COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Bushby Mustang II Series Aeroplanes
AD/BUSHBY M2/1 Canopy Frame - Modification 2/85
Applicability: All Models.
Requirement: Reinforce the canopy framework at the aft corners and manufacture and install an aft retaining pin and bracket I.A.W. Mustang II Canopy Frame Revision Instruction dated 11.1.84.
Note: Copies of Bushby Mustang II, Canopy Frame Revision dated 11.1.84 may be obtained from D of A Regional Offices.
Compliance: Modify prior to 31 August 1985.
Background: As a result of a fatal accident in which the canopy detached in flight, canopy reinforcement and improved latching is warranted.
Overview
The Civil Aviation Regulations 1998, enacted by the Commonwealth of Australia, address the problem of aircraft safety by ensuring that all aircraft meet specific airworthiness standards. Part 39 - 105 of the regulations, which pertains to the Civil Aviation Safety Authority's schedule of airworthiness directives, focuses on the Bushby Mustang II Series Aeroplanes. Specifically, AD/BUSHBY M2/1 mandates the modification of the canopy frame, including reinforcement at the aft corners and the installation of a new aft retaining pin and bracket, as per the Mustang II Canopy Frame Revision Instruction dated 11 January 1984. This directive was introduced in response to a fatal accident where the canopy detached in flight, underscoring the need for enhanced canopy latching and structural integrity. Compliance with these airworthiness directives is mandatory and must be achieved before 31 August 1985 to ensure the safety of all Bushby Mustang II Series Aeroplanes in operation.
Scope and Application
The Civil Aviation Regulations 1998, as amended, under the authority of the Civil Aviation Act 1988, apply to all aircraft operating within Australian airspace. Specifically, Part 39 - 105 addresses Airworthiness Directives for various aircraft types, including the Bushby Mustang II Series Aeroplanes. This directive mandates the reinforcement of the canopy frame at the aft corners and the installation of an aft retaining pin and bracket, as per the Mustang II Canopy Frame Revision Instruction dated 11 January 1984. This modification is necessitated by a fatal accident where the canopy detached in flight, thereby warranting enhanced safety measures. The directive applies to all models of the Bushby Mustang II series, and compliance must be achieved prior to 31 August 1985. Detailed instructions and copies of the revision may be obtained from the Department of Aviation Regional Offices. This regulatory requirement is binding on all aircraft operators and owners of Bushby Mustang II series aeroplanes within the Commonwealth of Australia.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes a Schedule of Airworthiness Directives, one of which is AD/BUSHBY M2/1 concerning the Bushby Mustang II Series Aeroplanes. This directive (section 2) mandates the reinforcement of the canopy framework at the aft corners and the installation of an aft retaining pin and bracket. This requirement is in response to a fatal accident where the canopy detached in flight, hence the directive's emphasis on structural integrity and safety.
Under this legislation, the parties or entities governed by the AD/BUSHBY M2/1 directive must ensure that modifications are made to the specified aircraft models before the stipulated deadline of 31 August 1985. The modifications must adhere to the specifications outlined in the Mustang II Canopy Frame Revision Instruction dated 11.1.84, which includes detailed technical instructions and diagrams for the required changes. These modifications are crucial to prevent a recurrence of canopy detachment incidents.
Failure to comply with the requirements set forth in AD/BUSHBY M2/1 can result in severe consequences. The regulations do not explicitly detail the penalties for non-compliance in this specific context, but generally, non-compliance with Civil Aviation Regulations can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). These actions may include fines, suspension or revocation of airworthiness certificates, and potential criminal charges if the non-compliance leads to accidents or endangers safety. It is imperative that operators of the Bushby Mustang II Series Aeroplanes ensure strict adherence to these directives to avoid such repercussions.
In summary, AD/BUSHBY M2/1 mandates the reinforcement of the canopy framework and installation of specific safety components on Bushby Mustang II Series Aeroplanes to prevent canopy detachment. Operators must complete these modifications by 31 August 1985, following the Mustang II Canopy Frame Revision Instruction dated 11.1.84. Non-compliance can result in significant regulatory and legal penalties, underscoring the importance of adherence to these safety directives.