AD/PC-6/33 - Lifting Sling and Aircraft Lifting Points - Limitations

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Legislation au F2006B06137 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

 


Pilatus Porter PC-6 Series Aeroplanes

 

AD/PC-6/33  Lifting Sling and Aircraft Lifting Points - Limitations


8/71

 

Applicability: All models. Document: Pilatus SB No. 010.

Compliance: Within 100 hours time in service after 30 September 1971.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, are a comprehensive set of rules designed to ensure the safety and efficiency of civil aviation within the country. Part 39, specifically, pertains to airworthiness directives, which are legally enforceable rules issued by the Civil Aviation Safety Authority (CASA) to address safety issues and ensure compliance with safety standards. This part was introduced to fill the gap in ensuring that all aircraft, including the Pilatus Porter PC-6 Series Aeroplanes, meet the necessary safety standards to operate in Australian airspace. One such directive, AD/PC-6/33, was introduced to address safety concerns related to the lifting sling and aircraft lifting points on the Pilatus Porter PC-6 Series Aeroplanes. This directive mandates compliance within 100 hours of time in service after 30 September 1971, as referenced in Pilatus Service Bulletin No. 010, to mitigate risks associated with the specified components and ensure the continued safety of these aircraft during operations.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39, mandates airworthiness directives under the jurisdiction of the Civil Aviation Safety Authority (CASA) to ensure the safe operation of aircraft within Australian airspace. The directive AD/PC-6/33 applies to all models of the Pilatus Porter PC-6 Series Aeroplanes and mandates compliance within 100 hours of time in service after 30 September 1971. This directive references Pilatus Service Bulletin No. 010, which outlines specific requirements and limitations regarding the lifting sling and aircraft lifting points. The directive applies to any person or entity operating these aircraft within Australia, including domestic and international flights, ensuring adherence to safety standards set forth by CASA. There are no stated exclusions or exemptions in this directive, and compliance is mandatory for the continued airworthiness of the specified aircraft models. The scope of this regulation can be further extended or clarified through subordinate instruments issued by CASA.

Key Provisions

The Civil Aviation Regulations 1998 (Cth), specifically Part 39 - 105, includes an Airworthiness Directive (AD) AD/PC-6/33 that applies to all models of Pilatus Porter PC-6 series aeroplanes (subsection 1). This directive mandates specific requirements regarding the aircraft’s lifting sling and lifting points. The directive is applicable to all Pilatus Porter PC-6 series aeroplanes and must be complied with within 100 hours of time in service after 30 September 1971 (subsection 2). Compliance is required to be achieved by adhering to Pilatus Service Bulletin No. 010, which provides detailed instructions and specifications on how to modify the lifting sling and aircraft lifting points to meet the safety limitations outlined in the AD. The obligations imposed by this AD are clear and specific. Operators and owners of Pilatus Porter PC-6 series aeroplanes must ensure that any modifications to the lifting sling and aircraft lifting points are carried out in accordance with Pilatus SB No. 010. This involves detailed technical work to ensure that the lifting points and slings meet the prescribed limitations and standards. Failure to comply with these requirements can result in the aircraft being considered unairworthy, which could prevent it from being operated legally. There are significant consequences for non-compliance with this AD. While the Civil Aviation Regulations 1998 do not explicitly outline specific penalties for non-compliance with ADs, general aviation regulations impose strict penalties for operating an aircraft that does not meet airworthiness standards. Such penalties may include fines, aircraft impoundment, and potential prosecution. In severe cases, where non-compliance leads to accidents or significant safety risks, criminal charges may be brought against the operator or responsible individuals, resulting in substantial fines and imprisonment. Ensuring adherence to this AD is, therefore, not only a regulatory requirement but also a critical safety measure to avoid these serious consequences.

Legal classification tags

Area of Law
Civil 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.