COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
British Aerospace BAe 3100 (Jetstream) Series Aeroplanes
AD/JETSTREAM/44 MLG Wheel Nut 8/91
Applicability: Model HP137 MK1 aircraft, Jetstream Series 200, Series 3100, and Series 3200 aircraft with installed main landing gear types listed in BAe SB 32-A-JA-910140.
Requirement: Action in accordance with Mandatory BAe Alert SB 32-A-JA 910140.
Note: BAe (Dynamics) Ltd SB 32-46 refers.
Compliance: As specified in the Requirement Document.
Note: The Requirement Document compliance statement is applicable in its entirety to Australian registered aircraft.
Background: Instances of main wheel roller bearing break-up have been reported. This has caused the loss of a main landing gear wheel. Inspection revealed that the main wheel bearing outer race had passed over the axle nut and the wheel departed from the aircraft.
Overview
The Civil Aviation Regulations 1998, administered by the Civil Aviation Safety Authority (CASA), were enacted to ensure the safe operation of aircraft within Australian airspace. One specific legislative instrument under these regulations is the Airworthiness Directive AD/JETSTREAM/44, issued in 1991, which addresses a critical safety issue concerning British Aerospace BAe 3100 (Jetstream) series aeroplanes. The directive was introduced in response to reports of main wheel roller bearing failures that led to the loss of main landing gear wheels. The policy objective of this directive is to mandate inspections and corrective actions in accordance with British Aerospace's Service Bulletin SB 32-A-JA 910140 to prevent such occurrences and ensure the continued airworthiness of affected aircraft.
The AD/JETSTREAM/44 applies to Jetstream Series 200, Series 3100, and Series 3200 aircraft equipped with specific main landing gear types, as detailed in British Aerospace's Service Bulletin. The directive requires compliance with the specified requirements to address the identified safety issue, ensuring that Australian-registered aircraft meet the same safety standards as those mandated by British Aerospace. This proactive measure aims to mitigate the risk of catastrophic failure by enforcing stringent inspection and maintenance protocols.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, addresses the maintenance and operation of aircraft in Australia, with a focus on ensuring safety through the issuance of Airworthiness Directives (AD). The scope of the AD/JETSTREAM/44 pertains to British Aerospace BAe 3100 (Jetstream) Series Aeroplanes, including the HP137 MK1 aircraft, Jetstream Series 200, Series 3100, and Series 3200 aircraft that have installed main landing gear types specified in BAe SB 32-A-JA-910140. This regulation applies to all aircraft registered in Australia that fall within these categories, enforcing the requirement to comply with the Mandatory BAe Alert SB 32-A-JA 910140. Compliance entails adhering to the specifications outlined in the Requirement Document, which is fully applicable to Australian registered aircraft. The directive is grounded in safety concerns stemming from reported instances of main wheel roller bearing failures, leading to wheel loss due to the bearing outer race passing over the axle nut. The regulation does not extend to other aircraft types or landing gear configurations not explicitly mentioned in the referenced service bulletins.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39 - 105, establish a schedule of airworthiness directives for British Aerospace BAe 3100 (Jetstream) Series aeroplanes. The directive AD/JETSTREAM/44 pertains to the MLG (Main Landing Gear) wheel nut and is applicable to the HP137 MK1 aircraft, as well as the Jetstream Series 200, 3100, and 3200 aircraft with certain main landing gear types installed, as detailed in BAe SB 32-A-JA-910140 (section 1). This directive mandates that actions must be taken in accordance with the Mandatory BAe Alert SB 32-A-JA 910140 (section 2). For further reference, BAe (Dynamics) Ltd SB 32-46 is noted, although it does not form part of the directive's requirement (section 3). Compliance with these directives is crucial, and it must align with the specified Requirement Document, which applies in its entirety to Australian registered aircraft (section 4).
Under this regulation, the primary obligation for the parties governed by this directive is to ensure that they comply with the actions outlined in the Mandatory BAe Alert SB 32-A-JA 910140. This includes adhering to the inspection and maintenance procedures detailed in the Requirement Document to prevent issues such as the main wheel roller bearing break-up that has previously led to the loss of a main landing gear wheel. The compliance statement in the Requirement Document must be strictly followed, ensuring that any necessary repairs or replacements are carried out to maintain the airworthiness of the aircraft (section 5). Failure to comply with these directives could result in significant safety risks and potential grounding of the aircraft.
In terms of consequences for non-compliance, the Civil Aviation Regulations 1998 impose penalties for breaches. The specifics of these penalties are not detailed in the given text, but generally, breaches of airworthiness directives can lead to civil or criminal penalties. These may include fines, enforcement actions, or even criminal charges for those found negligent in ensuring compliance. The exact penalties can vary depending on the severity of the breach and the circumstances, but the overarching goal is to ensure the highest standards of safety are maintained in the aviation sector (section 6). It is imperative that all stakeholders, including aircraft operators and maintenance personnel, are fully aware of their obligations under these regulations to avoid any legal repercussions.