AD/CESSNA 210/2 - Nose Gear Downlock - Modification

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Legislation au F2006B08070 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 210 Series Aeroplanes

 

AD/CESSNA 210/2 Nose Gear Downlock - Modification 10/60

Applicability: All models with S/Nos. prior to 57524. Document: Cessna SL No. 210-13.

Compliance: Before 1 September 1971.

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Overview

The Civil Aviation Regulations 1998, enacted by the Commonwealth Parliament, form a crucial component of Australia's civil aviation legal framework. This legislation is designed to ensure that the operations, maintenance, and airworthiness of aircraft within Australian airspace meet internationally recognised standards, thereby addressing the need for comprehensive regulation in the rapidly evolving field of civil aviation. The regulations aim to enhance safety and efficiency in civil aviation by setting stringent standards for aircraft operations and maintenance. In particular, Part 39 - 105 of the Civil Aviation Regulations addresses specific airworthiness directives for various aircraft models, including the Cessna 210 Series Aeroplanes, to mitigate identified safety risks. One such directive, AD/CESSNA 210/2, pertains to the nose gear downlock modification for Cessna 210 models with serial numbers prior to 57524. This directive mandates compliance by 1 September 1971, reflecting the regulatory intent to proactively address potential safety hazards associated with the nose gear system. The policy objective underpinning these regulations is to ensure that all aircraft in operation meet necessary safety and airworthiness standards, thereby protecting passengers, crew, and the public from aviation-related risks.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the scope and application of airworthiness directives, including those pertinent to the Cessna 210 series aeroplanes. This legislation applies to all models of Cessna 210 aeroplanes with serial numbers prior to 57524, mandating compliance with specific safety directives to ensure the airworthiness of these aircraft. The regulations extend to all persons and entities involved in the operation, maintenance, and registration of these aircraft within the jurisdiction of the Commonwealth of Australia. This includes airlines, aircraft maintenance companies, and individual aircraft owners who must adhere to the stipulated modifications and compliance dates outlined in the Civil Aviation Safety Authority's directives. The application of these regulations is enforced nationally, ensuring uniform safety standards across all states and territories. Any deviation from these directives could result in non-compliance, potentially leading to regulatory action against the entities or individuals responsible. Additionally, the regulations can be extended or restricted through subordinate instruments issued by the Civil Aviation Safety Authority, which may provide further clarification or specific conditions applicable to the enforcement of these directives.

Key Provisions

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, outlines the requirements for the airworthiness of various aircraft, including the Cessna 210 series aeroplanes. In this context, section AD/CESSNA 210/2 pertains to a critical modification of the nose gear downlock mechanism for certain models of Cessna 210 aeroplanes (10/60). This directive applies to all models with serial numbers prior to 57524, as detailed in the Cessna Service Letter No. 210-13 (10/60). Compliance with this directive was required before 1 September 1971, ensuring that the aircraft's nose gear downlock mechanism meets the specified safety standards. For parties governed by these regulations, compliance involves ensuring that the specified modifications to the nose gear downlock mechanism are completed according to the specifications provided in the referenced service letter. This entails thorough inspection, repair, or replacement of the nose gear downlock as necessary to meet the safety requirements set forth by the Civil Aviation Safety Authority (CASA). Operators must verify that the modifications have been properly implemented and documented, maintaining records of compliance to demonstrate adherence to the mandated safety directives. Failure to comply with the airworthiness directives stipulated in the Civil Aviation Regulations 1998 can lead to serious consequences. The Act imposes obligations on aircraft operators and maintenance personnel to ensure that all mandated modifications are completed accurately and on time. Non-compliance with these directives may result in enforcement actions by CASA, including potential fines, suspension, or revocation of the aircraft’s airworthiness certificate. The severity of penalties can vary, but in cases of significant non-compliance, maximum penalties may include substantial financial fines and imprisonment for responsible individuals, underscoring the critical importance of adhering to these safety directives.

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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.