COMMONWEALTH OF AUSTRALIA (Civil Aviation Safety Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CASR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
DHC-2 (Beaver) Series Aeroplanes
AD/DHC-2/33 Exhaust Collector Ring Segments 7/2003
Applicability: All Bombardier Inc. DHC-2 Mk. 1 aeroplanes.
Requirement: 1. Remove the carburettor heater muff, part number (P/N) C2-EE-181A, -161A, - 171A, and -1155A and inspect the exhaust collector ring segments, P/N C2- EE251A, -253A, -255A, and -257A, for cracks or burnt holes.
2. Replace segments that have developed major breaks, cracks other than minor, or burning.
3. Segments with minor cracks must either be replaced or repaired by welding as per DHC-2 Beaver Maintenance Manual Para. 5.4.3, and DHC-2 Beaver Repair Manual Para. 6-13.
4. Replace segments that have developed further cracking from repair welds.
Note: Transport Canada AD CF-2002-49 refers.
Compliance: 1. Within 150 flight hours from the effective date of this directive and thereafter at intervals not to exceed 150 flight hours.
2, 3 and 4. Before further flight.
This Airworthiness Directive becomes effective on 10 July 2003.
Background: To prevent the possibility of a carburettor fire upon starting, particularly when the hot air valve control is in the “hot” position, this Directive requires a 150- hour repetitive inspection on exhaust collector ring segments to verify their integrity.
Jim Coyne
Delegate of the Civil Aviation Safety Authority 28 May 2003
The above AD is notified in the Commonwealth of Australia Gazette on 18 June 2003.
Overview
The Civil Aviation Safety Regulations 1998 (CASR) were enacted by the Parliament of Australia to regulate the safety aspects of civil aviation within the country. This legislation provides a comprehensive framework for ensuring that aircraft, aviation personnel, and operations meet stringent safety standards. The regulations were introduced to address the need for a cohesive and enforceable set of safety rules to prevent accidents and incidents in the civil aviation sector. The Civil Aviation Safety Authority (CASA), as the delegate of the Parliament, issues Airworthiness Directives under subregulation 39.1 (1) of CASR 1998 to mandate safety measures. These directives are critical in addressing specific safety concerns identified in aircraft or aeronautical products. The policy objective of these regulations is to maintain and enhance the safety of civil aviation, ensuring the protection of life and property both on the ground and in the air.
Scope and Application
The Civil Aviation Safety Regulations 1998, specifically under Part 39 - 105, mandate Airworthiness Directives issued by the Civil Aviation Safety Authority (CASA) to ensure the safe operation of aircraft and aeronautical products. This particular AD/DHC-2/33 pertains to the Bombardier Inc. DHC-2 Mk. 1 aeroplanes, requiring operators to inspect and maintain the exhaust collector ring segments to prevent potential carburettor fires. The directive necessitates a thorough inspection of the exhaust collector ring segments within 150 flight hours from the directive's effective date and at intervals not exceeding 150 flight hours thereafter, with immediate action required for any detected issues before further flights. This regulatory measure underscores the importance of regular maintenance checks to uphold the airworthiness of these aircraft and ensure safety in civil aviation operations.
Key Provisions
The Civil Aviation Safety Regulations 1998 (CASR) include detailed provisions under Part 39, specifically section 105, which mandates Airworthiness Directives (ADs) to ensure the safety of aircraft and aeronautical products. Section 39.1 (1) allows a delegate of the Civil Aviation Safety Authority (CASA) to issue such ADs. This particular AD, numbered AD/DHC-2/33, pertains to the DHC-2 (Beaver) Series aeroplanes and specifically targets the exhaust collector ring segments. The directive mandates the removal and inspection of certain carburettor heater muffs and exhaust collector ring segments for cracks or burn holes. Segments with significant damage must be replaced, while those with minor cracks can either be replaced or repaired via welding, following guidelines in the DHC-2 Beaver Maintenance Manual and Repair Manual. The directive also stipulates that these actions must be taken within specific flight hour intervals and before further flights.
Under this AD, the primary obligations imposed on the parties involve regular inspection and maintenance of the specified carburettor heater muffs and exhaust collector ring segments. Owners or operators of DHC-2 aeroplanes must ensure that these components are inspected within 150 flight hours from the directive's effective date and at intervals not exceeding 150 flight hours thereafter. In addition, any segments identified with major cracks or burn holes must be replaced, and those with minor cracks must either be replaced or repaired according to the specified manuals. These requirements are designed to mitigate the risk of carburettor fires, particularly when the hot air valve control is in the "hot" position.
Failure to comply with the Airworthiness Directive can result in serious consequences. Non-compliance with the stipulated inspection and repair requirements may lead to unsafe conditions that could potentially result in accidents. While the regulations themselves do not explicitly state the penalties for breach, non-compliance with ADs generally falls under the broader regulatory framework that may include fines, enforcement actions, or even criminal charges in severe cases. The severity of the penalties would depend on the extent of the breach and its impact on aviation safety. CASA retains the authority to enforce these directives and ensure that all obligations are met to maintain the highest safety standards in civil aviation.