COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 310 Series Aeroplanes
AD/CESSNA 310/29 Wing Leading Edge Fuel Lines and
Wiring - Inspection and Modification
6/73
Applicability: All models 310C to 310Q with S/Nos. 35772 to 310Q0709 except those S/Nos. detailed in SL ME73-5, and all turbo 310 with S/Nos. 310P0001 to 310Q0709.
Requirement: Action in accordance with Cessna SL ME73-5 and supplement 2. Compliance: Within 100 hours time in service after 29 June 1973.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, are designed to ensure the safety and efficiency of civil aviation within Australia. Among the various parts and schedules of these regulations, Part 39 specifically addresses airworthiness directives, with Schedule 105 focusing on directives issued by the Civil Aviation Safety Authority (CASA). One such directive is AD/CESSNA 310/29, which pertains to the inspection and modification of wing leading edge fuel lines and wiring in Cessna 310 series aeroplanes. This directive was introduced to address safety concerns related to potential fuel leaks and electrical issues that could compromise the airworthiness and safety of the aircraft. The policy objective behind such regulations is to maintain the highest safety standards in civil aviation, ensuring the protection of passengers, crew, and the general public.
The AD/CESSNA 310/29 directive applies to all models 310C to 310Q with specific serial numbers and excludes those detailed in SL ME73-5, as well as all turbo 310 models within specified serial number ranges. The requirement is for actions to be taken in accordance with Cessna Service Letter ME73-5 and its supplement 2. Compliance with this directive must be achieved within 100 hours of time in service after 29 June 1973. This regulation is enforced by CASA to ensure that any identified issues are promptly addressed, thereby maintaining the safety and reliability of the aircraft in operation.
Scope and Application
The Civil Aviation Regulations 1998, under Part 39, Section 105, apply specifically to the Cessna 310 Series Aeroplanes, detailing Airworthiness Directives for these aircraft models. This legislation mandates inspections and modifications to the wing leading edge fuel lines and wiring for all Cessna 310 models ranging from 310C to 310Q with serial numbers from 35772 to 310Q0709, excluding those serial numbers detailed in SL ME73-5, as well as all turbo 310 models with serial numbers from 310P0001 to 310Q0709. The action required must comply with Cessna Service Letter ME73-5 and its supplement 2. Compliance with these directives is necessary within 100 hours of time in service after the directive's issuance on 29 June 1973. The scope of this regulation is limited to specific models and serial numbers of Cessna 310 aeroplanes, ensuring adherence to prescribed safety standards to maintain airworthiness.
Key Provisions
The Civil Aviation Regulations 1998, particularly Part 39 - 105, include detailed provisions under the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives. One such directive, AD/CESSNA 310/29, pertains specifically to the Cessna 310 Series Aeroplanes, addressing the wing leading edge fuel lines and wiring (section 1). This directive is applicable to all models 310C to 310Q with serial numbers (S/Nos.) ranging from 35772 to 310Q0709, except for those serial numbers detailed in Service Letter (SL) ME73-5, and to all turbo models with S/Nos. 310P0001 to 310Q0709. The requirement is to follow the action specified in Cessna SL ME73-5 and its supplement 2. Compliance with this directive must be achieved within 100 hours of time in service after 29 June 1973.
The obligations imposed by AD/CESSNA 310/29 are clear and specific. Aircraft operators and maintenance personnel must ensure that the inspections and modifications outlined in the referenced service letters are conducted meticulously. This includes verifying the integrity of the wing leading edge fuel lines and wiring, which are critical components for the safe operation of the aircraft. Operators must maintain accurate records of these inspections and any modifications made, ensuring that all work is performed in accordance with the detailed specifications provided by Cessna in SL ME73-5 and its supplements. This directive is designed to prevent potential failures that could compromise the safety of the aircraft during flight.
Failure to comply with AD/CESSNA 310/29 can result in serious consequences. The Civil Aviation Regulations 1998 establish various offences and penalties for non-compliance with airworthiness directives. The primary concern is the potential for accidents or incidents resulting from the failure to adhere to these safety measures. In terms of penalties, the maximum fines and potential criminal charges can be significant, depending on the severity of the breach and its impact on aviation safety. Operators found in violation of these requirements may face fines up to the maximum allowable by law, and in severe cases, criminal charges could be brought against the responsible parties, including both individuals and corporations. Additionally, non-compliance can lead to the grounding of the affected aircraft until the required actions are satisfactorily completed, which can have substantial financial and operational repercussions for the operator.