AD/CESSNA 400/74 - Fuel Pressure Switch Line - Inspection and Modification

Administered by Department of Infrastructure, Transport, Regional Development, Communications, Sport and the Arts

Legislation au F2006B08357 Not in force Legislative Instrument

Legislation content

COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY

SCHEDULE OF AIRWORTHINESS DIRECTIVES

 


Cessna 400 Series Aeroplanes

 

AD/CESSNA 400/74 Fuel Pressure Switch Line - Inspection

and Modification

Applicability: Model 402C with S/Nos. 402C0001 to 402C0292; Model 414A with S/Nos.

414A0001 to 414A0500.

 

Document: Cessna SIL No. ME80-23.

 

Compliance: Within 50 hours time in service after 13 August 1980.


9/80

 

Background:  An improved support is now available for the fuel pressure switch line in the engine nacelle. Chafing failure of this line may cause fuel to be sprayed on to the exhaust system.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, play a critical role in ensuring the safety and efficiency of the nation’s civil aviation operations. The legislation provides a comprehensive framework to govern various aspects of civil aviation, including the airworthiness of aircraft, licensing of personnel, and the establishment of safety standards. One of the key objectives of these regulations is to mitigate risks associated with aircraft operations, thereby enhancing the overall safety of civil aviation. The 1998 regulations were introduced to address the evolving challenges in the aviation industry, ensuring that Australian aviation remains compliant with international standards and best practices. Specifically, the Civil Aviation Regulations 1998 include provisions for issuing Airworthiness Directives (ADs) to address identified safety issues. For instance, AD/CESSNA 400/74 pertains to Cessna 400 Series Aeroplanes, mandating an inspection and modification of the fuel pressure switch line for certain models to prevent potential chafing failures that could lead to hazardous fuel spraying. This directive aims to ensure the continued airworthiness and safety of the affected aircraft, reflecting the regulatory body’s commitment to maintaining high safety standards within the industry.

Scope and Application

The Civil Aviation Regulations 1998, specifically PART 39 - 105, addresses the airworthiness directives related to certain models of Cessna 400 series aeroplanes. This legislative instrument applies to specific models of the Cessna 400 series, namely the Model 402C with serial numbers ranging from 402C0001 to 402C0292, and the Model 414A with serial numbers from 414A0001 to 414A0500. The regulation mandates that these aircraft must comply with the airworthiness directive within 50 hours of time in service after 13 August 1980. This directive aims to ensure safety by addressing potential chafing failure of the fuel pressure switch line, which could lead to fuel spraying onto the exhaust system. The regulation's jurisdictional reach is national, as it falls under the purview of the Commonwealth of Australia and the Civil Aviation Safety Authority. There are no stated exclusions or exemptions in the directive, and it extends its application through the specific identification of affected aircraft models and serial numbers.

Key Provisions

The Civil Aviation Regulations 1998, specifically Part 39 - 105, under the Civil Aviation Safety Authority's schedule of airworthiness directives, mandates particular requirements for the inspection and modification of fuel pressure switch lines in Cessna 400 series aeroplanes. This directive, AD/CESSNA 400/74, applies to the Model 402C with serial numbers ranging from 402C0001 to 402C0292 and Model 414A with serial numbers from 414A0001 to 414A0500. This regulation references the Cessna SIL No. ME80-23, which provides detailed instructions for compliance. According to the directive, compliance must be achieved within 50 hours of time in service after 13 August 1980. The primary obligation under this directive is to ensure that an improved support for the fuel pressure switch line in the engine nacelle is installed. This is crucial because chafing failure of this line may result in fuel being sprayed onto the exhaust system, which poses a significant safety risk. The directive mandates that the necessary inspection and modification must be completed within the specified timeframe to mitigate any potential hazards. Entities and operators of the affected Cessna 400 series aeroplanes must adhere to the requirements outlined in the AD/CESSNA 400/74 directive. This involves conducting a thorough inspection of the fuel pressure switch line and ensuring that any necessary modifications are performed according to the specifications provided in the referenced SIL No. ME80-23. Failure to comply with these requirements could result in serious safety concerns and potential operational issues. Non-compliance with the airworthiness directive AD/CESSNA 400/74 may lead to civil or criminal consequences. Under the Civil Aviation Act 1988, operators found in breach of the regulations may face penalties, including fines and potential prosecution. The exact penalties can vary, but they are established to enforce adherence to safety standards and to ensure the airworthiness of the aircraft. It is imperative for operators to ensure timely compliance to avoid any legal ramifications.

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Sourced from the Federal Register of Legislation at 26 August 2026. For the latest information on Australian Government law please go to https://www.legislation.gov.au.