AD/PROCTOR/10 (Re-Issue) - Front Seat Restraint Installations - Modification

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Legislation au F2006B06339 Not in force Legislative Instrument

Legislation content

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

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Percival Proctor Series Aeroplanes

 

AD/PROCTOR/10

(Re-Issue)


Front Seat Restraint Installations - Modification 11/72

 

Applicability: All models.

 

Requirement: Modify each front seat restraint installation by fitting a safety harness in accordance with a scheme approved by the Director- General.

 

Note: Guidelines for installation schemes are outlined in Airworthiness Advisory Circular No. 62 dated March 1972.

 

or DCA/PROCTOR/10.

 

Compliance: Before 1 December 1973.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, as part of Part 39, introduced by the Commonwealth of Australia, address the safety of airworthiness directives specifically targeting the Percival Proctor Series Aeroplanes. This legislative instrument, identified as F2006B06339, was enacted to ensure the safety and operational standards of these aircraft by mandating modifications to front seat restraint installations. The policy objective is to enhance the safety of pilots and passengers by requiring the installation of safety harnesses in front seats, as stipulated in the Airworthiness Directive AD/PROCTOR/10. This directive, reissued on 11 July 1972, applies to all models of the Percival Proctor Series and mandates compliance before 1 December 1973. The guidelines for these installation schemes are detailed in the Airworthiness Advisory Circular No. 62 dated March 1972, providing a framework for the required modifications to ensure adherence to aviation safety standards.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105 under the Civil Aviation Safety Authority Schedule of Airworthiness Directives, mandates modifications for Percival Proctor Series aeroplanes concerning the installation of front seat restraints. This directive applies universally to all models of the Percival Proctor Series aeroplanes, encompassing all entities and individuals involved in the operation, maintenance, or ownership of these aircraft. The regulation requires that each front seat restraint installation be modified to include a safety harness approved by the Director-General, with guidelines for the installation scheme provided in Airworthiness Advisory Circular No. 62 dated March 1972. Compliance with this directive is mandatory and must be achieved before 1 December 1973. The scope of the regulation extends throughout the Commonwealth of Australia, ensuring a uniform approach to aviation safety across all jurisdictions. There are no stated exclusions, exemptions, or thresholds specified in this particular directive, thereby enforcing a comprehensive application to all applicable aircraft within the prescribed timeframe.

Key Provisions

The Civil Aviation Regulations 1998, under Part 39 - 105, specifically address the airworthiness directives for the Percival Proctor Series Aeroplanes. Section 11/72 of this directive, AD/PROCTOR/10 (Re-Issue), mandates that all models of the Proctor series aeroplanes must have their front seat restraint installations modified. This modification requires the fitting of a safety harness that must comply with a scheme approved by the Director-General (s. 11/72). For guidance on the installation of these safety harnesses, reference can be made to Airworthiness Advisory Circular No. 62 dated March 1972, or DCA/PROCTOR/10, which provides detailed guidelines on the required installations. The Civil Aviation Regulations 1998 impose obligations on aircraft owners and operators to ensure that their aircraft comply with all specified airworthiness directives. Specifically, for the Percival Proctor Series Aeroplanes, this includes ensuring that the front seat restraint installations are modified to fit an approved safety harness before the compliance deadline of 1 December 1973 (s. 11/72). Failure to meet these requirements can result in the aircraft being deemed non-compliant and potentially grounding the aircraft until the necessary modifications are made. Breach of these airworthiness directives can have significant legal and safety consequences. The Civil Aviation Regulations 1998 do not explicitly outline the specific penalties for non-compliance with these directives within the provided text. However, non-compliance with civil aviation regulations generally can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). This may include fines, legal action, and the possibility of grounding or grounding of aircraft until the required modifications are completed. The severity of penalties may vary depending on the specific circumstances and the extent of non-compliance. It is crucial for aircraft owners and operators to adhere to these directives to ensure the safety of all persons on board and to avoid potential legal 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.