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.
Boeing 727 Series Aeroplanes
AD/B727/177 Main Deck Cargo Door Hinge, Cargo Door System
and Cargo Barrier - 1
11/2002
Applicability: Model 727 series aircraft that have been converted from a passenger to a cargo- carrying (“freighter”) configuration in accordance with Supplemental Type Certificate (STC) SA1767SO or SA1768SO.
Requirement: Action in accordance with the technical requirements of FAA AD 2002-16-19 Amdt 39-12858
Note: Accomplishment of the actions in accordance with Federal Express E.O. Revision Record 7-5230-7-5000, Revision B, release date 18 December 2001, constitutes compliance with the requirements of paragraphs (b) and (c) of the Requirement document.
Compliance: As specified in the Requirement document with a revised effective date of 31 October 2002.
This Airworthiness Directive becomes effective on 31 October 2002.
Background: The FAA has determined that the main deck cargo door hinge installed on conversion from a passenger carrying to a cargo carrying aircraft configuration, is not fail- safe; that certain main deck cargo door control systems do not provide an adequate leve l of safety; and that the main deck cargo barrier is not structurally adequate during an emergency landing.
David Alan Villiers
Delegate of the Civil Aviation Safety Authority 11 September 2002
The above AD is notified in the Commonwealth of Australia Gazette on 9 October 2002.
Overview
The Civil Aviation Regulations 1998 (CAR 1998) was enacted to provide a framework for the regulation of civil aviation in Australia, ensuring the safety and efficiency of aviation operations within the country. This legislation was introduced to address the need for comprehensive regulatory measures governing all aspects of civil aviation, from aircraft operations to maintenance and airworthiness standards. The CAR 1998 is administered by the Civil Aviation Safety Authority (CASA), which is the body responsible for enforcing these regulations. The primary policy objective of the CAR 1998 is to ensure the highest possible level of safety in civil aviation through rigorous regulatory oversight and the issuance of airworthiness directives as necessary.
One such example of regulatory action is the Airworthiness Directive (AD) issued under the CAR 1998 for Boeing 727 Series Aeroplanes, specifically addressing the main deck cargo door hinge, cargo door system, and cargo barrier. This AD was issued in response to identified safety concerns regarding the structural integrity and operational safety of these components on converted freighter aircraft. The directive mandates corrective actions to ensure these components meet required safety standards, thereby mitigating risks associated with the unsafe conditions identified. The AD was issued by a delegate of CASA and is aimed at ensuring compliance with specific technical requirements to maintain airworthiness and passenger safety.
Scope and Application
The Airworthiness Directive (AD) issued under the Civil Aviation Regulations 1998 pertains specifically to Boeing 727 series aircraft that have been converted from passenger to cargo-carrying configurations as per Supplemental Type Certificates (STCs) SA1767SO or SA1768SO. This AD mandates corrective actions to address safety concerns identified with the main deck cargo door hinge, cargo door system, and cargo barrier of these aircraft, as determined by the Federal Aviation Administration (FAA). The directive requires adherence to the technical specifications outlined in FAA AD 2002-16-19 Amdt 39-12858, and compliance with the Federal Express E.O. Revision Record 7-5230-7-5000, Revision B, dated 18 December 2001, for the actions to be considered compliant. The AD came into effect on 31 October 2002, following its notification in the Commonwealth of Australia Gazette on 9 October 2002. This regulatory action is crucial for ensuring the airworthiness and safety of the affected aircraft operating within Australia.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, includes provisions for Airworthiness Directives (AD) that are issued by the Civil Aviation Safety Authority (CASA) delegate. This particular AD, AD/B727/177, pertains to Boeing 727 Series Aeroplanes that have been converted from passenger to cargo-carrying configurations (section 1). The directive mandates certain actions to address identified unsafe conditions regarding the main deck cargo door hinge, cargo door system, and cargo barrier (section 2).
The AD applies to Model 727 series aircraft that have undergone conversion to cargo-carrying configurations as per Supplemental Type Certificate (STC) SA1767SO or SA1768SO (section 3). The directive requires adherence to the technical requirements specified in FAA AD 2002-16-19 Amdt 39-12858, and compliance with Federal Express E.O. Revision Record 7-5230-7-5000, Revision B, dated 18 December 2001, is noted as a means of fulfilling the requirements (section 4). The directive specifies a compliance period and an effective date of 31 October 2002 (section 5).
Entities and parties governed by this AD must take the necessary actions to correct the unsafe conditions identified within the specified timeframe. Failure to comply with the AD can result in civil and criminal consequences, including potential penalties for non-compliance. While the specific penalties are not detailed in this excerpt, the legislation generally provides for substantial fines and possible imprisonment for breaches of aviation safety regulations (section 6). The AD itself serves as a legal mandate to ensure that aircraft meet the required safety standards to prevent accidents and ensure the safety of passengers and crew.