COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
British Aerospace BAe 125 Series Aeroplanes
AD/HS 125/92 Nose Gear Pivot Pin 7/88 DM
Applicability: All models.
Requirement: Action in accordance with BAe-125 SB 32-217.
Note: CAA AD 008-02-88 refers.
Compliance: For components with more than 4000 landings, prior to 31 August 1988. For components with less than 4000 landings, before exceeding 4000 landings.
Background: Recent analysis by the manufacturer has resulted in a requirement to crack detect pivot pins fitted to all nose leg assemblies which have achieved or exceeded 4000 landings.
Overview
The Civil Aviation Regulations 1998, enacted by the Parliament of the Commonwealth of Australia, were introduced to regulate and ensure the safety of civil aviation within Australia. One particular legislative instrument within this regulation, F2006B10535, addresses a specific safety issue concerning British Aerospace BAe 125 Series Aeroplanes. This legislative instrument, issued by the Civil Aviation Safety Authority, aims to mitigate risks associated with the nose gear pivot pin of these aircraft. It mandates crack detection for pivot pins on nose leg assemblies that have reached or surpassed 4000 landings, aiming to maintain the integrity and safety of the aircraft's landing gear system. This directive aligns with the overarching policy objective of the Civil Aviation Regulations to safeguard air travel and prevent accidents related to aircraft maintenance and operational standards.
The specific directive AD/HS 125/92, referenced in the legislative instrument, outlines the necessary actions in accordance with British Aerospace Service Bulletin 32-217. The requirement is to perform the specified action for components that have completed more than 4000 landings by 31 August 1988 or before reaching 4000 landings if inspected thereafter. This proactive measure is a response to recent manufacturer analysis highlighting the need for enhanced safety checks on these critical components. The regulation also cross-references CAA AD 008-02-88, reinforcing the commitment to comprehensive aircraft safety standards.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 concerning the Civil Aviation Safety Authority Schedule of Airworthiness Directives for British Aerospace BAe 125 Series Aeroplanes, applies to all models of the BAe 125 aeroplanes. This legislation mandates action in accordance with BAe-125 Service Bulletin 32-217, referencing CAA AD 008-02-88. The requirement necessitates crack detection of the nose gear pivot pins on all nose leg assemblies that have either achieved or are expected to achieve 4000 landings. For components that have already exceeded 4000 landings as of 31 August 1988, compliance is required immediately. For those with less than 4000 landings at that date, compliance must be met before the landing count reaches 4000. This regulation is issued under the authority of the Commonwealth of Australia and applies nationally, ensuring safety and compliance across the entire aviation industry within Australia. The Act does not specify exclusions, exemptions, or thresholds beyond those outlined for the landing count, and any further details or extensions are managed through subordinate instruments as necessary.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates the compliance of airworthiness directives for certain aircraft models, including the British Aerospace BAe 125 Series Aeroplanes. One such directive, AD/HS 125/92, pertains to the nose gear pivot pin (7/88 DM) and requires actions in accordance with BAe-125 SB 32-217. The directive references CAA AD 008-02-88 for further details. The applicability of this directive covers all models of the BAe 125 Series. The requirement is to conduct a crack detection on the pivot pins fitted to all nose gear assemblies. For components with more than 4000 landings, this compliance must be achieved before 31 August 1988. For components with less than 4000 landings, the compliance must be achieved before the number of landings exceeds 4000.
The obligations imposed by this directive on the parties or entities it governs are straightforward. Aircraft operators must ensure that the nose gear pivot pins of their BAe 125 Series aeroplanes are inspected and tested for cracks as stipulated. This inspection and testing must adhere to the manufacturer’s service bulletin, BAe-125 SB 32-217, and must be completed within the specified timelines. For aircraft with more than 4000 landings, this inspection and testing must be completed before the deadline of 31 August 1988. For aircraft with fewer than 4000 landings, compliance must be achieved before the aircraft accumulates 4000 landings. Failure to comply with these obligations can lead to significant consequences.
The Civil Aviation Regulations 1998 also outline the potential offences, penalties, and consequences for non-compliance with the airworthiness directives. Breaching the requirements of AD/HS 125/92 can result in civil penalties, including fines and other enforcement actions by the Civil Aviation Safety Authority (CASA). The maximum penalties for non-compliance with these regulations can include substantial fines and, in severe cases, the grounding of the aircraft until the required inspections and repairs are completed. Additionally, persistent or egregious non-compliance can lead to criminal charges against the responsible parties, resulting in more severe penalties including imprisonment. The specific penalties are detailed in the Civil Aviation Act 1988 and the Civil Aviation Regulations 1998, which provide the legal framework for enforcement actions.