AD/BELL 206/124 Amdt 1 - Driveshaft Seal

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

Legislation au F2006B04439 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 Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters

 

AD/BELL 206/124

Amdt 1


Driveshaft Seal  2/93 TX

 

Applicability: All Model 206A, 206BII, 206BIII, 206L-1, 206L-3 and Agusta Bell AB206A and AB206B Helicopters fitted with driveshafts listed in the requirement documents.

 

Requirement: Action in accordance with:

 

  1. Bell machines: Bell Helicopter Alert Service Bulletin 206-91-61 or 206L-91-74 as applicable; and

 

2.    Agusta Bell machines: Agusta Bell Bollettino Tecnico 206-205 dated 20 July 1992.

 

Compliance: As specified in the requirement documents with an effective date of 28 December 1992.

 

Background: Due to possible damage of the seal assembly P/N 206-040-276-101 or 206-040-272- 101, inspection of the driveshaft for grease leakage is required. Grease loss could result in driveshaft failure and loss of rotor drive. This amendment adds Agusta Bell machines to this Directive.

 

Overview

The Civil Aviation Regulations 1998, as amended by the Legislative Instrument F2006B04439, addresses specific safety concerns related to the driveshaft seal on Bell Helicopter Textron Canada (BHTC) 206 and Agusta Bell 206 Series Helicopters. This amendment was enacted to ensure the safety and reliability of helicopters by requiring the inspection of driveshafts to prevent potential failures that could lead to a loss of rotor drive. The Civil Aviation Safety Authority (CASA) is the enacting body, and the policy objective is to enhance aviation safety through stringent maintenance and inspection requirements. The requirement necessitates compliance with specific service bulletins and technical notices issued by Bell and Agusta Bell, ensuring that any damage to the seal assembly is identified and rectified to avoid catastrophic outcomes during flight.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, govern the maintenance and operational standards for certain helicopter models. This particular regulation, AD/BELL 206/124 Amendment 1, applies to all Bell Helicopter Textron Canada (BHTC) 206 series and Agusta Bell 206 series helicopters equipped with specific driveshafts. The regulation mandates compliance with the Bell Helicopter Alert Service Bulletin or the Agusta Bell Bollettino Tecnico, requiring inspections for grease leakage in the specified driveshaft seals. These measures are crucial to prevent potential driveshaft failure, which could lead to the loss of rotor drive and compromise flight safety. The directive applies nationwide within the Commonwealth of Australia and extends its regulatory oversight to both Australian-based and foreign-registered helicopters operating within Australian airspace, ensuring a uniform standard of airworthiness across the board.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, outlines the Civil Aviation Safety Authority's (CASA) schedule of airworthiness directives. In this context, AD/BELL 206/124 Amendment 1 (section 2/93 TX) pertains to the driveshaft seal requirements for certain Bell Helicopter Textron Canada (BHTC) and Agusta Bell 206 Series helicopters. The directive applies to all Model 206A, 206BII, 206BIII, 206L-1, 206L-3, and Agusta Bell AB206A and AB206B helicopters equipped with specific driveshafts detailed in the requirement documents. The primary requirement of this directive is to address potential damage to the seal assembly P/N 206-040-276-101 or 206-040-272-101, which could lead to grease leakage. Such leakage might cause driveshaft failure and subsequent loss of rotor drive, which is a significant safety concern. Operators and owners of the affected helicopters must comply with the directive by performing inspections as specified in the requirement documents. For Bell machines, compliance involves following Bell Helicopter Alert Service Bulletin 206-91-61 or 206L-91-74, as applicable. Agusta Bell machines must adhere to Agusta Bell Bollettino Tecnico 206-205 dated 20 July 1992. The directive became effective on 28 December 1992, necessitating that all required inspections and corrective actions be completed by this date. The Civil Aviation Regulations 1998 impose clear obligations on helicopter operators and owners to ensure their aircraft meet the specified airworthiness standards. These obligations include timely inspections of the driveshaft seals and subsequent repairs or replacements as necessary. Failure to comply with the airworthiness directive could result in the aircraft being deemed unairworthy, potentially leading to grounding of the helicopter until the necessary actions are taken. Furthermore, non-compliance may also attract regulatory scrutiny, audits, and possible enforcement actions by CASA. In terms of penalties and consequences, breaches of the airworthiness directive can result in significant civil and criminal liabilities. Operators and owners found in non-compliance with the directive may face enforcement actions from CASA, including fines, enforcement notices, and even criminal charges if the breach results in a safety incident. The maximum penalties for such offences can vary but may include substantial fines and, in severe cases, imprisonment. It is imperative for operators and owners to adhere strictly to the requirements to avoid these adverse 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.