AD/CESSNA 188/6 - Rudder Stop

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, are a comprehensive set of rules governing all aspects of civil aviation within Australia. One specific piece of legislation under this regulatory framework is Part 39, which deals with airworthiness directives. These directives are critical in maintaining the safety standards of aircraft, and they ensure that any identified safety issues are addressed promptly and effectively. The policy objective of these regulations is to maintain a high standard of safety in the civil aviation sector by providing clear and enforceable guidelines that address potential safety risks. A particular instance of such regulations is found in AD/CESSNA 188/6 concerning the Cessna 188 (Agwagon) Series Aeroplanes. This directive was introduced to address a specific safety issue related to the rudder stop mechanism. The directive applies to all models 188 and A188 with serial numbers prior to 188-0318, with certain exceptions listed. The requirement involves compliance with Cessna Service Kit No. SK 188-13, referencing Cessna SL 67-53. This action must be completed before 1 April 1968, ensuring that the identified safety concerns are rectified in a timely manner. The Civil Aviation Safety Authority is responsible for enforcing these directives to ensure adherence and maintain the overall safety of civil aviation within Australia.

Scope and Application

The Civil Aviation Regulations 1998, as amended, govern the operation of aircraft in Australian airspace, including the maintenance and airworthiness of aircraft such as the Cessna 188 (Agwagon) Series Aeroplanes. Specifically, Part 39 - 105 within the Civil Aviation Regulations provides directives to ensure the safety of these aircraft, with AD/CESSNA 188/6 detailing a safety directive concerning the rudder stop. This directive applies to all Cessna 188 and A188 models with serial numbers prior to 188-0318, excluding certain serial numbers listed in the regulations. The directive requires compliance with Cessna Service Kit No. SK 188-13, referencing Cessna SL 67-53, and mandates that any necessary actions be completed before 1 April 1968. This regulation applies to aircraft operators, maintenance personnel, and other entities involved in the upkeep and operation of these aircraft within Australia, ensuring adherence to the specified safety standards to maintain the airworthiness of the aircraft. The geographic reach of this regulation is national, covering all operations and maintenance activities conducted within the Australian jurisdiction.

Key Provisions

The Civil Aviation Regulations 1998 (C1998L05182) in Part 39, particularly Section 105, outlines specific airworthiness directives for certain aircraft, such as the Cessna 188 (Agwagon) Series Aeroplanes. Specifically, AD/CESSNA 188/6 pertains to the rudder stop, and it applies to all models 188 and A188 with serial numbers prior to 188-0318, with a few exceptions listed (Section 105). The requirement under this directive mandates compliance with Cessna Service Kit No. SK 188-13, as referenced in Cessna SL 67-53, and this compliance must be achieved before 1 April 1968 (Section 105). Under this legislation, the primary obligation for the operators of Cessna 188 and A188 models within the specified serial number range is to ensure that the rudder stop action is performed in accordance with the prescribed service kit. This involves a detailed inspection and, if necessary, the modification or replacement of the rudder stop mechanism to meet the safety standards set forth by the Civil Aviation Safety Authority (CASA) (Section 105). This directive is critical for maintaining the airworthiness of these aircraft, ensuring that they remain safe for operation within Australian airspace. Failure to comply with the airworthiness directives stipulated in the Civil Aviation Regulations 1998 can result in significant consequences. Non-compliance may lead to enforcement actions under the Civil Aviation Act 1988, which could include fines, legal penalties, and potential grounding of the aircraft. The severity of the penalties depends on the nature and extent of the non-compliance, but they are designed to enforce strict adherence to safety standards. The maximum penalties can vary but are intended to ensure that all parties maintain the highest standards of airworthiness to protect public safety (Section 105).