AD/P166/25 - Nose Landing Gear Steering Control Flange - Modification

Overview

The Civil Aviation Regulations 1998, under Part 39 - 105, outlines the Civil Aviation Safety Authority's Schedule of Airworthiness Directives. Specifically, Airworthiness Directive AD/P166/25 pertains to the Piaggio P166 Series Aeroplanes, focusing on the modification of the nose landing gear steering control flange. This directive was introduced to address potential safety issues associated with the specified component, ensuring that all applicable aircraft meet the necessary safety standards. The directive was enacted by the Civil Aviation Safety Authority, which operates under the Australian Government, with the policy objective of maintaining and enhancing the safety of civil aviation operations within Australia. This legislative instrument was designed to ensure that all operators of Piaggio P166 Series Aeroplanes comply with the outlined modifications to the nose landing gear steering control flange as stipulated in the Piaggio SB P166-35 or RAI AD 63-48/P166-20 documents. The requirement for compliance is immediate, underscoring the importance of these modifications for ensuring the safe operation of the aircraft in question.

Scope and Application

The Civil Aviation Regulations 1998, under Part 39 - 105, govern the safety and operational standards of civil aviation within Australia. Specifically, AD/P166/25 pertains to the Piaggio P166 Series Aeroplanes, addressing the modification of the Nose Landing Gear Steering Control Flange. This directive applies to any person or entity operating Piaggio P166 aeroplanes within Australia, ensuring compliance with safety directives outlined in Piaggio SB P166-35 or RAI AD 63-48/P166-20. The regulations are applicable nationally and mandate compliance immediately, ensuring the safety and airworthiness of these aircraft. The legislation does not explicitly state any exclusions or thresholds but relies on specified documents for detailed compliance instructions, allowing for the extension or restriction of application through subordinate instruments.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes the Civil Aviation Safety Authority's (CASA) schedule of airworthiness directives (ADs). One such AD is AD/P166/25, which pertains to the nose landing gear steering control flange modification for Piaggio P166 Series aeroplanes (10/63). This regulation mandates that the specified modifications to the nose landing gear steering control flange must be implemented as soon as possible, following either the Piaggio SB P166-35 or RAI AD 63-48/P166-20 requirement document. The AD/P166/25 imposes clear obligations on the parties and entities it governs. Operators and owners of Piaggio P166 Series aeroplanes must ensure that the nose landing gear steering control flange is modified according to the detailed instructions provided in either Piaggio SB P166-35 or RAI AD 63-48/P166-20. This modification is critical to maintaining the safety standards of the aircraft, and failure to comply could result in serious safety implications. Compliance must be achieved without undue delay, as specified by the regulation. Breaching the requirements set out in AD/P166/25 can lead to significant legal consequences. The Civil Aviation Regulations 1998 do not explicitly state penalties within this specific AD, but general provisions under the Civil Aviation Act 1988 may apply. Violations could result in civil penalties, such as fines, or criminal charges, depending on the severity and intent behind the non-compliance. The potential penalties can be severe, reflecting the importance of adhering to airworthiness directives to ensure the safety of the aviation industry.