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 65/55
Amdt 1
Nose Baggage Compartment Door 3/89
Applicability: All models Queen Air 65, A65 and A65-8200 with S/Nos. L-1, L-2, L-6, LF-7, LF-8 and LC-1 to LC-335.
All models 65-80, 65-A80, 65-A80-8800 and 65-B80 with S/Nos. LD-1 to LD-511. All model 70 with S/Nos LB-1 through LB-35.
Requirement: Action in accordance with Beechcraft SI No 1181 Rev 1. Compliance: Within 300 hours’ time in service after 31 August 1981.
Background: Fatal accidents have occurred overseas caused by opening of the nose baggage locker door during takeoff. Amendment 1 consolidates Queen Air series 65 and 70 aircraft and references Rev 1 of the applicable Service Instruction.
Overview
The Civil Aviation Regulations 1998, amended through legislative instrument F2006B04151, was enacted to address critical safety issues in civil aviation, ensuring the safety of aircraft operations in Australia. This legislation, administered by the Civil Aviation Safety Authority, was introduced to rectify specific safety concerns identified in the operation of Beechcraft 65 and 70 (Queen Air) series aeroplanes. The underlying problem it aimed to address was the occurrence of fatal accidents overseas, which were attributed to the opening of the nose baggage compartment door during takeoff. The policy objective is to enhance the airworthiness and safety of these aircraft by mandating specific actions in compliance with Beechcraft Service Instruction No 1181 Revision 1, with a requirement for compliance within 300 hours of time in service after 31 August 1981.
This legislative amendment was made to mitigate the risk associated with the identified issue, ensuring that all applicable models and serial numbers of the Queen Air series adhere to the specified safety directives. By doing so, the Civil Aviation Safety Authority aims to prevent similar accidents from occurring in Australian airspace, thereby protecting the lives of passengers and crew, and maintaining the highest standards of aviation safety.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, under the authority of the Civil Aviation Safety Authority, mandates airworthiness directives for certain aircraft models. This particular directive, AD/BEECH 65/55 Amendment 1, pertains to the nose baggage compartment door of Beechcraft 65 and 70 (Queen Air) series aeroplanes. The directive applies to all models of Queen Air 65, including A65, A65-8200, 65-80, 65-A80, 65-A80-8800, 65-B80, and 70, identified by their specific serial numbers. The requirement necessitates compliance with Beechcraft Service Instruction No 1181 Revision 1, with a compliance deadline of 300 hours’ time in service after 31 August 1981. This directive aims to address safety concerns, particularly the risk of fatal accidents during takeoff due to the opening of the nose baggage locker door, as evidenced by overseas incidents. The regulation underscores the necessity for these aircraft to meet specified safety standards to ensure operational safety and compliance with civil aviation regulations.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the airworthiness directives for Beechcraft 65 and 70 (Queen Air) Series Aeroplanes. The relevant Airworthiness Directive (AD) in this case is AD/BEECH 65/55 Amendment 1, which pertains to the nose baggage compartment door (3/89). This AD applies to all models of Queen Air 65, A65, and A65-8200 with specific serial numbers (L-1 to L-2, L-6, LF-7, LF-8, LC-1 to LC-335) and models 65-80, 65-A80, 65-A80-8800, and 65-B80 with serial numbers LD-1 to LD-511. Additionally, it applies to all model 70 with serial numbers LB-1 through LB-35.
The directive mandates that operators of these aircraft must take corrective action as specified in Beechcraft Service Instruction (SI) No 1181 Revision 1. Compliance with this AD is required within 300 hours of the aircraft's time in service following 31 August 1981. This directive was issued in response to fatal accidents that occurred overseas, where the nose baggage locker door opened during takeoff, highlighting the critical need for this safety measure.
Operators of the affected aircraft must adhere to the requirements set forth in the Beechcraft SI No 1181 Rev 1 to ensure the nose baggage compartment door is secured properly. This includes inspecting, repairing, or replacing the door and associated hardware as necessary to prevent it from opening unintentionally during flight. Failure to comply with this directive could compromise the safety of the aircraft and its occupants, leading to severe consequences, including potential accidents.
Failure to comply with the AD/BEECH 65/55 Amendment 1 could result in significant legal and safety repercussions. The Civil Aviation Safety Authority (CASA) may impose penalties, including fines and other civil or criminal sanctions, for non-compliance with airworthiness directives. The exact penalties are determined by CASA but can be substantial, reflecting the importance of adhering to these safety requirements. It is imperative that operators ensure their aircraft meet these standards to avoid any legal or safety issues.