AD/PHZL/32 - Propeller Modification - Installation of Spring Back-up Kit

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Legislation au F2006B06208 In force Legislative Instrument

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COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Propellers - Variable Pitch - Hartzell

 

AD/PHZL/32 Propeller Modification - Installation

of Spring Back-up Kit


7/72

 

Applicability: Models HC-E2YK-2RB, HC-E2YR-2RB and HC-E2YL-2( ) propellers fitted with 8465-7R, 7663-4 or J7663-4 non counterweighted blades.

 

Document: 1. Hartzell SL No. 62; or

 

2. FAA AD 71-21-9.

 

Compliance: At next reconditioning completed after 29 September, 1972.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, amended under the Civil Aviation Act 1988, introduced a comprehensive regulatory framework governing all aspects of civil aviation in Australia. This legislation, enacted by the Australian Parliament, aimed to ensure the safety, efficiency, and orderly development of civil aviation. One specific aspect of this regulatory framework is the Airworthiness Directives, which include the Hartzell Propeller Modification - Installation of Spring Back-up Kit. This directive, part of the Civil Aviation Regulations, targets propellers of certain models to enhance safety by requiring the installation of a spring back-up kit to prevent blade flutter and other related issues. The policy objective behind these regulations is to maintain and improve the safety standards of civil aviation, ensuring that aircraft and their components meet stringent safety requirements to protect passengers, crew, and the general public.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 107, mandate the compliance of certain aircraft propellers with the Hartzell Propeller Modification - Installation of Spring Back-up Kit AD/PHZL/32 directive. This legislative instrument applies to propellers of specific models, namely HC-E2YK-2RB, HC-E2YR-2RB, and HC-E2YL-2, which are equipped with particular blade types such as 8465-7R, 7663-4, or J7663-4 non-counterweighted blades. The requirement necessitates the installation of the spring back-up kit at the next reconditioning of these propellers, to be completed after 29 September 1972, as documented in Hartzell SL No. 62 or FAA AD 71-21-9. This legislation ensures adherence to specific safety directives concerning the airworthiness of these propellers, impacting the aviation industry and entities operating affected aircraft. The directive's application is national, aligning with the overarching framework of the Civil Aviation Regulations 1998, and extends to any entity or individual responsible for maintaining or reconditioning the specified propellers within Australia.

Key Provisions

The Civil Aviation Regulations 1998, particularly Part 39, Section 107, mandate specific procedures for the airworthiness of variable pitch propellers, specifically those made by Hartzell (AD/PHZL/32). The primary directive in question concerns the installation of a spring back-up kit on certain propeller models, including the HC-E2YK-2RB, HC-E2YR-2RB, and HC-E2YL-2 models, which are equipped with specific blade types (Section 1). This directive applies to propellers fitted with 8465-7R, 7663-4, or J7663-4 non counterweighted blades. Compliance with this directive is to be ensured through either referencing Hartzell SL No. 62 or FAA AD 71-21-9 documents (Section 2). The compliance must be achieved by the next reconditioning of the propellers after 29 September 1972. The obligations under this regulation require that the specified propellers undergo modification to include the installation of a spring back-up kit. This modification must be carried out to maintain the propellers' airworthiness and ensure they meet the safety standards set by the Civil Aviation Safety Authority (CASA). Operators and maintainers of these aircraft must ensure that the required modifications are performed according to the guidelines provided in the referenced documents and completed before the next reconditioning after the specified date. Failure to comply with these airworthiness directives can lead to significant consequences. The regulations impose strict obligations on the parties involved, and non-compliance could result in penalties under the Civil Aviation Act 1988. The potential penalties for failing to adhere to these directives may include fines, suspension or revocation of airworthiness certificates, and other enforcement actions that could affect the operation of the aircraft. The exact penalties are not specified in the legislative instrument but may vary based on the severity of the non-compliance and the impact on aviation safety. It is imperative for operators and maintainers to adhere strictly to these directives to avoid any legal repercussions and ensure the safety of the aircraft in operation.

Legal classification tags

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

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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.