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.
Cessna 750 (Citation X) Series Aeroplanes
AD/CESSNA 750/1 Bulkhead Web Doubler 9/2004
Applicability: Model 750 aircraft, serial numbers 0001 through 0102.
Requirement: 1. Inspect the bulkhead web for an existing round bulkhead web doubler, in accordance with the Accomplishment Instructions of Cessna Service Bulletin SB750-53-19, dated 20 January 2000.
If there is a round bulkhead web doubler having part number 6711093-38, before further flight, remove the doubler in accordance with the Requirement document.
2. Install a new right bulkhead web doubler having part number 6791213-4 and a left bulkhead web doubler having part number 6791213-3 and enlarge the lightening holes, in accordance with the Accomplishment Instructions of Cessna Service Bulletin SB750-53-19.
Note: FAA AD 2001-07-04 Amdt 39-12169 refers.
Compliance: Before 30 September 2004, unless already accomplished.
This Airworthiness Directive becomes effective on 2 September 2004.
Background: This Directive requires removal of a certain existing bulkhead web doubler, installation of left and right bulkhead web doublers, and enlargement of the lightening holes. This action is necessary to prevent jamming of the roll control system, due to inadequate clearance between the control cable and web.
David Villiers
Delegate of the Civil Aviation Safety Authority 13 July 2004
The above AD is notified in the Commonwealth of Australia Gazette on 11 August 2004.
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Overview
The Civil Aviation Safety Regulations 1998 were enacted to provide comprehensive regulatory coverage for the safety of civil aviation within Australia. These regulations were introduced to address the need for a standardised and rigorous framework governing the maintenance, operation, and certification of aircraft to ensure public safety and compliance with international aviation standards. The regulations were enacted by the Australian Parliament and aim to prevent unsafe conditions that may compromise the safety of air travel. One specific legislative instrument under these regulations is the Airworthiness Directive (AD) concerning the Cessna 750 (Citation X) Series Aeroplanes, issued in 2004. This AD addresses an identified safety issue related to the installation of specific bulkhead web doublers to prevent potential jamming of the roll control system, ensuring continued airworthiness and compliance with safety standards.
Scope and Application
The Airworthiness Directive issued by the Civil Aviation Safety Authority (CASA) under the Civil Aviation Safety Regulations 1998 specifically targets Cessna 750 (Citation X) series aeroplanes with serial numbers ranging from 0001 to 0102. The directive is designed to ensure these aircraft meet required safety standards by addressing an unsafe condition identified with the bulkhead web doublers. The directive mandates inspections, removal, and installation of specific parts, as well as adjustments to lightening holes to prevent jamming of the roll control system. Compliance with this Airworthiness Directive is mandatory for the specified aircraft models, and it must be implemented before 30 September 2004, unless already completed. This directive is applicable nationally, reflecting the Commonwealth's commitment to maintaining civil aviation safety standards. The directive was published in the Commonwealth of Australia Gazette on 11 August 2004 and became effective on 2 September 2004, reinforcing the regulatory oversight and safety measures CASA enforces across the aviation industry.
Key Provisions
The Airworthiness Directive (AD) under subregulation 39.1(1) of the Civil Aviation Safety Regulations 1998 (CASR) applies to Cessna 750 (Citation X) Series aeroplanes, specifically those with serial numbers 0001 through 0102. The directive mandates a series of actions to address an identified unsafe condition related to the aircraft's bulkhead web. Firstly, the directive requires an inspection of the bulkhead web for the presence of a round bulkhead web doubler, specifically part number 6711093-38, as per the instructions in Cessna Service Bulletin SB750-53-19 dated 20 January 2000. If such a doubler is present, it must be removed before further flight. Secondly, the directive requires the installation of new bulkhead web doublers: a right bulkhead web doubler with part number 6791213-4 and a left bulkhead web doubler with part number 6791213-3, along with enlarging the lightening holes, again following the Accomplishment Instructions in Cessna Service Bulletin SB750-53-19.
The AD imposes specific obligations on the parties and entities it governs. Aircraft operators and maintainers must conduct the required inspection and modifications within the timeframe specified, which is before 30 September 2004, unless the modifications have already been completed. This involves ensuring that the aircraft meet the safety standards set out in the AD, which includes removing any existing round bulkhead web doubler if present and installing the specified replacements. These modifications are intended to prevent the jamming of the roll control system due to inadequate clearance between the control cable and the web, thereby maintaining the aircraft's airworthiness.
Failure to comply with the AD may result in serious consequences. The AD does not explicitly state the penalties for non-compliance, but non-compliance with ADs generally can lead to severe civil or criminal penalties under the Civil Aviation Act 1988 and the Civil Aviation Regulations 1988. For civil aviation safety regulations, penalties can include fines and potential grounding of the aircraft, while criminal penalties can include imprisonment and substantial fines. Compliance with ADs is crucial to ensure the safety of air travel, and any breach of these regulations can lead to significant legal repercussions for the non-compliant party.