COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Cessna 180, 182 and Wren 460 Series Aeroplanes
AD/CESSNA 180/66 King KFC 200 Flight Control System 10/82
Applicability: Models 182P and 182Q fitted with King KFC 200 flight control systems in accordance with STC SA1296CE.
Requirement: 1. Check the manual electric trim system travel time from full “nose up” to full “nose down” and full “nose down” to full “nose up”. This check should be carried out in accordance with King Installation Bulletin 215 Alert. The time to travel should be 40 + 8 seconds.
2. If the stop to stop time does not fall within 40 + 8 seconds, modify the system in accordance with King Installation Bulletin 215 Alert.
Compliance: Within 100 hours time in service after 31 October 1982.
Background: The manufacturer advises that for the system to meet safety requirements in a trim runaway (malfunction) condition, and still perform its intended function, the trim speed must fall within 40 + 8 seconds.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, were designed to establish a comprehensive regulatory framework governing civil aviation in Australia. One specific legislative instrument under these regulations, F2006B05078, targets the maintenance and safety standards of certain aircraft, including the Cessna 180, 182, and Wren 460 Series Aeroplanes. This instrument was introduced to address safety concerns regarding the flight control systems of these models, particularly focusing on the King KFC 200 system. The policy objective behind this regulation is to ensure that all aircraft maintain operational safety standards, preventing potential malfunctions that could compromise flight safety. The requirement outlined in the instrument mandates regular checks and modifications to the flight control system to comply with the specified time parameters, ensuring that the aircraft continue to operate within safe limits.
Scope and Application
The Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, specifically AD/CESSNA 180/66, pertains to Cessna 180, 182, and Wren 460 Series Aeroplanes. This directive applies to Models 182P and 182Q fitted with King KFC 200 flight control systems as per STC SA1296CE. The directive mandates that these aircraft undergo specific checks and modifications to their manual electric trim system to ensure compliance with safety standards. The requirement is to check the manual electric trim system travel time from full “nose up” to full “nose down” and vice versa, ensuring the time taken does not exceed 40 + 8 seconds as per King Installation Bulletin 215 Alert. If the time exceeds this limit, the system must be modified accordingly. Compliance with these directives is mandated within 100 hours of time in service after 31 October 1982. This legislation is applicable to the specified aircraft models and their flight control systems within Australia, and CASA oversees its enforcement to maintain airworthiness standards.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39, contain the schedule of airworthiness directives that govern the maintenance and safety of various aircraft, including the Cessna 180, 182 and Wren 460 Series Aeroplanes. In relation to these aircraft, Airworthiness Directive AD/CESSNA 180/66 pertains to the King KFC 200 flight control system on models 182P and 182Q. The directive requires operators to check the manual electric trim system travel time, ensuring it falls within 40 + 8 seconds from full “nose up” to full “nose down” and vice versa (Section 39-105). This check must be conducted in accordance with King Installation Bulletin 215 Alert. If the travel time does not meet this requirement, the system must be modified accordingly to meet the specified time.
Operators of affected aircraft must comply with the directive within 100 hours of time in service after 31 October 1982. This requirement ensures that the aircraft's manual electric trim system performs safely and effectively, particularly in the event of a trim runaway condition. The directive aims to maintain the integrity of the flight control system by adhering to the manufacturer's specifications, ensuring the aircraft remains airworthy and compliant with safety standards.
Failure to comply with the airworthiness directive can have serious consequences. The Civil Aviation Regulations 1998 impose significant obligations on aircraft operators to ensure their aircraft meet the required safety standards. Non-compliance with AD/CESSNA 180/66 could result in the aircraft being deemed unairworthy, which may lead to grounding and potential legal repercussions. Additionally, the Australian Civil Aviation Safety Authority (CASA) has the authority to take enforcement action against operators who fail to adhere to these directives, which can include fines and other penalties.
The potential penalties for non-compliance with airworthiness directives under the Civil Aviation Regulations 1998 can be severe. Civil penalties may include fines up to $33,000 for individuals and $165,000 for corporations, as outlined in the Civil Aviation Act 1988. In more serious cases, criminal penalties may apply, including imprisonment for up to two years for individuals and fines up to $1,100,000 for corporations. These penalties reflect the importance of adhering to safety directives to ensure the safety of all those involved in civil aviation.