COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 65 and 70 (Queen Air) Series Aeroplanes
AD/BEECH 65/54
Amdt 2
Aft and Nose Hinged Baggage Door Latching 3/89
Applicability: All models Queen Air 65, A65 and A65-8200 with S/Nos. L-1, L-2, LF-7, LF-8, LC- 1 to LC-335.
All models 65-80, 65-A80, 65-A80-8800 and 65-B80 with S/Nos. LD-1 to LD-505. All models 70 with S/Nos LB-1 through LB-35.
Requirement: Action in accordance with Beechcraft SI No 1126 Rev 1. Compliance: Within 100 hours’ time in service after 31 July 1980.
Background: To provide a more effective bellcrank stop for the hinged baggage door latch mechanism taking into account the possibility of dimensional variations in some original installations. Amendment 2 concerns reference to Rev 1 of SB and consolidates Queen Air series 65 and 70, aircraft.
Overview
The Civil Aviation Regulations 1998, specifically Part 39 - 105, was enacted to establish and maintain safety standards in civil aviation across Australia. This legislation was introduced to address the need for comprehensive regulations to ensure the safety and airworthiness of aircraft, thereby protecting passengers, crew, and the general public. The Civil Aviation Safety Authority, which operates under the authority of the Commonwealth of Australia, is the body responsible for enacting and enforcing these regulations. One such regulation, AD/BEECH 65/54 Amendment 2, targets the aft and nose hinged baggage door latching mechanisms of the Beechcraft 65 and 70 (Queen Air) series aeroplanes, aiming to enhance the safety of these aircraft by ensuring the baggage door latch mechanisms function correctly, taking into account potential variations in original installations.
This amendment is part of a broader policy objective to maintain and improve the safety of civil aviation by requiring specific actions to be taken within a defined timeframe. The regulation mandates that compliance must be achieved within 100 hours’ time in service after 31 July 1980, ensuring that the improvements to the baggage door latching mechanisms are implemented promptly and effectively.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, which pertains to the Civil Aviation Safety Authority's schedule of airworthiness directives, addresses the maintenance and operational standards of aircraft within Australian airspace. This particular directive, AD/BEECH 65/54 Amendment 2, applies to all Beechcraft 65 and 70 series aeroplanes, commonly known as Queen Air, with specific serial numbers as outlined in the legislation. This includes all models 65, A65, A65-8200, 65-80, 65-A80, 65-A80-8800, 65-B80, and 70. The directive mandates compliance with the action stipulated in Beechcraft Service Instruction No 1126 Revision 1, aimed at improving the functionality of the aft and nose hinged baggage door latching mechanism. Compliance is required within 100 hours of time in service after the directive's effective date of 31 July 1980. The directive is applicable to aircraft operating within the Australian jurisdiction, ensuring that these specific models adhere to the prescribed safety standards set by the Civil Aviation Safety Authority.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the safety directives for the Beechcraft 65 and 70 (Queen Air) series aeroplanes through Airworthiness Directive AD/BEECH 65/54 Amendment 2. This directive pertains to the aft and nose hinged baggage door latching mechanism, impacting all models of Queen Air 65, A65, and A65-8200 with specific serial numbers, as well as models 65-80, 65-A80, 65-A80-8800, 65-B80, and 70. The requirement under this directive mandates compliance with Beechcraft Service Information No 1126 Revision 1. This action must be completed within 100 hours of the aircraft’s time in service after 31 July 1980. The directive aims to enhance the effectiveness of the bellcrank stop for the baggage door latching mechanism, considering potential dimensional variations in original installations.
The obligations imposed by this directive are specific to the aircraft models and serial numbers mentioned. Operators of these aircraft must ensure that the modifications outlined in Beechcraft Service Information No 1126 Revision 1 are carried out by a licensed aircraft maintenance engineer or a similarly qualified individual. This requirement ensures that the safety modifications are implemented correctly and in accordance with the standards set forth by Beechcraft. The directive specifies a compliance timeline, mandating that the required actions be completed within 100 hours of the aircraft's service time post-31 July 1980, ensuring that the safety enhancements are implemented in a timely manner.
Failure to comply with the requirements outlined in AD/BEECH 65/54 Amendment 2 may result in significant consequences. The Civil Aviation Safety Authority (CASA) enforces these regulations, and non-compliance can lead to enforcement actions. These actions may include fines, operational restrictions, or other regulatory measures to ensure that the safety directives are adhered to. The potential penalties for not adhering to these safety directives can be severe, reflecting the importance of maintaining aircraft safety standards as stipulated by the Civil Aviation Regulations 1998. The directive underscores the critical nature of these safety measures, as failure to comply can compromise the integrity and safety of the aircraft in operation.