AD/A109/10 - Nose Landing Gear Actuator

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Legislation au F2006B01794 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

 


Agusta A109 Series Helicopters

 

AD/A109/10 Nose Landing Gear Actuator 12/87

Applicability: All Model A109A and A109AII Helicopters.

 

Requirement: Action in accordance with Agusta Bollettino Tecnico No. 109-62, Revision A.

 

Note: RAI AD No 87-93/A109-43 refers.

 

Compliance: As per the Requirement Document.

 

Background: Additional maintenance, particularly where operations are conducted in highly humid and saline conditions, is required the nose gear retraction servo to prevent the nose landing gear collapsing during ground operation.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, as part of the legislative framework overseen by the Civil Aviation Safety Authority (CASA), were enacted to ensure the safety of civil aviation in Australia. The regulations are a crucial part of maintaining high standards for aircraft operations, with particular emphasis on the airworthiness of aircraft and the safety of their operations. One such regulation, AD/A109/10 concerning the Agusta A109 Series Helicopters, was introduced to address specific safety concerns identified with the nose landing gear actuator of the A109A and A109AII helicopters. The policy objective behind this regulation is to mitigate the risk of the nose landing gear collapsing during ground operations, particularly in highly humid and saline environments, by mandating additional maintenance procedures in accordance with Agusta Bollettino Tecnico No. 109-62, Revision A. This directive ensures that operators adhere to the specified maintenance actions to uphold the safety and reliability of these helicopters in their operations.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all Model A109A and A109AII Helicopters within the Commonwealth of Australia. This regulation mandates compliance with Agusta Bollettino Tecnico No. 109-62, Revision A, concerning the maintenance of the nose landing gear actuator. The directive requires additional maintenance to prevent the nose landing gear from collapsing during ground operations, especially in highly humid and saline conditions. This safety measure is imperative to ensure the operational integrity and safety of these helicopters. The requirement for compliance is detailed in the relevant Requirement Document, which outlines the specific actions to be taken as per the technical bulletin. Additionally, the regulation references RAI AD No 87-93/A109-43, further detailing the necessary maintenance procedures. The scope of this regulation is confined to the specified helicopter models, and compliance is overseen by the Civil Aviation Safety Authority within the national jurisdiction of Australia.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes an airworthiness directive (AD/A109/10) concerning the nose landing gear actuator of Agusta A109 Series Helicopters. This directive applies to all Model A109A and A109AII helicopters (Regulation 39.105(1)). The key requirement is that these helicopters must be maintained in accordance with Agusta Bollettino Tecnico No. 109-62, Revision A. This directive was referenced in an earlier directive, RAI AD No 87-93/A109-43. The directive mandates compliance with the requirement document, ensuring that the necessary maintenance is carried out to prevent the nose landing gear from collapsing during ground operations, particularly in highly humid and saline environments. The Civil Aviation Regulations impose specific obligations on the parties governed by this directive. Owners and operators of the affected helicopters must ensure that maintenance actions are carried out as specified in Agusta Bollettino Tecnico No. 109-62, Revision A. This includes detailed inspection and maintenance procedures to address the potential failure of the nose landing gear retraction servo in challenging operational conditions. It is imperative that the maintenance is performed by qualified personnel and that records of compliance are maintained in accordance with the requirements set forth in the directive. Failure to comply with this airworthiness directive can result in serious consequences. Under the Civil Aviation Act 1988, non-compliance may lead to enforcement actions by the Civil Aviation Safety Authority (CASA). This can include the grounding of the affected aircraft until the necessary maintenance is performed. In more severe cases, CASA may take legal action against the operator or owner, which could result in substantial fines or other penalties. The exact penalties depend on the severity and circumstances of the non-compliance, but they can be significant, reflecting the importance of maintaining airworthiness standards to ensure safety in aviation operations.

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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.