AD/S-PUMA/27 Amdt 1 - Main Rotor Head Blade Horn Eye Bolts

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

Legislation au F2006B07104 In force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 



Eurocopter AS 332 (Super Puma) Series Helicopters

 

AIRWORTHINESS DIRECTIVE


For the reasons set out in the background section, the CASA delegate whose signature appears below revokes Airworthiness Directive (AD) AD/S-PUMA/27 and issues the following 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/S-PUMA/27

Amdt 1


Main Rotor Head Blade Horn Eye Bolts 4/2000

 

Applicability: Models AS 332 C, C1, L, and L1 helicopters; with eye bolts fitted to the blade horns, and whose eye bolt bearings were installed before 1 September 1997 and have been in service for less than 500 flying hours at the initial effective date of this airworthiness directive.

 

Requirement: Inspect in accordance with the Eurocopter AS 332 SB No 01-00-52.

 

Note: DGAC AD 1997-174-063(A)R1 refers.

 

Compliance: Unless already accomplished, within 50 hours time in service after 22 October 1997.

 

This Amendment becomes effective on 20 April 2000.

 

Background: A report was received of the deterioration of an eye bolt shaft bearing on the main rotor head blade horn which caused high amplitude vibrations in flight.

 

Amendment 1 revises the Requirement document and the DGAC AD reference only, no further work is required.

 

The original issue of this Airworthiness Directive became effective on 22 October 1997.


 

Eugene Paul Holzapfel

Delegate of the Civil Aviation Safety Authority 3 March 2000

 

 

 

 

 

 


The above AD is notified in the Commonwealth of Australia Gazette on 22 March 2000.

 

 

 

 

Overview

The Civil Aviation Regulations 1998 (CAR 1998) were enacted to regulate civil aviation safety and to establish standards for aircraft maintenance and operation within Australia. This legislation, overseen by the Civil Aviation Safety Authority (CASA), was introduced to address the need for comprehensive regulation and oversight in the civil aviation sector to ensure the safety and efficiency of air travel. One of the critical instruments under these regulations is the Airworthiness Directive (AD), which mandates corrective actions to be taken when an unsafe condition is identified in an aircraft. The AD aims to maintain the airworthiness of aircraft by requiring timely inspections and repairs to ensure safety standards are met. This legislative framework is crucial in preventing accidents and ensuring the highest standards of safety in the aviation industry.

Scope and Application

The Civil Aviation Regulations 1998, under the authority of the Civil Aviation Safety Authority (CASA), apply to the maintenance and operation of aircraft within Australia's national airspace. Specifically, Part 39 - 105 within the schedule of airworthiness directives targets particular models of aircraft, in this case, the Eurocopter AS 332 (Super Puma) series helicopters. This legislation applies to AS 332 C, C1, L, and L1 helicopters equipped with eye bolts fitted to the blade horns, provided these eye bolt bearings were installed prior to 1 September 1997 and have accumulated less than 500 flying hours by the initial effective date of this directive. The directive mandates an inspection in accordance with Eurocopter AS 332 SB No 01-00-52 to ensure compliance and rectify the identified unsafe condition. The directive is effective unless superseded by further amendments or additional airworthiness directives issued by CASA. The compliance timeline stipulates that the inspection must be completed within 50 hours of time in service after the initial effective date of 22 October 1997. This particular airworthiness directive, including its amendment, was published in the Commonwealth of Australia Gazette on 22 March 2000.

Key Provisions

The Civil Aviation Regulations 1998, specifically under Part 39, Section 105, address the issuance of Airworthiness Directives (ADs) for certain aircraft, in this case, Eurocopter AS 332 (Super Puma) Series helicopters. These ADs are essential tools used by the Civil Aviation Safety Authority (CASA) to ensure the safety of aircraft in operation by mandating specific actions to correct identified unsafe conditions. The key operative section here is Section 39.1 (1) of the CAR 1998, which provides the authority for CASA to issue such directives. The Airworthiness Directive AD/S-PUMA/27Amdt 1, issued on 3 March 2000, specifically targets the main rotor head blade horn eye bolts of AS 332 C, C1, L, and L1 models of the Super Puma helicopter, provided they were fitted with eye bolts and had their bearings installed before 1 September 1997 and have been in service for less than 500 flying hours at the directive's initial effective date. The AD imposes specific obligations on the operators of these helicopters. It mandates that the eye bolt shaft bearings on the main rotor head blade horns be inspected in accordance with the detailed instructions set out in Eurocopter AS 332 SB No 01-00-52. This inspection is necessary to address a reported condition where the deterioration of an eye bolt shaft bearing caused high amplitude vibrations in flight, posing a significant safety risk. Operators must ensure that this inspection is completed within 50 hours of time in service after the directive's effective date of 22 October 1997, unless it has already been accomplished. This requirement is further clarified by a note referencing DGAC AD 1997-174-063(A)R1, which provides additional context and instructions for the inspection process. Failure to comply with the provisions of this Airworthiness Directive could lead to serious safety issues. Although the specific penalties for non-compliance are not detailed in the provided text, non-compliance with CASA directives generally carries significant civil and criminal consequences. These can include fines, suspension of airworthiness certificates, and potential criminal charges for individuals responsible for the non-compliance. The severity of these consequences underscores the importance of adhering to CASA's safety directives to ensure the continued safe operation of aircraft within Australian airspace. The AD was formally notified in the Commonwealth of Australia Gazette on 22 March 2000, ensuring its legal effect and mandating compliance among the governed parties.

Legal classification tags

Area of Law
Aviation Law
Instrument
Legislative Instrument
Concepts
Definitions & Interpretation
Offence Provisions
Compliance Obligations

Interactions

Authorises

All Versions

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.