AD/BELL 412/8 - Installation of Main Rotor Droop Restraint Kit and Cyclic Stick Centring Indicator

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Legislation au F2006B04681 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

 


Bell Helicopter Textron 412 Series Helicopters

 

AD/BELL 412/8 Installation of Main Rotor Droop Restraint

Kit and Cyclic Stick Centring Indicator

Applicability: All models with S/Nos. prior to 33101. Document:  Bell Alert Service Bulletin No. 412-83-11. Compliance:               1 September 1983.


6/83

Background:  These modifications result from BHT investigations of main rotor yoke cracking. They are designed to prevent excessive main rotor yoke loads while the aircraft is parked, and during ground operation.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, represent a comprehensive framework designed to ensure the safety and efficiency of civil aviation within the country. Among these regulations, Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives addresses specific safety requirements for various aircraft models, including the Bell Helicopter Textron 412 Series Helicopters. This particular legislation was introduced to address the problem of main rotor yoke cracking in Bell 412 helicopters, as identified in Bell Alert Service Bulletin No. 412-83-11. The directive mandates the installation of a main rotor droop restraint kit and a cyclic stick centring indicator for all models with serial numbers prior to 33101 to mitigate the risks associated with excessive main rotor yoke loads during parking and ground operations. Compliance with this directive was required by 1 September 1983.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning the Civil Aviation Safety Authority Schedule of Airworthiness Directives, applies to the Bell Helicopter Textron 412 Series Helicopters with serial numbers prior to 33101. The directive mandates the installation of a Main Rotor Droop Restraint Kit and a Cyclic Stick Centring Indicator to address issues identified through Bell Helicopter Textron investigations, specifically concerning main rotor yoke cracking. This legislation ensures that these helicopters comply with safety standards to prevent excessive main rotor yoke loads while the aircraft is parked and during ground operations. The directive is enforceable across the Commonwealth of Australia, impacting all operators of the specified helicopter models. The compliance date is set for 1 September 1983, as referenced in Bell Alert Service Bulletin No. 412-83-11. The application of this directive is comprehensive, covering all relevant aircraft within the specified serial number range without any stated exclusions or exemptions. The enforcement of this directive may be further extended or detailed through subordinate instruments issued by the Civil Aviation Safety Authority.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandate the installation of a Main Rotor Droop Restraint Kit and a Cyclic Stick Centring Indicator for all Bell Helicopter Textron 412 Series Helicopters with serial numbers (S/Nos) prior to 33101 (AD/BELL 412/8). These modifications are intended to address the issues of main rotor yoke cracking by reducing the loads experienced by the yoke when the aircraft is parked or during ground operations. The compliance date for these modifications is set for 1 September 1983, as detailed in Bell Alert Service Bulletin No. 412-83-11. Operators and owners of Bell Helicopter Textron 412 Series Helicopters affected by this Airworthiness Directive are required to ensure that the specified modifications are installed before the compliance date. This involves the installation of the Main Rotor Droop Restraint Kit, which is designed to limit the droop of the main rotor blades, thereby reducing the stress on the yoke. Additionally, the Cyclic Stick Centring Indicator must be installed to provide operators with a visual indication that the cyclic control stick is properly centred, further aiding in the prevention of excessive yoke loads. These requirements are integral to maintaining the airworthiness of the aircraft and ensuring the safety of all personnel involved. Failure to comply with the Airworthiness Directive may result in serious safety issues, potentially leading to catastrophic failure of the main rotor system. The Civil Aviation Safety Authority (CASA) enforces these regulations rigorously, and non-compliance can lead to severe penalties. Civil penalties may include fines, and in the event of an accident resulting from non-compliance, criminal charges could be brought against the responsible parties. The exact penalties for non-compliance are not detailed in the directive but can be substantial, reflecting the gravity of the safety concerns at hand. It is imperative for operators to adhere strictly to the specified requirements to avoid these serious consequences.

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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.