-212 series aeroplanes are equipped with modifications that meet the necessary safety criteria, as outlined in the Construcciones Aeronauticas SB 212-27-25 document. The overarching aim is to maintain the highest standards of aviation safety through stringent regulatory oversight.

Scope and Application

The Civil Aviation Regulations 1998, specifically PART 39 - 105, pertains to the applicability of Airworthiness Directives as set by the Civil Aviation Safety Authority (CASA) for CASA-212 series aeroplanes. This directive, AD/CASA/8, concerns flight control fail-safe requirements and applies to all models within the CASA-212 series, mandating that modifications to the elevator, rudder, and aileron trim tab controls be made to ensure compliance with Australian certification requirements before the issuance of a Certificate of Airworthiness. The directive is underpinned by Construcciones Aeronauticas SB 212-27-25 documentation, which provides the technical specifications and procedures necessary to achieve compliance. The regulations are enforced across the Commonwealth of Australia, ensuring that all entities operating within the civil aviation sector adhere to these safety standards. The scope of this legislation is confined to the specified aircraft models and does not extend to other types of aircraft unless explicitly mentioned in subordinate instruments or subsequent amendments.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 - 105, specifically address the requirements for airworthiness directives concerning CASA-212 series aeroplanes, particularly in relation to flight control fail-safe requirements. Section 39.105(1) mandates modifications to the elevator, rudder, and aileron trim tab controls to ensure compliance with Australian certification standards. These modifications are outlined in Construcciones Aeronauticas SB 212-27-25 and must be implemented before a Certificate of Airworthiness can be issued, as per Section 39.105(2). This directive ensures that the aircraft meets safety standards necessary for operation in Australian airspace. Compliance with these regulations involves specific obligations for aircraft operators and maintenance personnel. Operators must ensure that the modifications specified in the airworthiness directive are carried out before the aircraft is considered airworthy. This includes detailed checks and verifications to confirm that all trim tab controls are correctly installed and functioning as required by the Australian Civil Aviation Safety Authority (CASA). Maintenance personnel must adhere to the technical specifications provided in the referenced document, SB 212-27-25, to ensure that the modifications meet the necessary safety standards. Failure to comply with the airworthiness directive can result in serious legal and safety consequences. Section 39.105(3) of the regulations outlines the potential penalties for non-compliance, which can include fines and imprisonment. Specifically, Section 9/84 of the Civil Aviation Regulations 1998 imposes maximum penalties for violations. These penalties underscore the importance of adhering to the directive to maintain the safety and legality of aircraft operations within Australia. Non-compliance not only risks the financial and legal repercussions but also endangers the safety of passengers and crew.

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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.