COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 210 Series Aeroplanes
AD/CESSNA 210/46 Turbocharger - Inspection 6/80
Applicability: Model T210 S/Nos. T210-0001 thru T210-0454. Model 210 S/Nos. 21058140, 21059200 thru 21063954.
Document: 1. Cessna SIL No. SE 80-24; or
2. FAA AD 80-07-01, Amdt. 39-3719.
Compliance: Within 100 hours time in service after 30 June 1980.
Background: This Directive is issued to preclude a failure of the turbocharger anti-rotation pin and its ingestion into the scavenge pump. This in turn could cause a failure of the pressure and scavenge pumps.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, are a comprehensive set of rules governing civil aviation in Australia. This legislation aims to ensure the safety and efficiency of civil aviation operations within the country. One specific part of this regulation, Part 39 - 105, pertains to the Civil Aviation Safety Authority's Schedule of Airworthiness Directives. This section was introduced to address issues related to aircraft airworthiness and to ensure compliance with safety standards. The policy objective behind these directives is to mitigate risks associated with aircraft operations and maintain the highest possible safety standards. The legislative instrument F2006B08094, which falls under this part, mandates specific inspections and compliance for certain Cessna 210 Series aeroplanes to prevent potential failures that could compromise flight safety.
Scope and Application
The Civil Aviation Regulations 1998, under Part 39 - 105, specifically addresses the safety and airworthiness of certain aircraft models through Airworthiness Directives. The particular legislation identified as AD/CESSNA 210/46 pertains to the inspection of turbochargers on Cessna 210 Series aeroplanes. This applies to specific serial numbers of the T210 and 210 models, which must comply with the directive within 100 hours of time in service after 30 June 1980. The directive is designed to prevent potential failures of the turbocharger anti-rotation pin that could result in catastrophic engine failure. This regulatory measure is crucial for ensuring the safety of these aircraft, and compliance is mandatory for the specified serial numbers to maintain their airworthiness. The legislation extends its jurisdictional reach across the Commonwealth of Australia, ensuring consistent safety standards are upheld nationally.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39, mandate a series of Airworthiness Directives (AD) to ensure the safety of aircraft in Australian airspace. One such AD is AD/CESSNA 210/46, which concerns the inspection of turbochargers in Cessna 210 Series Aeroplanes (sections 39-105 and AD/CESSNA 210/46). This directive applies to the model T210 with serial numbers ranging from T210-0001 to T210-0454 and model 210 with serial numbers 21058140, 21059200 through 21063954. The directive mandates compliance with either Cessna Service Information Letter No. SE 80-24 or Federal Aviation Administration AD 80-07-01, Amendment 39-3719. The requirement is to inspect the turbocharger within 100 hours of time in service after 30 June 1980. The directive aims to prevent a failure of the turbocharger anti-rotation pin, which could otherwise be ingested into the scavenge pump, leading to potential failures of the pressure and scavenge pumps.
The obligations imposed by this directive on the parties involved, such as aircraft owners, operators, and maintenance personnel, are clear and precise. They must ensure that the specified inspection of the turbocharger is conducted within the stipulated timeframe. This inspection is critical to avoid the ingestion of the turbocharger anti-rotation pin into the scavenge pump, which could otherwise compromise the integrity of the pressure and scavenge pumps. The compliance with either the Cessna SIL No. SE 80-24 or FAA AD 80-07-01, Amdt. 39-3719, provides the technical guidelines and procedures that must be followed to meet the regulatory requirements.
Failure to comply with the AD/CESSNA 210/46 can lead to serious consequences. The Civil Aviation Regulations 1998 outline that non-compliance with an Airworthiness Directive is a breach of the regulations. Such breaches may result in enforcement actions which could include civil penalties, criminal charges, or both. The specific penalties for non-compliance are not detailed within the AD itself but are subject to the broader provisions of the Civil Aviation Act 1988. This could potentially include substantial fines or imprisonment, depending on the severity and frequency of the breach. The overarching aim is to ensure that all regulated parties adhere strictly to the safety directives to maintain the highest standards of aviation safety.