COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Propellers - Variable Pitch - Hamilton Standard
AD/PHS/2
Amdt 1
Model 23260, 43E-60 and 43D-50 Reverse Solenoid Valve - Modification
6/66
Applicability: All model 23260, 43E60 and 43D50 propellers.
Requirement: Remove Hamilton Standard Model 67000 reverse solenoid valves and replace with approved, redesigned valves.
Compliance: Before installation in an aircraft after 28 July 1968.
Overview
The Civil Aviation Regulations 1998, amended in 2006, were introduced to regulate civil aviation safety in Australia, addressing gaps in the safety standards and procedures for aircraft operations. Enacted by the Parliament of Australia, these regulations aim to ensure the highest level of safety in the operation of aircraft by setting forth comprehensive safety standards. Specifically, the amendment F2006B06194 focuses on addressing issues related to the airworthiness of propellers, particularly those of the Hamilton Standard models 23260, 43E-60, and 43D-50. The policy objective of this amendment is to mandate the replacement of reverse solenoid valves in these propeller models to enhance their safety and reliability, ensuring compliance with the stringent airworthiness standards set by the Civil Aviation Safety Authority.
The Civil Aviation Regulations 1998, through their amendment, mandate that all model 23260, 43E-60, and 43D-50 propellers must remove the Hamilton Standard Model 67000 reverse solenoid valves and replace them with approved, redesigned valves. This directive is applicable to all such propellers and must be adhered to before their installation in an aircraft after 28 July 1968. The amendment is a direct response to identified safety concerns with the original solenoid valves, thereby reinforcing the commitment to maintaining the highest safety standards in civil aviation.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 107, pertains to the civil aviation safety authority's schedule of airworthiness directives, with a focus on propellers featuring variable pitch, such as those produced by Hamilton Standard. The particular legislative instrument referenced, AD/PHS/2 Amendment 1, applies to all model 23260, 43E-60, and 43D-50 propellers. This directive mandates the removal of Hamilton Standard Model 67000 reverse solenoid valves from these propellers and their replacement with approved, redesigned valves. The requirement for compliance with this airworthiness directive applies to any such propellers that are installed in an aircraft after 28 July 1968. The regulations are issued under the authority of the Commonwealth of Australia, ensuring a national standard of safety and compliance across the aviation industry within Australia. There are no exclusions or exemptions mentioned in this specific directive, and its applicability is consistent throughout the nation, reinforcing the importance of maintaining airworthiness standards across all territories and states.
Key Provisions
The Civil Aviation Regulations 1998, particularly in Part 39 under the section titled "Schedule of Airworthiness Directives" (107), address the mandatory modifications for specific propeller models to ensure safety and compliance. Specifically, Airworthiness Directive (AD) PH/S/2 Amendment 1 pertains to the modification of the reverse solenoid valves for Hamilton Standard Model 23260, 43E-60 and 43D-50 propellers. The directive mandates that all these model propellers must have the Hamilton Standard Model 67000 reverse solenoid valves removed and replaced with approved, redesigned valves (107). This requirement must be fulfilled before any installation of the propeller in an aircraft after 28 July 1968 (107).
In terms of obligations, the regulation places a clear requirement on the operators and maintainers of the specified propeller models to ensure the replacement of the reverse solenoid valves. This means that any person responsible for the maintenance or operation of these propellers must adhere to the directive and complete the specified modifications. Failure to comply with this directive can result in serious safety issues, as the original design of the solenoid valves was found to be inadequate, posing a potential risk to the aircraft and its occupants. Therefore, it is imperative that the replacement of these components is carried out meticulously and in accordance with the specified timeline.
Failure to comply with this Airworthiness Directive could result in significant consequences. The Civil Aviation Safety Authority (CASA) enforces strict compliance with these regulations to ensure the highest safety standards in aviation. Non-compliance could lead to enforcement actions, including fines and other penalties. The potential civil penalties for breaching these regulations can be substantial, and in severe cases, criminal charges could be brought against individuals or entities found to be in violation. The maximum penalties for such breaches are not explicitly stated in the directive but generally align with the broader civil aviation regulatory framework, which can include fines and imprisonment for serious offences. It is, therefore, crucial for all parties involved to take the directive seriously and ensure full compliance to avoid any legal repercussions.