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.
Israel Aircraft Industries 1125 (Astra) Series Aeroplanes
AD/IAI-A/17 Main Landing Gear Ground Contact Switches
12/2003
Applicability: Gulfstream Aerospace LP (GALP) Model 1125 Astra, Astra SPX and G100 aeroplanes with serial numbers 004 through 127 inclusive.
Requirement: Unless already accomplished, adjust the main landing gear ground contact switches in accordance with the revised procedures in the G100 Maintenance Manual and GALP Service Bulletin 1125-32A-233 Revision 1 dated 1 August 2003.
Note 1: The G100 Maintenance Manual procedures for adjusting the main landing gear ground contact switch were revised by Temporary Revision (TR) 32-8 dated 12 April 2001. Maintenance Manual Revision 4, dated 1 August 2001, subsequently incorporated the revised procedures and removed TR 32-8.
Note 2: Israel CAA AD 32-03-08-05 refers.
Compliance: Within 200 hours time in service after the effective date of this Directive This Airworthiness Directive becomes effective on 27 November 2003.
Background: The Israel Civil Aviation Administration has received reports of in-flight deployment of the ground airbrakes following lowering of the landing gear. This Directive requires the adjustment of the main landing gear ground contact switch to prevent false ‘Ground’ position signals causing the ground airbrakes to deploy and the aircraft to roll.
Jim Coyne
Delegate of the Civil Aviation Safety Authority 14 October 2003
The above AD is notified in the Commonwealth of Australia Gazette on 5 November 2003.
Overview
The Civil Aviation Safety Regulations 1998, under the authority of the Australian Parliament, were enacted to ensure the safety of civil aviation within Australia. The 1998 Regulations have been amended over time to address evolving safety concerns, with one such amendment being the introduction of Airworthiness Directives (ADs). An Airworthiness Directive is a legal requirement issued by the Civil Aviation Safety Authority (CASA) to address specific safety issues identified in aircraft or aeronautical products. AD/IAI-A/17, issued in 2003, is one such directive that mandates adjustments to the main landing gear ground contact switches for Gulfstream Aerospace LP Model 1125 Astra, Astra SPX, and G100 aeroplanes with certain serial numbers. This directive was introduced in response to reports of in-flight deployment of ground airbrakes following the lowering of the landing gear, a problem that CASA sought to rectify to prevent unsafe conditions. The policy objective is to maintain and enhance the safety of civil aviation by ensuring that aircraft and aeronautical products are maintained in a safe and airworthy condition.
Scope and Application
The Civil Aviation Safety Regulations 1998, under which the Airworthiness Directive (AD) was issued, apply to all aircraft and aeronautical products registered in Australia, including those manufactured by Gulfstream Aerospace LP. Specifically, the AD IAI-A/17 applies to the Gulfstream Aerospace LP Model 1125 Astra, Astra SPX and G100 aeroplanes with serial numbers 004 through 127 inclusive. The directive mandates the adjustment of the main landing gear ground contact switches as per the revised procedures outlined in the G100 Maintenance Manual and Gulfstream Aerospace LP Service Bulletin 1125-32A-233 Revision 1 dated 1 August 2003. The AD requires that this action be taken within 200 hours time in service after the effective date of the directive, which is 27 November 2003. The AD was issued by the Civil Aviation Safety Authority delegate to address the unsafe condition of the in-flight deployment of ground airbrakes following the lowering of the landing gear, a problem reported by the Israel Civil Aviation Administration. The AD is effective throughout the Commonwealth of Australia and was notified in the Commonwealth of Australia Gazette on 5 November 2003.
Key Provisions
The Civil Aviation Safety Regulations 1998, specifically Part 39, subsection 105, provides a framework for issuing Airworthiness Directives (ADs) aimed at maintaining the safety of aircraft and aeronautical products. Section 39.1(1) empowers the delegate of the Civil Aviation Safety Authority (CASA) to issue such directives when necessary to address unsafe conditions. An example of such an AD is AD/IAI-A/17, which pertains to the Gulfstream Aerospace LP (GALP) Model 1125 Astra, Astra SPX, and G100 aeroplanes with specific serial numbers (subsection 39.1(1)). This AD mandates the adjustment of the main landing gear ground contact switches to prevent in-flight deployment of ground airbrakes, a condition reported by the Israel Civil Aviation Administration (subsection 39.1(1) and the Background section).
The obligations under this AD are clear and specific. Operators of the affected aircraft must adjust the main landing gear ground contact switches in accordance with the revised procedures outlined in the G100 Maintenance Manual and GALP Service Bulletin 1125-32A-233 Revision 1, dated 1 August 2003. This adjustment must be completed within 200 hours of time in service after the effective date of the AD, which is 27 November 2003 (subsections 39.1(1) and the Compliance section). Failure to adhere to these requirements can result in significant safety risks, including the in-flight deployment of ground airbrakes, which can lead to loss of control and potential accidents.
Failure to comply with the provisions of this AD may result in severe consequences. While the specific civil or criminal penalties are not detailed within the text of the AD itself, non-compliance with ADs generally can lead to enforcement actions by CASA. These actions may include fines, suspension or revocation of airworthiness certificates, and legal proceedings under the Civil Aviation Act 1988. The exact penalties would be determined based on the severity of the non-compliance and the potential risk to aviation safety. It is imperative for operators to adhere strictly to the timelines and procedures specified to avoid these adverse outcomes.