COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
C.A.C. CA-28 (Ceres) Series Aeroplanes
AD/CERES/5
Amdt 1
Pilot’s Safety Harness Inertia Reel - Installation 9/99
Applicability: All models.
Requirement: Modify the pilot’s shoulder harness installation by removing the harness release lock and attaching the shoulder straps to the aircraft structure through a multi-directional type inertia reel complying with the U.S. Specification MIL-R-8236 or other specification acceptable to the Secretary.
Note: Modifications performed in accordance with AD/CA-28/5 satisfy the requirements of this Directive.
Compliance: Before 1 July 1968.
This Amendment becomes effective on 9 September 1999.
Background The original issue of this Airworthiness Directive became effective on 18 April 1968.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, establish a comprehensive framework for ensuring the safety and efficiency of civil aviation within the country. The regulations, administered by the Civil Aviation Safety Authority (CASA), address various aspects of aviation operations, including aircraft maintenance, pilot qualifications, and airworthiness standards. One specific amendment, AD/CERES/5Amdt 1, pertains to the installation of pilot’s safety harness inertia reels in Ceres series aeroplanes. This directive was introduced to mitigate safety risks associated with the harness release mechanism, ensuring compliance with stringent safety standards. The objective is to mandate modifications to the harness installation to enhance pilot safety by incorporating a multi-directional inertia reel, thereby addressing potential hazards and maintaining the highest safety benchmarks in aviation operations.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all entities involved in the operation of civil aircraft within Australia, including aircraft manufacturers, operators, maintenance providers, and pilots. The regulation focuses on the installation of pilot's safety harness inertia reels for Ceres series aeroplanes, ensuring that they comply with specified standards to maintain airworthiness. This requirement extends to all models within the Ceres series, demanding that the harness release locks are removed and the shoulder straps are attached to the aircraft structure via a multi-directional inertia reel that meets the U.S. Specification MIL-R-8236 or an equivalent specification approved by the Secretary. Modifications carried out in accordance with AD/CA-28/5 are recognised as fulfilling the requirements of this directive. The amendment to the directive becomes effective on 9 September 1999, but compliance with the initial directive, which was effective from 1 July 1968, is mandated for all relevant parties. This legislation operates under the jurisdiction of the Commonwealth of Australia and aims to ensure the safety and reliability of civil aviation operations within the country.
Key Provisions
The key provision of the Civil Aviation Regulations 1998 (Part 39 - 105) mandates that all CA-28 (Ceres) series aeroplanes must modify their pilot’s shoulder harness installation (Section 39 - 105). Specifically, the requirement is to remove the harness release lock and attach the shoulder straps to the aircraft structure using a multi-directional type inertia reel that meets either the U.S. Specification MIL-R-8236 or another specification acceptable to the Secretary (AD/CERES/5 Amendment 1). This modification is applicable to all models of the CA-28 series. Additionally, it is noted that modifications carried out in accordance with AD/CA-28/5 will satisfy the requirements of this directive. This directive originally became effective on 18 April 1968, with compliance expected before 1 July 1968. The latest amendment to this directive was made effective on 9 September 1999.
Entities governed by this Act must ensure that all modifications to the pilot’s shoulder harness installation are completed in adherence to the specified requirements. This includes the removal of the harness release lock and the proper installation of the multi-directional inertia reel. The compliance date for these modifications was set before 1 July 1968, but any ongoing modifications must meet the requirements of the latest amendment, which became effective on 9 September 1999. It is essential that these modifications are carried out correctly to maintain airworthiness and safety standards.
Failure to comply with the provisions of the Airworthiness Directive can result in significant consequences. While specific penalties are not detailed in the text, non-compliance with Civil Aviation Regulations can typically lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Such actions may include fines, grounding of the aircraft, and other regulatory measures. The exact penalties would depend on the nature and severity of the non-compliance, as well as any resulting safety risks. It is imperative for operators to ensure adherence to these directives to avoid any adverse outcomes.