COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes
AD/AC/78 Flight Control Chain Connector Link - Inspection 1/83
Applicability: Models 500, 500A, 500B, 500U, 520, 560, 560A, 560E, 560F, 680, 680E, 680F, 680F(P), 680FL, 680FL(P), 680T, 680V, 680W, 720, with S/Nos. 1 thru 1854.
Model 500S, S/Nos. 1755 thru 1876 and 3050 thru 3323.
Model 681, S/Nos. 6001 thru 6072.
Model 685, S/Nos. 12001 thru 12066.
Models 690, 690A and 690B, S/Nos. 11001 thru 11566.
Model 690C, S/Nos. 11600 thru 11727.
Model 690D, S/Nos. 15000 thru 15014.
Model 695, S/Nos. 95000 thru 95084.
Model 695A, S/Nos. 96001 thru 96042.
Document: Gulfstream American (Commander Division) SL No. 353. Compliance: Within 100 hours’ time in service after 1 February 1983.
Background: Installation of flight control chain connector link requires verification.
Overview
The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, aims to ensure the safety and regulation of civil aviation within the country. The legislation addresses the need for stringent safety standards and compliance measures to mitigate risks associated with civil aviation operations. Part 39 of these regulations, specifically pertaining to airworthiness directives, is critical in establishing requirements that aircraft manufacturers and operators must adhere to in order to maintain the highest safety standards. One such directive, AD/AC/78, focuses on the inspection of the flight control chain connector link for Twin Commander series aeroplanes, addressing potential safety issues by mandating regular verification and compliance within a specified timeframe. This directive is designed to ensure the continued airworthiness and safety of these aircraft, thereby protecting passengers, crew, and the general public.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, applies to all Twin Commander (Gulfstream/Rockwell/ Aerocommander 500, 600 and 700) Series Aeroplanes as outlined in AD/AC/78. The legislation mandates inspections of the flight control chain connector link for certain serial numbers and models, including but not limited to the specified Twin Commander aeroplanes with specific serial number ranges. This directive applies across the Commonwealth of Australia and is enforced by the Civil Aviation Safety Authority (CASA). The purpose of this regulation is to ensure the safety and airworthiness of the aircraft by requiring the inspection of the flight control chain connector link within 100 hours’ time in service after 1 February 1983. The regulations do not explicitly state any exclusions or exemptions, implying that all applicable aircraft must comply with the inspection requirements. The scope of application can be extended or further detailed through subordinate instruments issued by CASA.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes a schedule of airworthiness directives that govern the maintenance and inspection of aircraft. Section AD/AC/78 pertains to the flight control chain connector link inspection for Twin Commander (Gulfstream/Rockwell/Aerocommander 500, 600, and 700) series aeroplanes. This regulation applies to specific models and serial numbers, necessitating a thorough inspection of the flight control chain connector link. The directive requires compliance within 100 hours of time in service after 1 February 1983, as outlined in the document Gulfstream American (Commander Division) SL No. 353.
The obligations under this section are primarily focused on the verification and maintenance of the flight control chain connector link. Owners, operators, and maintenance personnel must ensure that the specified inspection is conducted within the stipulated timeframe. This involves a detailed examination of the connector link to ascertain its airworthiness, ensuring that it meets the required standards set forth by the Civil Aviation Safety Authority. The goal is to prevent any potential failures in the flight control system, which could compromise the safety of the aircraft.
Failure to comply with the airworthiness directive can result in significant consequences. Non-compliance may lead to the grounding of the affected aircraft until the necessary inspections and repairs are completed. This not only poses a risk to the safety of the flight but also incurs potential financial penalties. The severity of the penalties may vary, but under the Civil Aviation Regulations, penalties for non-compliance can include substantial fines and, in more severe cases, prosecution. The maximum penalties are not explicitly stated in the directive but can be severe, reflecting the importance of adhering to these safety regulations.
Additionally, any breaches of the airworthiness directive may lead to investigations by the Civil Aviation Safety Authority, which could result in further sanctions against the operators or owners of the aircraft. It is crucial for all parties involved to be fully aware of their obligations under this directive to avoid any legal or safety repercussions. The overarching aim of these regulations is to ensure the highest standards of aviation safety, and compliance is mandatory to achieve this goal.