AD/BEA 121/10 - Rudder Drain Hole

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

Legislation au F2006B03574 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

 


Beagle B121 (Pup) Series Aeroplanes

 

AD/BEA 121/10 Rudder Drain Hole 4/72

Applicability: All models.

 

Requirement: Provide a suitable drain hole in the lower rudder area to ensure satisfactory drainage of moisture from within the rudder.

 

Compliance: Within 100 hours time in service after 28 April 1972.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, aim to regulate and maintain safety standards in civil aviation. Within this legislative framework, the specific amendment F2006B03574 addresses a technical requirement for Beagle B121 (Pup) Series Aeroplanes, particularly concerning the installation of a rudder drain hole to ensure the satisfactory drainage of moisture from within the rudder. This was introduced to address a potential safety issue related to moisture accumulation that could affect the aircraft's control surfaces. The policy objective behind this safety directive is to enhance the operational safety and reliability of the specified aircraft models by preventing moisture-related malfunctions. Compliance with this directive is mandatory within 100 hours of time in service after the directive's effective date of 28 April 1972, ensuring that all applicable models are equipped with the necessary modifications to meet the safety standards set by the Civil Aviation Safety Authority.

Scope and Application

The Civil Aviation Regulations 1998, specifically PART 39 - 105, which pertains to the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, applies to all models of the Beagle B121 (Pup) series aeroplanes, mandating the installation of a suitable drain hole in the lower rudder area to ensure satisfactory drainage of moisture from within the rudder. This requirement must be met within 100 hours of time in service after 28 April 1972. The directive applies nationwide, affecting all operators of Beagle B121 (Pup) aeroplanes within Australia. The regulations extend to ensuring compliance with safety standards to maintain airworthiness, with no stated exclusions or exemptions in this directive. Any non-compliance could potentially result in aircraft being grounded, thus emphasising the critical nature of adherence to these safety mandates.

Key Provisions

The Civil Aviation Regulations 1998, specifically in Part 39 - 105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, include detailed provisions for maintaining the airworthiness of various aircraft. In relation to Beagle B121 (Pup) Series Aeroplanes, AD/BEA 121/10 addresses the requirement for a rudder drain hole (section 4/72). This directive applies to all models of the Beagle B121 (Pup) Series and mandates the installation of a suitable drain hole in the lower rudder area. The primary purpose of this requirement is to ensure that moisture can be effectively drained from within the rudder, thereby maintaining the aircraft's structural integrity and operational safety. The obligations under this directive are clear and specific. Operators of Beagle B121 (Pup) Series Aeroplanes must ensure that the designated rudder drain hole is installed within 100 hours of time in service following the effective date of the directive, which is 28 April 1972. This involves conducting a thorough inspection of the rudder and, if necessary, retrofitting the rudder with the appropriate drain hole. Operators must also maintain records of compliance, which may be required for verification during routine inspections by the Civil Aviation Safety Authority. Failure to comply with this directive could result in the aircraft being deemed unairworthy, leading to potential grounding and further regulatory action. Non-compliance with AD/BEA 121/10 can result in significant legal and operational consequences. Under the Civil Aviation Act 1988, failure to adhere to an airworthiness directive can be considered an offence. Specifically, section 30 of the Act states that a person who contravenes any airworthiness requirement, including those set out in the Civil Aviation Regulations, is liable to penalties. The maximum penalties for such offences include substantial fines and, in severe cases, imprisonment. Additionally, operators may face civil penalties imposed by the Civil Aviation Safety Authority, which can include financial penalties and operational restrictions. These consequences underscore the importance of strict adherence to airworthiness directives to ensure the safety and reliability of civil aviation operations.

Legal classification tags

Area of Law
Aviation Law
Instrument
Regulation
Concepts
Definitions & Interpretation
Compliance Obligations
Enforcement Powers
Catchwords
Airworthiness

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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.