COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Piper PA-34 (Seneca) Series Aeroplanes
AD/PA-34/14 Fuel Line Chafing - Inspection 10/74
Applicability: Model PA-34-200 with S/Nos. 34-7250001 to 34-7450209. Document: Piper SB No. 429.
Compliance: Within 100 hours time in service after 31 October 1974.
Overview
The Civil Aviation Regulations 1998, administered by the Civil Aviation Safety Authority, were enacted to ensure the safety of aviation operations in Australia. The regulations establish standards and procedures that must be followed by all aviation entities to maintain a high level of safety. One of the key components of these regulations is the issuance of Airworthiness Directives (ADs), which are legal requirements aimed at correcting known safety deficiencies in specific aircraft models. The Piper PA-34 (Seneca) Series Aeroplanes Fuel Line Chafing - Inspection AD/PA-34/14, for instance, was introduced to address the problem of fuel line chafing in specific models of the Piper PA-34-200 series, with serial numbers ranging from 34-7250001 to 34-7450209. This directive mandates inspections to ensure that fuel lines are not compromised, thereby preventing potential fuel leaks that could lead to fire or other safety hazards. The policy objective of such directives is to proactively manage and mitigate safety risks, ensuring the continued airworthiness of the affected aircraft and the safety of passengers and crew.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertain to the Airworthiness Directives issued by the Civil Aviation Safety Authority (CASA) and address the safety of aircraft operations within Australia. One such directive, AD/PA-34/14, applies to Piper PA-34 (Seneca) Series aeroplanes, more precisely model PA-34-200 with serial numbers ranging from 34-7250001 to 34-7450209. This directive mandates an inspection of the fuel lines to prevent chafing, which is a critical safety measure to avoid potential fuel leaks and consequent fire hazards. Compliance with this directive is required within 100 hours of the aircraft's time in service after 31 October 1974, ensuring that the aircraft remain airworthy and meet the safety standards set by CASA. The directive is applicable to all entities operating these specific aircraft models within Australia and extends to any aviation operations conducted under the jurisdiction of the Commonwealth, ensuring a standardised approach to aircraft safety across the nation. The directive's applicability is delineated by the specified model and serial numbers, with no exclusions or exemptions provided within the text.
Key Provisions
The primary sections of the Civil Aviation Regulations 1998, Part 39 - 105 concerning the Piper PA-34 (Seneca) Series Aeroplanes (AD/PA-34/14) establish mandatory requirements for aircraft maintenance and inspection. Specifically, section 39-105 of the AD/PA-34/14 focuses on the inspection of fuel lines to prevent chafing. This applies to the model PA-34-200 with serial numbers ranging from 34-7250001 to 34-7450209. Compliance with these directives is necessary within 100 hours of time in service after 31 October 1974, as detailed in Piper Service Bulletin No. 429.
These regulations impose clear obligations on aircraft operators and maintenance personnel. They must ensure that the specified fuel lines on the Piper PA-34-200 series aircraft are inspected for any signs of chafing, wear, or damage. This inspection must be carried out within the stipulated 100 hours of operational time following the date of the directive. Failure to adhere to these requirements can result in non-compliance with aviation safety standards, potentially leading to grounding of the aircraft until the necessary inspections and repairs are completed.
Violation of the provisions outlined in the Civil Aviation Regulations 1998 can result in serious consequences. Under section 202 of the Civil Aviation Act 1988, non-compliance with Airworthiness Directives can lead to civil penalties, including fines of up to $22,200 for individuals and $111,000 for corporations, as stipulated by section 203. Additionally, enforcement actions can be taken by the Civil Aviation Safety Authority (CASA), which may include legal proceedings and potential criminal charges if the breach is deemed severe enough. The maximum penalties for criminal offences under the Civil Aviation Act 1988 can include fines of up to $275,000 and imprisonment for up to five years for individuals, and higher fines for corporations, reflecting the gravity of ensuring air safety compliance.