COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Beechcraft 60 (Duke) Series Aeroplanes
AD/BEECH 60/5 Heated Stall Warning Switch 2/70
Applicability: Model 60 with S/Nos. P-3 to P-5, P-7 to P-35, P-37 to P-44, P-46 to P-53, P-55 to P- 60, P-62 to P-65, P-67, P-68, P-70 to P-72, P-75, P-77 and P-78.
Requirement: Action in accordance with Beechcraft SI No. 0271-355. Compliance: Forthwith.
Overview
The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the safety of aircraft operations within Australia by mandating compliance with airworthiness directives. One such directive, AD/BEECH 60/5, pertains to the heated stall warning switch in Beechcraft 60 (Duke) Series aeroplanes. This legislation was introduced to ensure that specific models of the Duke series adhere to necessary safety standards, thus mitigating the risk of accidents due to inadequate stall warning systems. The directive applies to a range of serial numbers within the Duke series and requires immediate compliance with the specified instructions, as outlined in Beechcraft Service Information No. 0271-355. The policy objective is to maintain high safety standards in civil aviation, protecting both passengers and crew by ensuring aircraft meet the required safety benchmarks. The Civil Aviation Safety Authority, under the authority of the Australian Government, enacts these regulations to uphold the integrity and safety of the nation's airspace.
Scope and Application
The Civil Aviation Safety Authority (CASA) under the Civil Aviation Regulations 1998, specifically in Part 39, has issued an Airworthiness Directive (AD) that applies to Beechcraft 60 (Duke) Series Aeroplanes. The directive, identified as AD/BEECH 60/5, pertains to a specific requirement for the heated stall warning switch on particular models of the Duke series. The directive applies to Model 60 aircraft with serial numbers ranging from P-3 to P-5, P-7 to P-35, P-37 to P-44, P-46 to P-53, P-55 to P-60, P-62 to P-65, P-67, P-68, P-70 to P-72, P-75, P-77, and P-78. The AD mandates that compliance with the directive must be achieved in accordance with Beechcraft Service Instruction No. 0271-355, with immediate effect. This directive forms part of the broader regulatory framework managed by CASA and ensures that specific safety concerns are addressed to maintain the airworthiness of the affected aircraft. The geographic and jurisdictional reach of this directive is nationwide within Australia, as CASA is the regulatory body under the Commonwealth of Australia. The directive does not specify any exclusions or exemptions, and compliance is mandatory for the listed serial numbers.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39 - 105, include specific Airworthiness Directives for various aircraft models, such as the Beechcraft 60 (Duke) series aeroplanes. The directive AD/BEECH 60/5 pertains to the installation and functionality of the heated stall warning switch (section 105). This directive applies to specific serial numbers of the Beechcraft 60 model, as listed in the applicability section. Operators of these aircraft are required to comply with the instructions outlined in Beechcraft Service Instruction No. 0271-355, which includes the necessary actions to ensure the heated stall warning switch is functioning correctly (section 2/70).
Under this regulation, the primary obligation for the aircraft operators is to ensure that the modifications or checks on the heated stall warning switch are performed without delay, as indicated by the term "forthwith" in the compliance requirement (section 2/70). This means that operators must address any issues with the stall warning switch promptly to maintain the airworthiness of the aircraft. It is imperative that these checks and modifications are conducted according to the specifications provided in the referenced Beechcraft Service Instruction.
Failure to comply with the directives stipulated in AD/BEECH 60/5 may result in serious consequences. Non-compliance with airworthiness directives is not only a breach of the Civil Aviation Regulations but can also lead to severe civil or criminal penalties. The Civil Aviation Safety Authority (CASA) has the authority to take enforcement actions, which may include fines or other penalties as outlined in the relevant sections of the Civil Aviation Act 1988. The exact nature and severity of the penalties depend on the degree of non-compliance and the risk posed to aviation safety. In extreme cases, CASA may also suspend or revoke an aircraft's certificate of airworthiness, which would effectively ground the aircraft until the required modifications are made.