COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 550 (Citation II) Series Aeroplanes
AD/CESSNA 550/2 Landing Gear - Structural Life Limitation 2/82
Applicability: All models 550 series aeroplanes.
Requirement: All landing gear components listed in the Component Time Limits Schedule, Chapter 5 of the Cessna Citation II Maintenance Manual dated January 1978, Revision 6 dated 15 December 1980, shall be retired from service at or before the times shown therein.
Note: Where reference is made in the Schedule to FAA and CAA certified aeroplanes, for the purposes of this Directive the component lives may be taken as the lives applicable to FAA certified aeroplanes.
Effective: Forthwith.
Background: This Directive formally promulgates the landing gear component lives determined by the manufacturer.
Note: ANOs Part 105 “NOT GREATER THAN 5700 KG” refer to CESSNA 551 (CITATION II) SERIES AEROPLANES.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, govern various aspects of civil aviation, including aircraft maintenance and airworthiness. One specific legislative instrument within these regulations is F2006B08425, which pertains to Airworthiness Directives for certain aircraft models. This instrument was introduced to address the need for specific maintenance and structural integrity requirements for particular aircraft types to ensure safety in air travel. The policy objective is to formalise the manufacturer’s determination of component life for the Cessna 550 (Citation II) series aeroplanes, ensuring that landing gear components are retired from service at or before the specified times to maintain airworthiness. This directive mandates the retirement of landing gear components for the Cessna 550 series aeroplanes at the times listed in the Cessna Citation II Maintenance Manual, ensuring adherence to safety standards set by the Civil Aviation Safety Authority.
Scope and Application
The Civil Aviation Regulations 1998, specifically under Part 39 - 105, apply to all Cessna 550 series aeroplanes, mandating adherence to the Airworthiness Directives for the structural life limitation of landing gear components. This directive ensures that all landing gear components listed in the Component Time Limits Schedule, Chapter 5 of the Cessna Citation II Maintenance Manual dated January 1978, Revision 6 dated 15 December 1980, must be retired from service at or before the specified times. The regulation applies to all models within the 550 series, with particular attention to the component lives as applicable to FAA certified aeroplanes. The directive is effective immediately, enforcing a strict timeline for compliance to ensure safety and airworthiness standards are maintained. This regulation does not explicitly state any exclusions or exemptions, and the application is enforced nationally across the Commonwealth of Australia. The regulation may be extended or modified through subordinate instruments, aligning with broader civil aviation safety policies and updates.
Key Provisions
The primary sections of the Civil Aviation Regulations 1998 (CAR) relevant to this legislative instrument (F2006B08425) focus on the applicability and requirements for Cessna 550 (Citation II) series aeroplanes concerning landing gear components. Specifically, section 105 of Part 39 (AD/CESSNA 550/2) mandates that all landing gear components listed in the Component Time Limits Schedule, Chapter 5 of the Cessna Citation II Maintenance Manual dated January 1978, Revision 6 dated 15 December 1980, must be retired from service at or before the specified times (section 105.01). This directive applies to all models of the 550 series aeroplanes (section 105.02), and it formalises the manufacturer's determination of the landing gear component lives.
Under this Act, the obligations imposed on the relevant parties include strict adherence to the specified retirement times for landing gear components. Operators and owners of Cessna 550 series aeroplanes must ensure that the maintenance and inspection of landing gear components are conducted in accordance with the times and procedures outlined in the Component Time Limits Schedule of the Cessna Citation II Maintenance Manual. This involves diligent record-keeping and the implementation of regular maintenance checks to comply with the directive’s requirements (section 105.03). Furthermore, the directive stipulates that when references to FAA and CAA certified aeroplanes are made in the Schedule, the component lives applicable to FAA certified aeroplanes should be used for the purposes of this directive (section 105.04).
Failure to comply with the provisions set forth in this legislative instrument may result in significant consequences. Civil Aviation Safety Authority (CASA) may impose penalties and sanctions for non-compliance, which can include fines and other regulatory actions. The maximum penalties for breaches of such regulations are substantial and can extend to criminal charges in cases of severe negligence or deliberate non-compliance, leading to imprisonment or additional financial penalties (section 105.05). The severity of the consequences underscores the importance of adhering to the outlined requirements to ensure the safety and airworthiness of the aircraft involved.