COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 310 Series Aeroplanes
AD/CESSNA 310/54 Auxiliary Fuel Pump Wiring Modification 12/89
Applicability: All models 310 which have been modified in accordance with Cessna Service Bulletin MEB 88-3.
Requirement: Unless already accomplished, action in accordance with Cessna Service Bulletin MEB 88-3 Revision 1.
Note: This Requirement does not apply to aeroplanes that have not incorporated SB MEB 88-3.
Compliance: Prior to the issue of the next Maintenance Release after 31 December 1989.
Background: Compliance with the original issue of SB MEB88-3 was not considered to warrant the issue of an Airworthiness Directive. This AD is raised to ensure that necessary features of Revision 1 are incorporated into modified aeroplanes.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, address the need to ensure safe and efficient aviation practices across the country. Specifically, Part 39 - 105 of the Regulations provides a schedule of Airworthiness Directives that serve to maintain the safety standards of aircraft within Australia's airspace. One such directive is AD/CESSNA 310/54, which pertains to the Cessna 310 Series Aeroplanes, mandating the modification of auxiliary fuel pump wiring as per Cessna Service Bulletin MEB 88-3 Revision 1 for all models 310 that have undergone specific modifications. This legislative instrument aims to rectify any safety issues that may arise from non-compliance with the updated wiring requirements, ensuring that only aeroplanes that have incorporated the specified service bulletin are subject to these directives. The policy objective behind this regulation is to enhance the safety and reliability of civil aviation operations by enforcing necessary modifications on specific aircraft models.
Scope and Application
The Civil Aviation Safety Authority Schedule of Airworthiness Directives under Part 39 - 105 of the Civil Aviation Regulations 1998 pertains specifically to Cessna 310 Series Aeroplanes, with a focus on the auxiliary fuel pump wiring modification as outlined in AD/CESSNA 310/54. This directive applies to all models of the Cessna 310 series that have undergone modifications in line with Cessna Service Bulletin MEB 88-3. It mandates that unless the specified modifications have already been completed, all such modified aeroplanes must adhere to the requirements of Cessna Service Bulletin MEB 88-3 Revision 1. Importantly, this directive does not apply to Cessna 310 aeroplanes that have not been modified according to the aforementioned service bulletin. Compliance with these requirements is necessary before the issuance of the next Maintenance Release following 31 December 1989. This directive was instituted to ensure that the critical features outlined in Revision 1 of the service bulletin are implemented in aeroplanes that have already been modified under the original bulletin.
Key Provisions
The Civil Aviation Regulations 1998, particularly under Part 39, Section 105, include specific Airworthiness Directives (ADs) to ensure the safety and airworthiness of certain aircraft models. One such directive, AD/CESSNA 310/54, pertains to the Cessna 310 Series Aeroplanes, focusing on the modification of auxiliary fuel pump wiring. This directive applies to all models of the 310 series that have been modified in accordance with Cessna Service Bulletin MEB 88-3 (Section 12/89). The primary requirement, as outlined in the legislation, is that unless already completed, the action specified in Cessna Service Bulletin MEB 88-3 Revision 1 must be undertaken. It is crucial to note that this requirement does not apply to aeroplanes that have not incorporated the aforementioned service bulletin (SB MEB 88-3). Compliance with this directive must be achieved before the issuance of the next Maintenance Release after 31 December 1989.
The Civil Aviation Regulations impose specific obligations on the parties involved, particularly those operating Cessna 310 Series Aeroplanes that have been modified according to SB MEB 88-3. These obligations include ensuring that the auxiliary fuel pump wiring modifications as detailed in SB MEB 88-3 Revision 1 are completed by the specified deadline. Operators and maintenance personnel must adhere to the directives to maintain the airworthiness of the aircraft. The directive ensures that any modifications or actions are conducted in a manner that aligns with safety standards set by the Civil Aviation Safety Authority (CASA). Compliance with these directives is mandatory and must be verified through the appropriate maintenance release processes.
Failure to comply with the provisions of AD/CESSNA 310/54 could result in serious safety implications and potential legal consequences. The Civil Aviation Regulations do not explicitly state the penalties or consequences for non-compliance within the text of the directive itself. However, non-compliance with airworthiness directives generally leads to enforcement actions by CASA, which may include fines, suspension or revocation of the aircraft’s certificate of airworthiness, and potential criminal charges. The severity of penalties can vary depending on the nature and extent of the non-compliance, with CASA having the authority to impose appropriate sanctions to ensure adherence to safety standards. Operators are thus under a significant obligation to ensure that all modifications and compliance actions are carried out in a timely and effective manner.