COMMONWEALTH OF AUSTRALIA (Civil Aviation Safety Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
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 CASR 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.
Pilatus Britten-Norman BN-2 Series Aeroplanes
AD/BN-2/80 Folding Passenger Seat Rear Frame 10/2003
Applicability: All BN2, BN2A, BN2B, BN2T, BN2T-4R, and BN2T-4S series Islander aircraft. Requirement: Inspect in accordance with B-N Group Limited Service Bulletin SB 286.
Compliance: Within 100 hours time in service or 100 landings after 2 October 2003, whichever occurs first. Thereafter at intervals not to exceed 100 hours time in service or 100 landings, whichever occurs first.
This Airworthiness Directive becomes effective on 2 October 2003.
Background: A report was received where, during boarding and loading of passengers onto the aircraft, the tubing on a passenger seat rear frame failed.
David Villiers
Delegate of the Civil Aviation Safety Authority 12 August 2003
The above AD is notified in the Commonwealth of Australia Gazette on 10 September 2003.
Overview
The Civil Aviation Safety Regulations 1998 were enacted to regulate the airworthiness of aircraft and aeronautical products within Australia, thereby ensuring the safety of air travel. The specific Airworthiness Directive (AD) addressed in this legislative instrument is AD/BN-2/80, which was issued on 10 October 2003 and applies to the Pilatus Britten-Norman BN-2 series Islander aircraft. The directive was introduced to address a safety issue identified with the folding passenger seat rear frame, which had reportedly failed during the boarding and loading of passengers, potentially leading to unsafe conditions. The policy objective of this AD, issued by the delegate of the Civil Aviation Safety Authority, is to mandate specific inspections and corrective actions to mitigate the risk of such failures, thereby maintaining the airworthiness of the affected aircraft.
Scope and Application
The Civil Aviation Safety Regulations 1998, specifically Part 39 - 105 Airworthiness Directives, apply to all BN2, BN2A, BN2B, BN2T, BN2T-4R, and BN2T-4S series Islander aircraft, mandating specific maintenance and safety actions to ensure airworthiness. This regulation is issued by the Civil Aviation Safety Authority (CASA) and applies nationally, as CASA is the federal authority overseeing civil aviation safety in Australia. The directive requires an inspection of the folding passenger seat rear frame in accordance with B-N Group Limited Service Bulletin SB 286 to address a previously reported failure of the tubing during passenger boarding. The inspection must be completed within 100 hours of time in service or 100 landings after the directive's effective date of 2 October 2003, and then at intervals not exceeding 100 hours of time in service or 100 landings thereafter. This ensures ongoing safety and compliance with national aviation standards.
Key Provisions
The Civil Aviation Safety Regulations 1998, under Part 39, specifically Section 105, establish an Airworthiness Directive for the Pilatus Britten-Norman BN-2 series aeroplanes. This directive, AD/BN-2/80, mandates specific actions to be taken to ensure the safety of the aircraft. The AD applies to all BN2, BN2A, BN2B, BN2T, BN2T-4R, and BN2T-4S series Islander aircraft. The requirement outlined in the directive is to inspect the folding passenger seat rear frame in accordance with B-N Group Limited Service Bulletin SB 286. This inspection is critical because of the reported incident where the tubing on a passenger seat rear frame failed during boarding and loading of passengers.
Operators and owners of the specified aircraft are obligated to ensure that these inspections are carried out within 100 hours of time in service or 100 landings, whichever comes first, after the directive's effective date of 2 October 2003. Following this initial inspection, further inspections must occur at intervals not exceeding 100 hours of time in service or 100 landings, whichever comes first. This continuous inspection requirement underscores the importance of maintaining the structural integrity of the passenger seat rear frames to prevent potential failures and ensure passenger safety.
Failure to comply with the Airworthiness Directive can lead to serious consequences. The Civil Aviation Safety Authority (CASA) enforces strict measures to ensure adherence to these regulations. Non-compliance with the AD may result in severe civil or criminal penalties. While specific penalties are not detailed in the AD itself, CASA has the authority to impose fines and other sanctions under the Civil Aviation Act 1988 and related regulations. The potential penalties for not adhering to these safety directives can include significant financial penalties and, in severe cases, criminal charges that may lead to imprisonment. Ensuring compliance is therefore crucial for the safety of passengers and the continued airworthiness of the aircraft.