COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 56TC (Turbo Baron) Series Aeroplanes
AD/BEECH 56/24 Nose Baggage Door Secondary Latch 8/82
Applicability: All model 56TC and A56TC with S/Nos. TG-2 to TG-94. Requirement: Action in accordance with Beechcraft SI No. 1195.
Compliance: Unless previously accomplished, within 100 hours’ time in service after 31 August 1982.
Background: Instances have been reported by the manufacturer of nose baggage doors becoming unsafe in flight.
Overview
The Civil Aviation Regulations 1998, specifically Part 39 - 105, contains Airworthiness Directives aimed at ensuring the safety of aircraft. One such directive, AD/BEECH 56/24, pertains to the nose baggage door secondary latch of Beechcraft 56TC (Turbo Baron) Series Aeroplanes with serial numbers TG-2 to TG-94. This directive was introduced to address the reported instances of nose baggage doors becoming unsafe during flight. The Civil Aviation Safety Authority, under the authority of the Australian Parliament, established this directive to ensure the continued airworthiness of these aircraft by requiring compliance with Beechcraft Service Instruction No. 1195. The primary objective is to enhance flight safety by ensuring the nose baggage door latch remains secure, thus preventing potential in-flight hazards.
The directive mandates that the specified Beechcraft 56TC aeroplanes must comply with the specified service instruction within 100 hours of time in service after 31 August 1982, unless such compliance has already been achieved. This requirement is essential for maintaining the integrity of the aircraft's structure and ensuring that passengers and crew remain safe during flights. The regulation underscores the importance of adhering to manufacturer guidelines and safety instructions to prevent incidents that could compromise the safety of air travel.
Scope and Application
The Civil Aviation Safety Authority (CASA) has issued Airworthiness Directives (ADs) under the Civil Aviation Regulations 1998, which pertain specifically to the maintenance and safety of aircraft. One such directive, AD/BEECH 56/24, is applicable to all model 56TC and A56TC Beechcraft 56 Turbo Baron series aeroplanes with serial numbers ranging from TG-2 to TG-94. This directive mandates action in accordance with Beechcraft Service Instruction No. 1195, specifically addressing the nose baggage door secondary latch to prevent instances of the nose baggage door becoming unsafe in flight. Compliance with this directive is required unless the specified action has already been completed, and must be undertaken within 100 hours’ time in service after 31 August 1982. The AD applies across the Commonwealth of Australia, overseen by CASA, ensuring that all relevant aircraft within the specified serial number range adhere to the safety measures stipulated by this directive.
Key Provisions
The primary sections of the AD/BEECH 56/24 concerning the nose baggage door secondary latch of the Beechcraft 56TC (Turbo Baron) Series Aeroplanes include section 39-105, which outlines the applicability and requirements (39-105.1), and section 39-105.2, which specifies the compliance timeframe. According to section 39-105.1, the directive applies to all model 56TC and A56TC aeroplanes with serial numbers ranging from TG-2 to TG-94. Section 39-105.2 mandates that the corrective action specified in Beechcraft Service Instruction No. 1195 must be completed unless it has already been accomplished. This action must be taken within 100 hours of time in service after 31 August 1982.
The obligations imposed by the Civil Aviation Regulations 1998 on the operators of the affected Beechcraft 56TC and A56TC aeroplanes are to ensure that the nose baggage door secondary latch is addressed as per the specified directive. Operators must comply with the action outlined in Beechcraft SI No. 1195, which is intended to mitigate the risk of the nose baggage door becoming unsafe in flight. The regulation underscores the necessity of adhering to the manufacturer’s instructions to maintain the airworthiness of the aircraft.
Failure to comply with the directives outlined in AD/BEECH 56/24 may result in serious consequences. Section 105.1 of the Civil Aviation Regulations 1998 states that operating an aeroplane in contravention of an airworthiness directive is an offence. Such breaches may lead to enforcement actions by the Civil Aviation Safety Authority (CASA), which can include fines and other penalties. The specific penalties are not detailed in the provided excerpt, but they could include significant financial penalties and potential grounding of the aircraft until compliance is verified. The severity of the consequences underscores the importance of timely adherence to the directive to ensure the continued safety of the aircraft and its passengers.