AD/DAUPHIN/52 - Main Rotor Blade Life Limits

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Legislation au F2006B08764 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

 



Eurocopter SA 360 and SA 365 (Dauphin) Series Helicopters

 

AIRWORTHINESS DIRECTIVE


For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.

 

AD/DAUPHIN/52 Main Rotor Blade Life Limits 9/2000

Applicability: SA 365 models C, C1, C2 and C3. Requirement:  Remove from service main rotor blades:

  1. P/N 365A 11.0010.03 before attaining 10 000 hours time in service; and

 

b.    P/N 365A 11.0020.02 and .03 before attaining 12 000 hours time in service.

 

Note: DGAC AD 2000-235-045(A) refers.

 

Compliance: From the effective date of this directive.

 

This Airworthiness Directive becomes effective on 7 September 2000.

 

Background: This directive is to limit the life of certain main rotor blades.


 

David Alan Villiers

Delegate of the Civil Aviation Safety Authority 20 July 2000

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 


The above AD is notified in the Commonwealth of Australia Gazette on 9 August 2000.

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth Parliament, are designed to ensure the safety of civil aviation within Australia. As part of these regulations, the Civil Aviation Safety Authority (CASA) is empowered to issue Airworthiness Directives to address specific safety concerns. One such directive, AD/DAUPHIN/52, was introduced on 7 September 2000 to mitigate the risk associated with the operational lifespan of certain main rotor blades on SA 365 models C, C1, C2, and C3. This directive mandates the removal from service of specific main rotor blades before they reach certain time-in-service thresholds, aiming to prevent potential failures and ensure the continued safety of these aircraft. The directive aligns with international standards, referencing the French Directorate General for Civil Aviation's directive AD 2000-235-045(A), and became effective upon its notification in the Commonwealth of Australia Gazette on 9 August 2000.

Scope and Application

The Airworthiness Directive issued under the Civil Aviation Regulations 1998 applies specifically to SA 365 models C, C1, C2, and C3 helicopters, which are part of the Eurocopter SA 360 and SA 365 (Dauphin) series. The directive mandates that certain main rotor blades must be removed from service before reaching specific time-in-service thresholds to ensure the continued airworthiness and safety of the aircraft. The requirement necessitates the removal of P/N 365A 11.0010.03 blades before they accumulate 10,000 hours of service and P/N 365A 11.0020.02 and .03 blades before they reach 12,000 hours of service. The directive became effective on 7 September 2000 and was published in the Commonwealth of Australia Gazette on 9 August 2000, indicating its binding nature across the national jurisdiction. This directive is a critical measure taken by the Civil Aviation Safety Authority to mitigate identified risks associated with the specified main rotor blades.

Key Provisions

The Civil Aviation Regulations 1998, specifically PART 39 - 105, address the issuance of Airworthiness Directives (ADs) which are critical in maintaining safety standards within the aviation sector. In this case, the directive in question, AD/DAUPHIN/52, applies to Eurocopter SA 360 and SA 365 (Dauphin) Series Helicopters. Section 39.1 (1) empowers the Civil Aviation Safety Authority (CASA) delegate to issue such directives when necessary to ensure airworthiness. The directive mandates specific actions to be taken concerning the main rotor blades of certain Dauphin models to prevent unsafe conditions (AD/DAUPHIN/52, applicability and requirement sections). Operators of SA 365 models C, C1, C2, and C3 are required to remove specific main rotor blades from service before they reach certain time-in-service thresholds. The blades P/N 365A 11.0010.03 must be removed before reaching 10,000 hours of service, and blades P/N 365A 11.0020.02 and.03 must be removed before reaching 12,000 hours. This requirement is intended to address identified issues with blade life and performance, ensuring that these components do not pose a risk to flight safety (AD/DAUPHIN/52, requirement section). The directive is complemented by a reference to DGAC AD 2000-235-045(A), which provides additional context and regulatory alignment. The obligations imposed by this AD are clear and direct. Operators must adhere to the specified removal timelines and ensure that the affected rotor blades are inspected and replaced as required. This involves maintaining detailed records of the service hours for each blade and scheduling necessary maintenance actions promptly to comply with the directive. Failure to comply could result in serious safety risks, and thus, it is imperative that operators implement the directive in a timely and effective manner (AD/DAUPHIN/52, compliance section). Failure to comply with the Airworthiness Directive can lead to significant legal and safety consequences. Under the Civil Aviation Act 1988, non-compliance with ADs can result in civil penalties, including fines, and criminal charges for operators who fail to adhere to safety directives. The maximum penalties for contravening these regulations can be substantial, reflecting the critical nature of airworthiness compliance. Operators must therefore take the directive seriously and ensure that all mandated actions are completed within the specified timeframes to avoid any adverse legal or safety repercussions.

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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.