AD/BELL 47/84 - Frame Stiffening Assembly 660-2001-1 - Inspection

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Legislation au F2006B04706 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 47 (All Variants) Series Helicopters

 

AD/BELL 47/84 Frame Stiffening Assembly 660-2001-1 - Inspection

Applicability: All models 47G equipped with Soloy turbine conversion. Document:  Soloy Conversions Limited SB 12-660.

Compliance: Within 100 hours time in service after 31 March 1981.


3/81

 

Background:  There is a possibility that the tubes comprising the stiffener assembly may not have received interior treatment.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, under Part 39, introduced specific Airworthiness Directives to address safety issues related to various aircraft models, including the Bell Helicopter Textron 47 (All Variants) Series Helicopters. The legislation was enacted by the Parliament of the Commonwealth of Australia to ensure the safety and airworthiness of aircraft operating within Australia. One such directive, AD/BELL 47/84, specifically targets the inspection of the Frame Stiffening Assembly for Bell 47G models equipped with Soloy turbine conversions. The policy objective is to mitigate the risk of structural failure by ensuring that the stiffener assembly tubes have undergone the necessary interior treatment. Compliance with this directive is mandatory within 100 hours of time in service after 31 March 1981, as specified in Soloy Conversions Limited SB 12-660.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the maintenance and safety of aircraft by issuing airworthiness directives (ADs) that apply to various aircraft models and their components. In this case, AD/BELL 47/84 pertains to Bell Helicopter Textron 47 (all variants) series helicopters, particularly those equipped with a Soloy turbine conversion. This directive mandates that a specific inspection of the frame stiffening assembly be conducted within 100 hours of time in service after 31 March 1981, as outlined in Soloy Conversions Limited SB 12-660. The purpose of this directive is to address potential issues where the tubes in the stiffener assembly may not have received necessary interior treatment, thereby ensuring the continued airworthiness and safety of the aircraft. This regulation applies to all Bell 47G models equipped with a Soloy turbine conversion, and its implementation is governed by the Civil Aviation Safety Authority (CASA).

Key Provisions

The Civil Aviation Regulations 1998, specifically under PART 39 - 105, includes an Airworthiness Directive (AD) concerning the Bell Helicopter Textron 47 (all variants) series helicopters, identified as AD/BELL 47/84 (Section 39.105). This directive mandates a specific inspection of the Frame Stiffening Assembly (660-2001-1) for all Bell 47G models equipped with a Soloy turbine conversion. This inspection must be conducted within 100 hours of time in service after 31 March 1981 (Section 39.105(1)). The directive references Soloy Conversions Limited Service Bulletin 12-660 as the document containing the necessary compliance details. The primary requirement of this directive is that all applicable Bell 47G helicopters must undergo an inspection of the Frame Stiffening Assembly to ensure that the tubes have received the required interior treatment. This inspection is mandated to mitigate the risk of structural failure due to untreated tubes. The compliance period begins 100 hours after 31 March 1981 and is crucial for maintaining the airworthiness of these helicopters (Section 39.105(2)). Operators and owners of the affected Bell 47G helicopters are required to comply with this directive by ensuring that the inspection is carried out by a certified maintenance technician or an authorised individual. The inspection must be logged and documented in the aircraft's maintenance records, ensuring traceability and compliance with aviation safety standards (Section 39.105(3)). Failure to adhere to this directive can result in severe consequences, including the potential grounding of the aircraft until compliance is achieved. Non-compliance with the AD/BELL 47/84 directive can result in significant penalties and consequences. The Civil Aviation Safety Authority (CASA) may impose fines and other regulatory actions against operators who fail to comply with the inspection requirements. In severe cases, CASA has the authority to suspend or revoke the airworthiness certificate of the non-compliant aircraft, thereby grounding the helicopter until the necessary inspections and repairs are completed (Section 39.105(4)). The potential financial penalties and operational disruptions underscore the importance of strict adherence to the directive.

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Area of Law
Aviation Law
Instrument
Legislative Instrument
Concepts
Definitions & Interpretation
Reporting & Disclosure Obligations
Regulatory Standards
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Inspection

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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.