AD/CESSNA 180/52 - Nose Gear Drag Strut Attach Fitting

Overview

The Civil Aviation Regulations 1998, which were enacted by the Parliament of Australia, address various aspects of aviation safety and regulation. Specifically, Part 39 - 105 of these regulations, established by the Civil Aviation Safety Authority, sets forth a schedule of airworthiness directives to ensure that aircraft meet safety standards. One such directive, AD/CESSNA 180/52, focuses on the nose gear drag strut attach fitting of Cessna 180, 182, and Wren 460 series aeroplanes. This directive was introduced to address a specific safety issue related to the nose gear strut attach bolt, aiming to mitigate any potential risks by modifying the fitting to prevent accidental removal or disengagement. Compliance with this directive is mandatory and must be achieved before an Australian Certificate of Airworthiness can be issued.

Scope and Application

The Civil Aviation Regulations 1998, specifically under Part 39 - 105 concerning Airworthiness Directives, apply to all operators of Cessna R182 aircraft within the Australian jurisdiction. This regulation is part of the broader framework overseen by the Civil Aviation Safety Authority (CASA) and is designed to ensure that all aircraft meet specific safety standards. The directive mandates modifications to the nose gear drag strut attach fitting of the Cessna 182 series to enhance safety and reliability. Operators must modify the nose gear drag strut attach fitting, P/N 2243009-1, by blanking off a specific hole with a steel button, P/N CM 2692-32, sealed with Pro-Seal No. 700, to prevent any potential issues that might arise from the original design. Compliance with this directive is required before the issuance of an Australian Certificate of Airworthiness, ensuring that all aircraft meet the prescribed safety standards before being cleared for operation.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, detail the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives for certain aircraft models. For Cessna 180, 182, and Wren 460 series aeroplanes, AD/CESSNA 180/52 mandates the modification of the nose gear drag strut attach fitting for all models of the Cessna R182. This directive requires the fitting to be modified by blanking off the hole originally intended for the installation and removal of the nose landing gear strut attach bolt (Section 1). The modification must be carried out using a steel button, identified as P/N CM 2692-32, which should be sealed with Pro-Seal No. 700, ensuring that the closure is both readily removable and replaceable when necessary (Section 2). The obligations under this directive are clear and specific. Owners or operators of the affected aircraft must ensure that the modification is performed before the aircraft is issued an Australian Certificate of Airworthiness (Section 3). This requirement underscores the importance of adhering to CASA's safety directives to maintain the airworthiness of the aircraft. The directive mandates that the fitting must be modified in accordance with the specified procedures to avoid any risk associated with the original design, which could potentially compromise the structural integrity and safety of the aircraft during operation. Failure to comply with this airworthiness directive can result in serious consequences. Under the Civil Aviation Regulations 1998, non-compliance with an AD can lead to penalties, including fines and potential criminal charges. The exact penalties are not detailed in the provided text, but generally, CASA has the authority to impose significant financial penalties and may pursue criminal charges for serious violations. These consequences serve as a deterrent against non-compliance, ensuring that all aircraft meet the necessary safety standards before being returned to service.