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 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.
Beechcraft 200 (Super King Air) Series Aeroplanes
AD/BEECH 200/70 External Door Operating Instructions 4/2003
Applicability: Model 200 and B200 aircraft, serial numbers BB-2, BB-6 through BB-1313, BB-1315 through BB-1384, and BB-1389 through BB-1662.
Model 200C and B200C aircraft, serial numbers BL-1 through BL-72 and BL-124 through BL-140.
Model 200CT and B200CT aircraft, serial numbers BN-1 through BN-4.
Model 200T and B200T aircraft, serial numbers BT-1 through BT-38, and BB-1314.
Requirement: Modify the exterior door operating procedures by incorporating the applicable kit in accordance with the applicable kit instructions as specified in the Accomplishment Instructions section in Raytheon Mandatory Service Bulletin SB 52-3096 Revision 1, Revised: June 2002.
Note: FAA AD 2003-02-03 Amdt 39-13019 refers.
Compliance: Within 200 hours time in service or 12 calendar months after 17 April 2003, whichever occurs first; unless already accomplished.
This Airworthiness Directive becomes effective on 17 April 2003.
Background: Following an accident investigation, the National Transportation Safety Bo ard issued a recommendation to the FAA for improved exterior operating instruction placards on the exterior of the Model 1900 airstair door. Raytheon Aircraft developed door operating instruction placards of improved visibility and legibility for the Model 1900 and other affected turbo propeller aircraft. The actions specified by this Directive are intended to assure that the airstair door or emergency exits can be opened during an emergency situation.
David Alan Villiers
Delegate of the Civil Aviation Safety Authority 28 February 2003
The above AD is notified in the Commonwealth of Australia Gazette on 26 March 2003.
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Overview
The Civil Aviation Safety Regulations 1998, administered by the Civil Aviation Safety Authority (CASA), were enacted to ensure the safety of civil aviation in Australia. The 1998 Regulations introduced a comprehensive framework to regulate the safety of aircraft and related products, services, and personnel, addressing a gap in aviation safety oversight. Part 39 - 105, which pertains to the Schedule of Airworthiness Directives, was established to mandate specific safety measures for aircraft types identified as having potential safety issues. This legislative instrument aims to mitigate risks by enforcing corrective actions on aircraft and aeronautical products deemed unsafe under certain conditions. The policy objective is to enhance overall aviation safety by ensuring that aircraft meet the necessary safety standards, thereby protecting passengers, crew, and the general public from potential hazards.
Scope and Application
The Civil Aviation Safety Regulations 1998, specifically Part 39 - 105, sets forth the Civil Aviation Safety Authority (CASA) Schedule of Airworthiness Directives, which applies to certain aircraft models within the Commonwealth of Australia. This particular Airworthiness Directive (AD) pertains to the Beechcraft 200 (Super King Air) Series Aeroplanes, specifically targeting model 200 and B200 aircraft with particular serial numbers, as well as model 200C and B200C aircraft, and models 200T and B200T. The directive mandates modifications to the exterior door operating procedures to enhance safety during emergency situations. The requirement is to incorporate an applicable kit in accordance with specified instructions within 200 hours in service or 12 calendar months from 17 April 2003, whichever comes first, unless the modifications have already been completed. The AD became effective on 17 April 2003 and is published in the Commonwealth of Australia Gazette on 26 March 2003.
Key Provisions
The Airworthiness Directive (AD) under subregulation 39.1 (1) of the Civil Aviation Safety Regulations 1998 (CAR 1998) (section 1) applies to specific models and serial numbers of Beechcraft 200 (Super King Air) Series Aeroplanes, specifically Model 200 and B200 aircraft with serial numbers BB-2, BB-6 through BB-1313, BB-1315 through BB-1384, and BB-1389 through BB-1662; Model 200C and B200C aircraft with serial numbers BL-1 through BL-72 and BL-124 through BL-140; Model 200CT and B200CT aircraft with serial numbers BN-1 through BN-4; and Model 200T and B200T aircraft with serial numbers BT-1 through BT-38, and BB-1314 (section 2). The directive mandates the modification of the exterior door operating procedures by incorporating the applicable kit in accordance with the instructions specified in Raytheon Mandatory Service Bulletin SB 52-3096 Revision 1, Revised: June 2002 (section 3). This action is necessary to address an unsafe condition identified following an accident investigation, ensuring that airstair doors or emergency exits can be opened during an emergency situation.
The AD imposes obligations on the owners and operators of the affected aircraft to modify their exterior door operating procedures as per the instructions provided in the Raytheon Mandatory Service Bulletin. This includes incorporating the specified kit and following the accomplishment instructions detailed in the bulletin. The compliance period for these modifications is within 200 hours of time in service or 12 calendar months after 17 April 2003, whichever comes first, unless the modifications have already been accomplished (section 4). Failure to comply with these requirements may result in the aircraft being deemed unairworthy, potentially leading to operational restrictions or grounding until the necessary modifications are completed.
In the event of non-compliance with the Airworthiness Directive, the Civil Aviation Safety Authority (CASA) may take enforcement actions. While the regulations do not specify maximum penalties for non-compliance, such actions could include fines, operational restrictions, and potential grounding of the aircraft. In severe cases, the authority may pursue legal action against the owner or operator, resulting in civil or criminal penalties as appropriate under the applicable aviation safety laws. The consequences of non-compliance can also extend to increased safety risks and potential liability for accidents or incidents arising from the failure to adhere to the mandated safety directives.