COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 50 (Twin Bonanza) Series Aeroplanes
AD/BEECH 50/18
Amdt 3
Elevator Control Rod 12/78
Applicability: All model 50 with S/Nos. H-1 to H-11;
All models B50 and C50 with S/Nos. CH-12 to CH-360;
All models D50, D50A, D50B, D50C and D50E with S/Nos. DH-1 to DH-347; All model E50 with S/Nos. EH-1 to EH-70;
All model F50 with S/Nos. FH-71 to FH-96;
All model G50 with S/Nos. GH-94, GH-97 to GH-119; All model H50 with S/Nos. HH-120 to HH-149;
All model J50 with S/Nos. JH-150 to JH-176.
Requirement: Action in accordance with Beechcraft SI No. 0334-152, Rev. III. Compliance: As per Requirement Document.
Overview
The Civil Aviation Regulations 1998, established by the Commonwealth of Australia, aim to ensure the safety and efficiency of civil aviation within the country. One aspect of these regulations is Part 39, which includes 105 Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives. This part addresses specific issues related to the airworthiness of aircraft, ensuring that they meet the required safety standards. The directive for the Beechcraft 50 (Twin Bonanza) Series Aeroplanes, specifically AD/BEECH 50/18 Amendment 3 concerning the elevator control rod, was introduced to address a gap in the safety protocols for certain models of the Beechcraft 50 series. The objective of this amendment is to ensure compliance with the specified requirements to mitigate any potential safety risks associated with the elevator control rod.
The Beechcraft 50 series aircraft covered under this directive include specific serial number ranges for various models such as H-1 to H-11, CH-12 to CH-360, DH-1 to DH-347, and so on. The directive mandates actions in accordance with Beechcraft Service Instruction No. 0334-152, Revision III, to address issues related to the elevator control rod. Compliance with this directive is essential to maintain the airworthiness of the affected aircraft, and it is to be executed as per the requirements outlined in the specified service instruction. The directive is enacted by the Commonwealth of Australia, with the policy objective being to enhance the safety and reliability of civil aviation operations.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 – 105 of the Civil Aviation Safety Authority's Schedule of Airworthiness Directives, applies to all Beechcraft 50 (Twin Bonanza) series aeroplanes within specified serial number ranges. These ranges encompass models H-1 to H-11, B50 and C50 from CH-12 to CH-360, D50, D50A, D50B, D50C and D50E from DH-1 to DH-347, E50 from EH-1 to EH-70, F50 from FH-71 to FH-96, G50 from GH-94, GH-97 to GH-119, H50 from HH-120 to HH-149, and J50 from JH-150 to JH-176. The directive mandates compliance with Beechcraft Service Instruction No. 0334-152, Rev. III, ensuring that the relevant elevator control rod action is taken as outlined in the requirement document. This regulation is applicable on a national scale within the Commonwealth of Australia and is enforced by the Civil Aviation Safety Authority. The Act does not specify any exclusions, exemptions, or thresholds within the provided excerpt, but it is noted that further details may be governed through subordinate instruments or additional documentation.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39, detail the requirements for airworthiness directives which are critical for ensuring the safety and airworthiness of aircraft. Section 39-105 of these regulations addresses specific directives for various aircraft models, including the Beechcraft 50 (Twin Bonanza) series aeroplanes. The directive AD/BEECH 50/18 Amendment 3 pertains to the elevator control rod and applies to a specific range of serial numbers for various models of the Beechcraft 50 series (sections 39-105).
The main requirement of AD/BEECH 50/18 Amendment 3 is that the elevator control rod must be actioned in accordance with Beechcraft Service Instruction (SI) No. 0334-152, Revision III (section 39-105). This directive is applicable to a specific set of serial numbers for each model of the Beechcraft 50 series, ranging from H-1 to JH-176. The compliance for this directive must be carried out as per the instructions outlined in the requirement document provided by Beechcraft.
Entities and individuals governed by these regulations are obligated to ensure that the specified action on the elevator control rod is carried out meticulously as per the service instruction provided. This includes the aircraft owners, operators, and maintenance personnel who must follow the steps and guidelines outlined in the directive to maintain the airworthiness of the aircraft. Compliance involves ensuring that all necessary inspections, repairs, or replacements are conducted by qualified personnel in accordance with the specified service instruction.
Failure to comply with the provisions outlined in AD/BEECH 50/18 Amendment 3 can lead to serious safety risks and potential legal consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce these directives, and non-compliance can result in enforcement actions, including fines and other penalties. The specific penalties for non-compliance are not detailed in the provided text but are typically governed by other sections of the Civil Aviation Regulations, which can include substantial monetary penalties and potential criminal charges for serious breaches.