AD/AMD 20/6 - Rudder Pedal Assembly

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, were introduced to regulate civil aviation in Australia, providing a comprehensive framework for ensuring the safety and efficiency of air travel within the country. The specific legislative instrument, F2006B02373, pertains to Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, which includes amendments to the airworthiness directives for the Fan Jet Falcon (Falcon 20/Mystere-Falcon 200) series aeroplanes. This particular amendment, AD/AMD 20/6, focuses on the rudder pedal assembly and mandates compliance with AMD SB No. 429 (27-49) for all models, with a requirement that the action be completed before 30 April 1971. The policy objective of this regulation is to ensure the continued airworthiness and safety of the specified aircraft models by enforcing specific maintenance and modification standards.

Scope and Application

The Civil Aviation Regulations 1998, under Part 39 - 105, pertain specifically to the safety directives issued by the Civil Aviation Safety Authority (CASA) and apply to all models of the Fan Jet Falcon (Falcon 20/Mystere-Falcon 200) series aeroplanes. The regulation in question, AD/AMD 20/6, mandates that any rudder pedal assembly within these aircraft must comply with the specifications outlined in AMD Service Bulletin No. 429 (27-49). This directive is a critical safety measure and applies to all relevant aircraft irrespective of their owners or operators within Australia's jurisdiction. The compliance date set forth in the regulation is before 30 April 1971, which indicates that adherence to these safety directives was mandatory for ensuring the airworthiness of the specified aircraft models within that timeframe. No exclusions or exemptions are specified in the given text, implying that all applicable aircraft must strictly adhere to the outlined requirements. The regulation extends its reach through subordinate instruments, ensuring that the safety standards are uniformly implemented across the designated industry.

Key Provisions

The main sections of the Civil Aviation Regulations 1998 that are relevant to this legislative instrument are Part 39, which covers airworthiness directives, and specifically the section related to AMD Fan Jet Falcon (Falcon 20/Mystere-Falcon 200) Series Aeroplanes (section 39-105). This section outlines the applicability of the rudder pedal assembly directive for all models of the specified aircraft series and mandates compliance with the requirements set forth in the Airworthiness Maintenance Directive (AMD) Service Bulletin (SB) No. 429 (section 39-105(3/71)). Compliance with this directive must be achieved before 30 April 1971 (section 39-105(3/71)(b)). The obligations imposed by this Act on the parties or entities it governs include ensuring that the rudder pedal assembly of the Fan Jet Falcon (Falcon 20/Mystere-Falcon 200) Series Aeroplanes is inspected, repaired, or replaced as necessary in accordance with the requirements outlined in AMD SB No. 429. This means that the aircraft owner, operator, or any authorised maintenance personnel must follow the specific maintenance procedures and technical instructions provided in the service bulletin to ensure the rudder pedal assembly meets the necessary safety standards. Failure to comply with these requirements can result in the aircraft being deemed unairworthy, potentially leading to grounding and operational disruptions. The Civil Aviation Regulations 1998 also outline potential offences, penalties, and consequences for non-compliance with the airworthiness directives. Specifically, failure to adhere to the compliance date or to perform the required actions on the rudder pedal assembly can be considered a breach of the regulations. Such breaches may lead to enforcement actions by the Civil Aviation Safety Authority (CASA), including fines and other penalties. In severe cases, non-compliance can result in the suspension or revocation of the aircraft's airworthiness certificate, which could prevent the aircraft from operating until the necessary corrective actions are taken and compliance is verified.