AD/BEECH 56/16 - Wing Strobe Lights

Overview

The Civil Aviation Regulations 1998 (Cth) were enacted by the Australian Parliament to establish a comprehensive regulatory framework for civil aviation, ensuring the safety and efficiency of air travel. Part 39, specifically, focuses on airworthiness directives which are critical in maintaining the safety standards of aircraft. The enactment of this legislation was intended to address gaps in the regulation of aviation safety, particularly in ensuring that aircraft remain in a condition that is safe for operation. One such directive, AD/BEECH 56/16, pertains to the Beechcraft 56TC (Turbo Baron) Series aeroplanes, specifically addressing the installation and compliance requirements of wing strobe lights. The policy objective of these regulations is to ensure that all aircraft maintain a standard of airworthiness that protects the safety of passengers and crew, as well as the general public.

Scope and Application

The Civil Aviation Regulations 1998, as amended, under Part 39 - 105, pertains to the Civil Aviation Safety Authority’s Schedule of Airworthiness Directives, specifically addressing the Beechcraft 56TC (Turbo Baron) Series Aeroplanes. This legislation applies to all models A56TC, serial numbers TG-84 through TG-94, that are equipped with either the Hoskins P/N 30-0187-21 or Grimes P/N 30-0669-1 wing strobe lights. The regulations are designed to ensure that these specific aircraft models meet certain safety standards and operational requirements as stipulated by the Civil Aviation Safety Authority. The directive mandates compliance with Beechcraft Service Instruction No. 0800-362, with an implementation timeline of 100 hours of time in service following 29 October 1976. This requirement ensures that the specified aircraft meet the necessary safety criteria within a defined operational period, thereby maintaining airworthiness and safety standards in accordance with Australian aviation laws.

Key Provisions

The Civil Aviation Regulations 1998, specifically under Part 39 - 105, detail the Civil Aviation Safety Authority's (CASA) Schedule of Airworthiness Directives for various aircraft types, including the Beechcraft 56TC (Turbo Baron) Series Aeroplanes. The directive AD/BEECH 56/16 focuses on the wing strobe lights of certain models within this series. The directive applies to all models A56TC with serial numbers ranging from TG-84 to TG-94 that are equipped with either Hoskins part number 30-0187-21 or Grimes part number 30-0669-1 wing strobe lights (section 10/76). The primary requirement outlined in AD/BEECH 56/16 is for operators to take specific action as per Beechcraft Service Instruction (SI) No. 0800-362. This directive mandates that the required action must be completed within 100 hours of time in service following the issue date of 29 October 1976. Operators of the affected aircraft must ensure that the specified wing strobe lights are addressed as per the instructions provided in the Beechcraft SI to maintain compliance with airworthiness standards. Operators and owners of the Beechcraft 56TC aeroplanes affected by AD/BEECH 56/16 are obligated to follow the action requirements strictly. This includes ensuring that the wing strobe lights are either replaced or repaired according to the specifications detailed in the Beechcraft SI No. 0800-362. Failure to comply with the directive within the stipulated timeframe may result in the aircraft being considered non-airworthy, which could lead to grounding and potential enforcement actions by CASA. Failure to comply with the requirements of AD/BEECH 56/16 can result in significant consequences. Non-compliance may lead to penalties under the Civil Aviation Act 1988, which can include substantial fines and legal action. The maximum penalties for such offences can be significant, reflecting the critical nature of maintaining airworthiness standards to ensure safety in aviation operations. Operators must therefore ensure prompt and thorough compliance to avoid any legal or financial repercussions.