AD/BELL 205/9 - Servo Cylinder Upper Control Tube Fittings

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

Legislation au F2006B04411 Not 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

 

Bell Helicopter Textron 205 Series Helicopters

 

AD/BELL 205/9 Servo Cylinder Upper Control Tube Fittings 5/71

Applicability: All 205A/A1 models. Document:  Bell SL 205A-69.

Compliance: Within 100 hours time in service after 31 May 1971.

Overview

The Civil Aviation Regulations 1998, enacted by the Australian Parliament, serve as a comprehensive regulatory framework governing all aspects of civil aviation within Australia. Within this extensive regulatory structure, Part 39 - 105, specifically addressing the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, plays a crucial role in ensuring the ongoing airworthiness of aircraft. This particular legislation, AD/BELL 205/9, was introduced to address issues related to the servo cylinder upper control tube fittings in Bell Helicopter Textron 205 Series Helicopters. The policy objective is to mandate compliance within 100 hours of time in service after 31 May 1971, ensuring that all 205A/A1 models adhere to the specifications outlined in Bell SL 205A-69 to maintain operational safety standards.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, which pertains to Airworthiness Directives, applies to all Bell Helicopter Textron 205 Series Helicopters, including the 205A/A1 models, and mandates compliance with the requirements outlined in the directive AD/BELL 205/9 concerning the servo cylinder upper control tube fittings. This legislation is applicable to aircraft operators, maintenance personnel, and any other entities involved in the operation or maintenance of the specified helicopter models. The directive is enforced by the Civil Aviation Safety Authority (CASA) and extends its reach nationally, affecting all operations within the Commonwealth of Australia. The directive requires compliance within 100 hours of time in service after 31 May 1971, ensuring that all affected aircraft meet the specified airworthiness standards. The application of this directive is mandatory and is not subject to exclusions or exemptions, ensuring consistent safety standards across the industry. The enforcement and interpretation of this directive can be further defined through subordinate instruments issued by CASA.

Key Provisions

The Civil Aviation Regulations 1998, under PART 39 - 105, establish specific requirements for the airworthiness directives related to certain aircraft, including Bell Helicopter Textron 205 Series Helicopters. Section AD/BELL 205/9 focuses on the servo cylinder upper control tube fittings, as outlined in document Bell SL 205A-69, applicable to all 205A/A1 models. This directive is crucial for ensuring the safety and compliance of these aircraft in Australian airspace. The main operative sections of this directive require that the specified modifications to the servo cylinder upper control tube fittings be implemented within 100 hours of time in service following the directive's effective date of 31 May 1971. This timeframe is critical for the compliance of 205A/A1 model helicopters, ensuring that they meet the necessary safety standards set by the Civil Aviation Safety Authority. Compliance with these directives is mandatory, as they are essential for maintaining the operational safety and airworthiness of the aircraft. Operators of 205A/A1 model helicopters must adhere to the requirements set forth in the directive, which include conducting necessary inspections, repairs, or modifications to the servo cylinder upper control tube fittings within the stipulated 100-hour period. This obligation ensures that the helicopters remain airworthy and compliant with safety regulations. Failure to comply with these requirements can result in the aircraft being grounded, as the modifications are integral to preventing potential safety hazards. Failure to comply with the airworthiness directive AD/BELL 205/9 may result in serious civil or criminal consequences. The Civil Aviation Regulations 1998 impose penalties for non-compliance, which can include fines and other legal actions. The maximum penalties for breaches of these regulations are significant, reflecting the importance of adhering to safety standards in civil aviation. It is imperative for operators to ensure timely compliance to avoid these penalties and to maintain the safety and airworthiness of their aircraft.

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Area of Law
Aviation Law
Instrument
Regulation
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Definitions & Interpretation
Regulatory Standards
Compliance Obligations

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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.