AD/CESSNA 210/64 - Aircraft Repair

Overview

The Civil Aviation Regulations 1998 were enacted by the Parliament of Australia to ensure the safety of civil aviation in the country. Specifically, Part 39 - 105 of these regulations pertains to airworthiness directives, which serve as a critical mechanism for addressing issues that could compromise the safety of aircraft. AD/CESSNA 210/64 targets the Cessna 210 Series aeroplanes repaired by Capricorn Aircraft Repair between 2 December 1985 and 29 November 1990. The directive was introduced to address discrepancies identified in structural repair data and replacement components, ensuring that any such issues are rectified to maintain the airworthiness of the affected aircraft. The objective is to mandate inspections to verify that repairs were conducted in accordance with approved data and that any replacement components are either identical to the originals or approved alternatives. Compliance with this directive is required at the next scheduled maintenance inspection following 21 March 1991, and any deficiencies must be rectified before further flight, with the Civil Aviation Safety Authority to be notified of all inspections conducted under this directive.

Scope and Application

The Civil Aviation Regulations 1998, as amended, govern the safety of aviation in Australia and include specific directives to ensure aircraft safety and compliance with operational standards. In this context, Part 39 - 105 of the Civil Aviation Regulations 1998 imposes a specific Airworthiness Directive (AD) for the Cessna 210 series aeroplanes, identified as AD/CESSNA 210/64. This particular directive applies to all aircraft of the Cessna 210 series that have undergone repairs by Capricorn Aircraft Repair, located in Thangool, Queensland, within the timeframe of 2 December 1985 to 29 November 1990. The directive mandates that these aircraft must be inspected to ensure that any repairs conducted by Capricorn Aircraft Repair were performed in accordance with approved data, and that any replacement components used in the repairs are either identical to the original components or are approved as suitable replacements. Any aircraft found to be non-compliant with these requirements must have the deficiencies rectified before further flight, and the Civil Aviation Safety Authority must be notified of all inspections conducted under this directive. Compliance with this directive must be achieved by the next scheduled maintenance inspection following 21 March 1991.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, outlines the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives, with AD/CESSNA 210/64 being pertinent to Cessna 210 series aeroplanes. This directive applies to all aircraft repaired by Capricorn Aircraft Repair in Thangool, Queensland, between 2 December 1985 and 29 November 1990. The primary requirement of this directive is for the aircraft to be inspected to ensure that any repairs conducted by Capricorn Aircraft Repair are supported by approved data (Section 1). Additionally, it mandates that the replacement components used in the repairs are identical to the original components they replaced or are approved as replacement components (Section 2). The obligations imposed by this directive are clear and specific. Aircraft owners or operators must ensure that the aircraft in question are inspected by qualified personnel to determine compliance with the approved data and component specifications (Section 3). This inspection must occur at the next scheduled maintenance inspection after 21 March 1991. Furthermore, if any discrepancies are found, such as the absence of approved data or the use of non-identical or non-approved replacement components, these deficiencies must be rectified before the aircraft can be cleared for further flight (Section 4). CASA must also be notified of any aircraft that have been inspected under this directive (Section 5). Failure to comply with the requirements of AD/CESSNA 210/64 can lead to several consequences. Aircraft found to be non-compliant with the approved data or component specifications will not be permitted to fly until the necessary corrections are made (Section 6). The directive does not explicitly state penalties for non-compliance, but it can be inferred that non-compliance could lead to enforcement actions by CASA, including the potential for grounding the aircraft and imposing fines or other sanctions. The specific penalties would be determined based on the nature and severity of the non-compliance, as per the broader regulatory framework under which CASA operates.