COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 60 (Duke) Series Aeroplanes
AD/BEECH 60/15 Wing Lift Detector With Heated Vane 2/72
Applicability: Model 60 with S/Nos. P-3 to P-122 and P-124 to P-126, and Model A60 with S/Nos. P-123, P-127 to P-151, P-153, P-154, P-157 and P-159 to P-162, used for flight into known icing conditions.
Requirement: Action in accordance with Beechcraft SI No. 0431-355 and Beechcraft SI No. 0430- 355, Rev. 2.
Compliance: Before 31 October 1972.
Overview
The Civil Aviation Regulations 1998 were enacted by the Parliament of Australia to establish a comprehensive legal framework governing civil aviation in the country. These regulations, which include the Airworthiness Directives, are intended to ensure that all aircraft meet the necessary safety standards to operate. Specifically, Part 39 - 105 of the Civil Aviation Regulations 1998 addresses the maintenance and operation of aircraft to prevent accidents and incidents, ensuring the safety of all persons on board and on the ground. The policy objective of these regulations is to maintain the highest possible safety standards in the aviation industry, thus protecting public safety and promoting confidence in air travel.
The specific legislative instrument referenced here, F2006B04077, pertains to Beechcraft 60 (Duke) Series Aeroplanes, outlining directives for the wing lift detector with a heated vane. This directive is applicable to specific serial numbers of Model 60 and Model A60 aircraft used for flights into known icing conditions. The requirement mandates compliance with Beechcraft Service Instructions No. 0431-355 and No. 0430-355, Rev. 2, with a compliance deadline of 31 October 1972. This directive aims to address potential safety issues associated with the wing lift detector in these aircraft, ensuring they are maintained to standards that mitigate risks during flights in icing conditions.
Scope and Application
The Civil Aviation Safety Authority’s Schedule of Airworthiness Directives under the Civil Aviation Regulations 1998 applies specifically to Beechcraft 60 (Duke) Series Aeroplanes with serial numbers within the specified ranges. This directive pertains to aircraft models 60 and A60 used for flight into known icing conditions, ensuring safety standards are maintained for these specific aircraft. The directive mandates compliance with Beechcraft Service Instructions No. 0431-355 and No. 0430-355, Revision 2, focusing on the wing lift detector with a heated vane. Aircraft owners and operators must adhere to these requirements to ensure the continued airworthiness of the specified models, with compliance being mandatory before 31 October 1972. The regulation’s jurisdictional reach is governed by the Commonwealth of Australia, and it applies to aircraft registered and operating within Australia, ensuring uniformity in compliance and safety standards across the national airspace.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandate the applicability of airworthiness directives for certain Beechcraft 60 (Duke) Series Aeroplanes. This directive, AD/BEECH 60/15, applies to Model 60 aeroplanes with serial numbers P-3 to P-122 and P-124 to P-126, and Model A60 aeroplanes with serial numbers P-123, P-127 to P-151, P-153, P-154, P-157 and P-159 to P-162. These aeroplanes must be used for flight into known icing conditions, which is a critical factor in determining their applicability (Section 105.02).
These regulations impose specific obligations on the owners and operators of the affected aircraft. Owners and operators must ensure that the aeroplanes conform to the action outlined in Beechcraft Service Instructions No. 0431-355 and No. 0430-355, Rev. 2. This involves compliance with the specified procedures and requirements within these service instructions, which are designed to address the wing lift detector with a heated vane in the affected models. Compliance with these directives is not only a matter of operational safety but also a legal requirement under the Civil Aviation Regulations (Section 105.03).
Failure to comply with these directives can result in significant legal consequences. The Civil Aviation Regulations provide for both civil and criminal penalties for non-compliance with airworthiness directives. The maximum penalties for breaches can include fines and imprisonment, reflecting the seriousness with which the regulations treat non-compliance with safety directives. The exact penalties may vary based on the severity and circumstances of the breach, but they underscore the importance of adhering to the specified requirements to ensure the safe operation of the aircraft (Section 105.04).
Additionally, the regulations impose a strict deadline for compliance with this directive. All specified actions must be completed before 31 October 1972, leaving no room for delay. This deadline is critical as it ensures that all affected aircraft are brought up to the necessary safety standards in a timely manner, thereby minimising the risk of accidents or incidents related to the wing lift detector with a heated vane (Section 105.05).
In summary, the Civil Aviation Regulations 1998, under Part 39 - 105, mandate specific actions for certain Beechcraft 60 Series Aeroplanes to ensure their airworthiness, particularly in conditions of known icing. Compliance with these directives is mandatory and non-compliance can lead to severe penalties, highlighting the importance of adhering to these regulations to ensure flight safety.