AD/DHC-2/3 - Rudder Pedal Assembly - Modification

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, serve as the primary legislative framework governing civil aviation safety within the country. This legislation includes specific regulations to ensure that aircraft operations adhere to stringent safety standards. One such regulation, F2006B09048, was introduced as a legislative instrument to address issues related to the airworthiness of DHC-2 (Beaver) Series Aeroplanes, specifically focusing on rudder pedal assembly modifications. This regulation was established to ensure that any conversion from land-plane to float-plane configurations meets safety requirements, thereby preventing potential operational hazards. The policy objective is to maintain the highest standards of aviation safety through precise regulatory oversight and compliance measures.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertain to the Civil Aviation Safety Authority's Schedule of Airworthiness Directives for DHC-2 (Beaver) series aeroplanes, focusing on rudder pedal assembly modifications as outlined in AD/DHC-2/3. This legislation applies to all DHC-2 models with serial numbers ranging from 1 to 863 that are equipped with floats. Compliance with this directive is mandatory and must be met either before the issue of a Certificate of Airworthiness or upon conversion from a land-plane configuration to a float-plane configuration. The directive is grounded in the DH (Canada) Engineering Bulletin, Series "B" No. 2, Issue 2, ensuring that the modifications adhere to recognised engineering standards. The regulations extend across the Commonwealth of Australia, overseen by the Civil Aviation Safety Authority, and do not explicitly detail exclusions or exemptions within the provided text. The scope of the legislation is further extended and defined through subordinate instruments and notices, ensuring comprehensive application and enforcement within the aviation industry.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998 (CAR) Part 39 - 105, specifically concerning AD/DHC-2/3, relate to the modification of the rudder pedal assembly in DHC-2 (Beaver) Series Aeroplanes, particularly those with serial numbers 1 to 863 that are fitted with floats. Section 39.105 details the requirements for these modifications, which must be undertaken before the issue of a Certificate of Airworthiness (C of A) or upon conversion from a land-plane to a float-plane. The modification guidelines are outlined in the DH (Canada) Engineering Bulletin, Series "B" No. 2, Issue 2. Entities governed by this legislation are required to ensure that any DHC-2 Series Aeroplanes with the specified serial numbers and float configurations undergo the necessary rudder pedal assembly modifications as outlined in the referenced engineering bulletin. This includes performing any required checks and maintenance to comply with the safety directives. The regulations mandate that these modifications must be completed to maintain airworthiness and ensure compliance with the standards set by the Civil Aviation Safety Authority (CASA). In terms of consequences for non-compliance, the regulations impose both civil and potential criminal penalties for breaches. Failure to adhere to these directives can result in significant fines or other civil penalties, as stipulated under the Civil Aviation Act 1988. Moreover, in cases where the non-compliance leads to safety hazards or incidents, it could potentially incur criminal penalties. The maximum penalties for such breaches can vary, but they are severe, reflecting the critical nature of maintaining airworthiness standards in aviation. It is imperative for operators to strictly follow these directives to avoid any legal repercussions and to ensure the safety of all flights.