COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Airtractor 600 Series Aeroplanes
AIRWORTHINESS DIRECTIVE
For the reasons set out in the background section, the CASA delegate whose signature appears below issues the following Airworthiness Directive (AD) under subregulation 39.1 (1) of CAR 1998. The AD requires that the action set out in the requirement section (being action that the delegate considers necessary to correct the unsafe condition) be taken in relation to the aircraft or aeronautical product mentioned in the applicability section: (a) in the circumstances mentioned in the requirement section; and (b) in accordance with the instructions set out in the requirement section; and (c) at the time mentioned in the compliance section.
AD/AT 600/1 Airframe Life Limits 8/2000
Applicability: All models.
Requirement: Retire from service the airframe components listed in the Retirement Schedule below.
RETIREMENT SCHEDULE |
Component | Part No. | Retirement Life (Flight Hours) |
L/H Lower Spar Cap in Wing | 20603-1 | 6500 |
R/H Lower Spar Cap in Wing | 20603-2 | 6500 |
Wing Attach Block on Lower Cap | 20602-1 | 6500 |
Wing Attach Block on Lower Cap | 20602-2 | 6500 |
Plate Assy. – Fin Front Spar Attach | 30511-1 | 4000 |
Spar Assy. – Fin Rear | 30505-1 | 4000 |
Spring - Main Landing Gear Leg (including the forward and aft main gear clamp block bolts and the inboard main gear large bolt). | 40086-4 | 3000 hours or 8000 landings, whichever occurs first |
Spring – Tail Landing Gear Leg | 40092-4 | 3000 hours or 8000 landings, whichever occurs first |
Where the total number of landings during a period of service has not been recorded, three landings per one hour time in service must be assumed.
Compliance: Retire prior to exceeding the applicable time in service listed in the Retirement Schedule.
Note: The Type Certificate Data Sheet states that the lives are listed in the Maintenance Manual; however they are in fact listed in the Owners Manual.
This Airworthiness Directive becomes effective on 10 August 2000.
COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Background: This Directive has been issued to formally promulgate the airframe component life limitations determined by the manufacturer.
Neville James Probert
Delegate of the Civil Aviation Safety Authority 27 June 2000
The above AD is notified in the Commonwealth of Australia Gazette on 12 July 2000.
Overview
The Civil Aviation Regulations 1998, as amended, were enacted to ensure the safety of civil aviation in Australia. The regulations are administered by the Civil Aviation Safety Authority (CASA), which is tasked with maintaining and improving the safety standards in the aviation industry. A specific problem or gap addressed by the regulations includes the need for detailed airworthiness directives to ensure that aircraft meet safety standards throughout their operational life. The Civil Aviation Regulations 1998 provide a framework for the implementation of such directives. The policy objective behind these regulations is to safeguard the public by ensuring that aircraft are maintained and operated in a manner that minimises risks to safety.
Scope and Application
The Civil Aviation Regulations 1998, specifically under PART 39 - 105, encompasses the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, which applies to various aircraft and aeronautical products, including Airtractor 600 Series Aeroplanes. This particular Airworthiness Directive (AD) pertains to the mandatory retirement of specific airframe components to ensure continued airworthiness and safety of these aircraft. The AD applies to all models of the Airtractor 600 Series and mandates the retirement of certain components once they have reached specified flight hours or landings. The directive applies to all owners and operators of Airtractor 600 Series Aeroplanes and is enforceable under the jurisdiction of the Commonwealth of Australia. Compliance with this directive is necessary to mitigate the risk of unsafe conditions, and failure to adhere to the retirement schedules could result in the grounding of the affected aircraft. This Airworthiness Directive is effective from 10 August 2000 and was issued under the authority of the CASA delegate, Neville James Probert, on 27 June 2000.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandate the issuance of Airworthiness Directives (AD) by the Civil Aviation Safety Authority (CASA) to ensure the safety of aircraft operations. Section 39.1 (1) of the CAR 1998 empowers the CASA delegate to issue such directives when necessary to correct unsafe conditions. In this instance, AD/AT 600/1 pertains to the Airtractor 600 Series aeroplanes, requiring the retirement of specific airframe components once they reach their designated life limits (section 105).
The applicability of AD/AT 600/1 extends to all models of the Airtractor 600 Series aeroplanes. The directive mandates that certain components be retired from service once they reach the specified flight hours or landings, as detailed in the Retirement Schedule (section 105). For example, the L/H Lower Spar Cap in Wing and the R/H Lower Spar Cap in Wing must be retired after 6500 flight hours, while the Spring - Main Landing Gear Leg must be retired after 30,000 flight hours or 8000 landings, whichever comes first. The Compliance section further specifies that these components must be retired prior to exceeding the applicable service time listed in the Retirement Schedule.
The obligations imposed by AD/AT 600/1 are stringent and require operators of Airtractor 600 Series aeroplanes to adhere to the Retirement Schedule strictly. Operators must ensure that the specified components are inspected and retired from service as per the requirements, with particular attention to the life limits detailed. Failure to comply with these requirements may result in the aircraft being deemed non-airworthy, potentially leading to enforcement actions.
Breaching the provisions of AD/AT 600/1 could lead to significant consequences. Under section 39.1 (2) of CAR 1998, non-compliance with an Airworthiness Directive is an offence, potentially resulting in civil penalties for individuals and criminal penalties for corporations. The maximum penalty for a corporation found in breach can include substantial fines and, in severe cases, imprisonment of the responsible officers. The directive thus places a clear responsibility on aircraft operators to ensure adherence to the specified life limits to maintain airworthiness and avoid legal repercussions.