COMMONWEALTH OF AUSTRALIA (Civil Aviation 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 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.
Pilatus Britten Norman BN-2 Series Aeroplanes
AD/BN-2/73 Emergency Exit Window 13/2001 DM
Applicability: All Model BN-2 Series aircraft.
Requirement: Inspect in accordance with B-N Group Service Bulletin SB 277.
Note: UK CAA AD 001-08-2001 refers.
Compliance: Within 10 flight hours after the effective date of this Directive, unless already accomplished.
This Airworthiness Directive becomes effective on 7 November 2001.
Background: A report was received from the UK Air Accidents Investigation Board of an emergency exit window that could not be fully opened due to required sealant incorrectly applied.
David Alan Villiers
Delegate of the Civil Aviation Safety Authority 31 October 2001
The above AD is notified in the Commonwealth of Australia Gazette on 7 November 2001.
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Overview
The Civil Aviation Regulations 1998, specifically under Part 39, include Airworthiness Directives that are critical for ensuring the safety of aircraft and aeronautical products. These regulations were enacted to address the need for stringent oversight and safety measures within the civil aviation sector. The Civil Aviation Safety Authority (CASA) has the authority to issue such directives to correct any unsafe conditions identified in aircraft operations. The Airworthiness Directive AD/BN-2/73, issued on 31 October 2001, is an example of such measures, requiring inspections on the Pilatus Britten Norman BN-2 Series aeroplanes to address an issue with the emergency exit window, as identified in a report from the UK Air Accidents Investigation Board. This directive aims to rectify the unsafe condition where the emergency exit window could not be fully opened due to incorrect application of sealant, ensuring compliance within 10 flight hours from the effective date of the directive.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, issued by the Civil Aviation Safety Authority (CASA), applies to all aircraft and aeronautical products within Australia, ensuring adherence to safety standards mandated by the Commonwealth. This particular Airworthiness Directive (AD/BN-2/73) targets all Pilatus Britten Norman BN-2 Series aircraft, mandating an inspection of the emergency exit window in line with B-N Group Service Bulletin SB 277 to address an unsafe condition identified in a UK CAA AD. The directive requires the specified inspection to be completed within 10 flight hours after the effective date of the directive, which is 7 November 2001. This AD is a regulatory measure issued under subregulation 39.1 (1) of the Civil Aviation Regulations 1998, and it becomes enforceable upon its notification in the Commonwealth of Australia Gazette on the same effective date. The directive does not specify any exclusions or exemptions but mandates strict compliance to ensure air safety.
Key Provisions
The Civil Aviation Regulations 1998, under Part 39 - 105, specifically mandate the creation and dissemination of Airworthiness Directives (ADs) by the Civil Aviation Safety Authority (CASA). These directives, such as AD/BN-2/73, are issued to address safety concerns identified with certain aircraft models (s. 39.1(1)). In this case, the AD concerns all Model BN-2 Series aircraft and mandates a specific inspection procedure (s. 105). The requirement outlined in the directive is that an inspection must be conducted in accordance with B-N Group Service Bulletin SB 277 (s. 105). This inspection must be completed within 10 flight hours after the directive's effective date of 7 November 2001, unless it has already been performed (s. 105). The directive references a UK Civil Aviation Authority AD and explains the necessity for the inspection due to a reported issue with the emergency exit window that could not be fully opened due to incorrect application of sealant (s. 105).
The AD imposes specific obligations on the owners and operators of BN-2 Series aircraft. These obligations include ensuring that the aircraft are inspected according to the detailed instructions provided in B-N Group Service Bulletin SB 277. Operators must adhere strictly to the compliance timeframe, which requires the inspection to be completed within 10 flight hours from the effective date of the AD, unless the inspection has already been carried out (s. 105). Failure to comply with these requirements may result in the aircraft being deemed unsafe for operation until the necessary actions are taken.
Violations of the requirements set out in an AD can result in severe consequences. Specifically, the Civil Aviation Regulations 1998 include provisions for both civil and criminal penalties for non-compliance. Civil penalties can include fines, while criminal penalties may include imprisonment, reflecting the serious nature of ensuring aircraft airworthiness and safety. The exact penalties are not specified in the AD itself but would be determined under the broader regulatory framework of the Civil Aviation Act 1988 and associated regulations. The AD serves as a formal directive, and non-compliance can lead to enforcement actions by CASA, potentially culminating in legal proceedings and significant financial and reputational repercussions for the offending parties.