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 56/23
Amdt 1
Elevators 12/84
Applicability: All models 56TC which have installed a new elevator with a S/No. referenced in Beechcraft SI No. 2030.
Requirement: Action in accordance with Beechcraft S.B. No. 2030.
Compliance: Unless already accomplished in accordance with Beechcraft SI No. 1207, within 100 hours’ time in service after 31 December 1984.
Background: Elevators on certain aeroplanes or aeroplanes fitted with replacement elevators may have improperly bonded honeycomb stiffener strips installed. S.B. No. 2030 extends compliance to other models, corrects part number errors and supersedes and cancels Service Instruction No. 1207.
Overview
The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, are a comprehensive set of rules governing the safety and operation of civil aviation within Australian airspace. One specific legislative instrument, F2006B04054, pertains to the airworthiness of Beechcraft 56TC (Turbo Baron) series aeroplanes. This regulation was introduced to address the issue of improperly bonded honeycomb stiffener strips on elevators of certain aeroplanes, particularly those that have had replacement elevators installed. The problem arises from the potential safety risks posed by such defects, which can compromise the structural integrity and operational safety of the aircraft. The policy objective is to ensure that the identified aircraft comply with the necessary safety standards to mitigate any associated risks. The Civil Aviation Safety Authority is the enacting body responsible for issuing these airworthiness directives and ensuring adherence to the specified compliance timelines.
This legislative instrument aims to safeguard the public by enforcing stringent safety standards on the airworthiness of Beechcraft 56TC aeroplanes. By mandating specific actions in accordance with Beechcraft Service Bulletin No. 2030, the regulation seeks to rectify the identified defects and ensure that these aircraft are operated safely. The requirement for compliance within 100 hours’ time in service after 31 December 1984 underscores the urgency and importance of addressing these issues promptly. Through the establishment of clear directives and timelines, the Civil Aviation Regulations 1998 play a crucial role in maintaining the high safety standards expected in Australian civil aviation.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all Beechcraft 56TC (Turbo Baron) series aeroplanes that have had a new elevator installed with a serial number referenced in Beechcraft Service Instruction No. 2030. This legislation is applicable to aircraft within the Commonwealth of Australia and is enforced by the Civil Aviation Safety Authority. The primary objective of this regulation is to ensure the airworthiness of these aircraft by addressing the issue of improperly bonded honeycomb stiffener strips in the elevators. The directive mandates that corrective action must be taken in accordance with Beechcraft Service Bulletin No. 2030, unless the required action has already been completed as per Beechcraft Service Instruction No. 1207. Compliance with this directive is necessary within 100 hours of time in service after 31 December 1984, unless the aircraft has already met the requirements of Beechcraft Service Instruction No. 1207. This regulation underscores the importance of maintaining the structural integrity of aircraft components to ensure safety in civil aviation.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes detailed directives concerning the airworthiness of certain aircraft models. For instance, AD/BEECH 56/23 Amendment 1 addresses elevators on Beechcraft 56TC (Turbo Baron) series aeroplanes (Section 12/84). This directive applies to all models 56TC that have had a new elevator installed, with serial numbers referenced in Beechcraft Service Instruction (SI) No. 2030. The primary requirement of this directive is that action must be taken in accordance with Beechcraft Service Bulletin (S.B.) No. 2030 (Section 12/84). Specifically, if compliance has not already been achieved pursuant to Beechcraft SI No. 1207, the required action must be completed within 100 hours’ time in service after 31 December 1984.
The obligations imposed by this regulation are quite clear. Owners and operators of the affected Beechcraft 56TC aeroplanes must ensure that any newly installed elevators are addressed according to the specific instructions laid out in Beechcraft S.B. No. 2030. This involves verifying the condition of the honeycomb stiffener strips on the elevators and taking corrective action where necessary. The compliance timeframe is stringent, mandating that these checks and any required modifications must be completed within 100 hours of operation after a specified date, ensuring that the aeroplanes remain in a safe and airworthy condition.
Failure to comply with the requirements set out in this directive can lead to serious consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce these regulations, and non-compliance could result in penalties or other legal actions. While the specific penalties are not detailed in this particular directive, they typically include fines, enforcement notices, or other measures that could affect the operator's ability to continue flying the aircraft until the required actions are taken and compliance is achieved. It is crucial for operators to adhere to these directives to avoid any potential repercussions that might arise from non-compliance.