COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 56TC (Turbo Baron) Series Aeroplanes
AD/BEECH 56/1
Amdt 2
Rudder Spar and Hinges 5/68
Applicability: Model 56TC with S/Nos. TG-1 to TG-51.
Requirement: Action in accordance with Beechcraft SB 67-34, Rev. 1.
Compliance: Inspect for cracking within 100 hours’ time in service from 16 May 1968 and thereafter at intervals not exceeding 100 hours’ time in service until modified. Modify and inspect for alignment within 300 hours’ time in service from 16 May 1968.
Overview
The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, provide a framework for ensuring the safety of civil aviation. Part 39, specifically, contains the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, which includes amendments and safety measures for various aircraft. This legislative instrument addresses issues related to the airworthiness of specific aircraft models, ensuring that they meet safety standards and comply with necessary maintenance and inspection requirements. The policy objective is to safeguard the safety of passengers, crew, and the general public by enforcing rigorous safety protocols and regular maintenance checks for aircraft.
One example of such an amendment is AD/BEECH 56/1 Amendment 2 concerning the Beechcraft 56TC (Turbo Baron) Series Aeroplanes. This amendment applies to Model 56TC with serial numbers TG-1 to TG-51 and mandates specific actions to be taken in accordance with Beechcraft Service Bulletin 67-34, Revision 1. The requirement includes inspecting for cracking within 100 hours’ time in service from 16 May 1968 and thereafter at intervals not exceeding 100 hours’ time in service until modifications are made. Additionally, modifications and alignment inspections must be completed within 300 hours’ time in service from the same date. This directive underscores the importance of adhering to detailed maintenance schedules to prevent potential safety hazards associated with rudder spar and hinge issues.
Scope and Application
The Civil Aviation Safety Authority Schedule of Airworthiness Directives, specifically AD/BEECH 56/1 Amendment 2, pertains to Beechcraft 56TC (Turbo Baron) series aeroplanes with serial numbers TG-1 to TG-51. This legislative instrument mandates compliance with Beechcraft Service Bulletin 67-34, Revision 1, which requires an inspection for cracks in the rudder spar and hinges within 100 hours of time in service from 16 May 1968. This initial inspection must be followed by further inspections at intervals not exceeding 100 hours of time in service until modifications are made. Additionally, the directive mandates modification and inspection for alignment within 300 hours of time in service from the same date. The regulation applies to a specific subset of Beechcraft 56TC aeroplanes, ensuring that these aircraft maintain airworthiness standards set by the Civil Aviation Safety Authority. The directive is a component of the overarching framework provided by the Civil Aviation Regulations 1998 and is applicable within the jurisdictional reach of the Commonwealth of Australia.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39 - 105, address airworthiness directives pertinent to the Beechcraft 56TC (Turbo Baron) series aeroplanes. Section AD/BEECH 56/1 Amendment 2 pertains to the rudder spar and hinges, applicable to model 56TC with serial numbers TG-1 to TG-51 (section 5/68). The primary requirement of this directive is that operators must take action in accordance with Beechcraft Service Bulletin 67-34, Revision 1. Compliance with these directives is crucial for maintaining the safety and airworthiness of these aircraft.
Under these regulations, the operators of the specified Beechcraft 56TC series aeroplanes are obligated to conduct an inspection for cracking within 100 hours of time in service from the date of 16 May 1968. This initial inspection is crucial to identify any potential structural issues with the rudder spar and hinges. Following this initial inspection, subsequent inspections must be conducted at intervals not exceeding 100 hours of time in service until the modifications are implemented. Additionally, the operators must also modify and inspect for alignment within 300 hours of time in service from the same date. These actions are necessary to ensure that the aircraft remain compliant with airworthiness standards.
Failure to comply with these airworthiness directives may result in significant consequences. The Civil Aviation Regulations 1998 establish specific offences and penalties for non-compliance with airworthiness directives. While the exact penalties are not detailed within this particular legislative instrument, general provisions within the Civil Aviation Act 1988 and related regulations typically include fines and potential grounding of non-compliant aircraft. Non-compliance can also lead to criminal charges and civil liabilities, further underscoring the importance of adhering to these directives.
In summary, the Civil Aviation Regulations 1998 mandate that operators of Beechcraft 56TC series aeroplanes must adhere to specific inspection and modification requirements for the rudder spar and hinges. These requirements are designed to maintain the safety and airworthiness of the aircraft, with significant penalties for non-compliance. It is imperative for operators to follow these directives to avoid legal repercussions and ensure the continued safe operation of their aircraft.