COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 107 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Seats and Berths
AD/SEATS/1 Pilots Seat - Reinforcement 1/84
Applicability: A.M.I. Pilot Seat Model 716-1, -2, -11, -12, -21 and -22 and Model 865-1 to -9 and
-11.
Requirement: Reinforce pilot seat frame assembly P/N 865J10005-1 by installation of A.M.I. Industries, Inc. seat frame brace kit P/N 865K9000-1 I.A.W. AMI Industries Inc., service Bulletin No 25-10-865-01, dated January 31, 1983.
Note: FAA AD 83-21-06 refers.
Compliance: Unless previously accomplished, before 30 April 1984.
Background: Failure of the pilots seat during a survivable emergency landing contributed to occupant injury. Subsequent T.S.O. tests verified failure of the seat frame at loads below the 9G. forward requirement. AD/BEECH 18/23 and AD/BEECH 90/72 address specific aircraft installations.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of Australia, are a comprehensive set of rules designed to ensure the safety and efficiency of civil aviation within Australia. This legislation plays a crucial role in addressing issues related to airworthiness, including the reinforcement of specific components such as pilot seats, as outlined in Part 39, which pertains to the Civil Aviation Safety Authority's schedule of airworthiness directives. One such directive, AD/SEATS/1, specifically mandates the reinforcement of A.M.I. Pilot Seat models to prevent failures during survivable emergency landings that could cause occupant injury, thereby ensuring compliance with safety standards set forth by the Civil Aviation Safety Authority.
The policy objective behind the Civil Aviation Regulations 1998, particularly in relation to airworthiness directives like AD/SEATS/1, is to maintain the highest possible safety standards for all civil aviation activities. This is achieved by enforcing mandatory safety measures and ensuring that aircraft components, such as pilot seats, meet stringent criteria to prevent accidents and mitigate risks during emergency situations. The directive to reinforce A.M.I. Pilot Seats exemplifies the regulatory framework's focus on proactive safety measures to protect occupants in the event of an emergency landing.
Scope and Application
The Civil Aviation Regulations 1998, specifically PART 39 - 107 under the Civil Aviation Safety Authority, apply to the reinforcement of pilot seats in certain aircraft models to ensure compliance with airworthiness standards. This legislative instrument targets A.M.I. Pilot Seat Models 716-1, -2, -11, -12, -21, -22, and 865-1 to -9 and -11, mandating that the pilot seat frame assembly P/N 865J10005-1 be reinforced with the installation of the A.M.I. Industries, Inc. seat frame brace kit P/N 865K9000-1 as per AMI Industries Inc., service bulletin No 25-10-865-01, dated January 31, 1983. This directive is in response to failures observed during survivable emergency landings that led to occupant injuries, with tests confirming that the seat frames did not meet the 9G forward requirement. The regulation necessitates compliance before 30 April 1984 unless the reinforcement has already been accomplished. The regulation is applicable nationally within the Commonwealth of Australia, overseen by the Civil Aviation Safety Authority.
Key Provisions
The Civil Aviation Regulations 1998, particularly Part 39 - 107, detail several key provisions concerning the airworthiness directives, including those related to the reinforcement of pilot seats. Specifically, Airworthiness Directive (AD) AD/SEATS/1 pertains to the reinforcement of pilot seat frames for certain A.M.I. Pilot Seat models (Section 1/84). This directive applies to A.M.I. Pilot Seat Models 716-1, -2, -11, -12, -21, -22, and Model 865-1 to -9 and -11. The requirement is to reinforce the pilot seat frame assembly by installing the A.M.I. Industries, Inc. seat frame brace kit P/N 865K9000-1, in accordance with A.M.I. Industries, Inc. service bulletin No 25-10-865-01 dated January 31, 1983. This action follows the Federal Aviation Administration (FAA) AD 83-21-06.
The obligations imposed by AD/SEATS/1 are clear and time-bound: operators must ensure that the specified reinforcement is completed before 30 April 1984, unless it has already been accomplished. This directive was issued due to the failure of the pilot's seat during a survivable emergency landing, which led to occupant injury. Subsequent tests conducted by the Technical Standard Order (T.S.O.) verified that the seat frame failed at loads below the required 9G forward load. The directive is further supported by other airworthiness directives such as AD/BEECH 18/23 and AD/BEECH 90/72, which address specific aircraft installations.
Failure to comply with the AD/SEATS/1 could result in significant civil and criminal consequences. The Civil Aviation Safety Authority (CASA) has the authority to enforce these regulations, and non-compliance may lead to penalties as stipulated by the Civil Aviation Act 1988. While the specific penalties are not detailed within the AD itself, general provisions under the Act allow for fines and potential imprisonment for individuals or corporations found in breach of safety regulations. The exact penalties depend on the severity of the breach and the discretion of the court. Ensuring compliance with these airworthiness directives is therefore critical to maintaining the safety standards required in civil aviation.