COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Consolidated Aeronautics, Colonial and LA-4 Series Aeroplanes
AD/LA-4/20 Main Landing Gear - Rocker Castings
P/N 2-4113-1 - Inspection and Replacement
Applicability: All model LA4-200 with S/Nos. 740 to 997.
1/80
Requirement: 1. Visually inspect Rocker Castings P/No. 2-4113-1, located at upper end of main landing gear struts, for cracks radiating from the bolt holes.
2. Replace Rocker Castings P/No. 2-4113-1 with fabricated items P/Nos. 2-4113-3 or 2-4110-7.
Note: SB No. B63-4497 refers.
Compliance: 1. At each daily or overnight inspection. For aircraft maintained in accordance with ANO 100.5.1 this Directive shall be entered on the maintenance release as maintenance required. The inspection may be performed by the pilot in command, in which case certification is not required. In all other cases certification may be made on the maintenance release. This inspection may also be performed and certified by any Licensed Aircraft Maintenance Engineer.
2. Before 1 January 1981.
Background: Failure of the subject P/No. Rocker Castings has occurred on overseas registered aeroplanes.
Overview
The Civil Aviation Regulations 1998, established by the Australian Parliament, serves as a comprehensive framework for the regulation of civil aviation in Australia, aiming to ensure the safety and efficiency of air travel. This legislation, specifically within Part 39, addresses the issuance of Airworthiness Directives to maintain aircraft safety standards. The enactment of these regulations fills a critical gap by providing clear, enforceable standards for aircraft maintenance and operation, thus protecting the public and ensuring the integrity of the national airspace. This particular legislative instrument, F2006B11071, pertains to the maintenance requirements of Consolidated Aeronautics, Colonial and LA-4 Series Aeroplanes, focusing on the inspection and replacement of main landing gear rocker castings. The objective of this directive is to prevent structural failures by mandating regular inspections and timely replacements, thereby enhancing aviation safety.
Scope and Application
The Civil Aviation Regulations 1998, under Part 39 - 105, specifically mandate compliance with the Civil Aviation Safety Authority’s Airworthiness Directives, including AD/LA-4/20 concerning Consolidated Aeronautics, Colonial and LA-4 Series Aeroplanes. This directive applies to all model LA4-200 aircraft with serial numbers ranging from 740 to 997.1/80. The directive requires a thorough visual inspection of Rocker Castings P/No. 2-4113-1 at the upper end of the main landing gear struts for any cracks emanating from the bolt holes, and mandates the replacement of these castings with fabricated items P/Nos. 2-4113-3 or 2-4110-7. Compliance is mandatory at each daily or overnight inspection, and must be documented on the maintenance release as maintenance required. This task can be performed by the pilot in command, who does not need certification for the inspection, or by a Licensed Aircraft Maintenance Engineer. The directive applies nationally within Australia and is enforced by the Civil Aviation Safety Authority, which has the authority to extend or restrict its application through subordinate instruments.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, includes AD/LA-4/20, which pertains to Consolidated Aeronautics, Colonial and LA-4 Series Aeroplanes. This directive (Section 1) mandates the inspection and replacement of main landing gear rocker castings on model LA4-200 aeroplanes with serial numbers between 740 and 997.1/80. The requirement (Section 1) is to visually inspect Rocker Castings P/No. 2-4113-1 for cracks emanating from the bolt holes and to replace them with fabricated items P/Nos. 2-4113-3 or 2-4110-7.
The regulations (Section 2) outline that the inspection should occur at each daily or overnight inspection and must be recorded as maintenance required if the aircraft is maintained under ANO 100.5.1. This inspection can be performed by the pilot in command, in which case certification is not required. However, if performed by someone else, such as a Licensed Aircraft Maintenance Engineer, certification is necessary. Additionally, the directive mandates that this action must be taken before 1 January 1981, in line with Service Bulletin No. B63-4497.
The obligations imposed by this directive (Section 3) are stringent and clear. Operators of the specified aeroplanes must ensure that the daily or overnight inspections include a detailed visual check of the rocker castings. Any defects found must be addressed immediately by replacing the castings with the specified fabricated items. Additionally, the directive must be recorded in the maintenance release to ensure compliance. The directive allows flexibility in who can perform the inspection, which can be the pilot in command or a licensed engineer, but requires certification in the latter case.
Failure to comply with AD/LA-4/20 (Section 4) could have significant consequences. The regulations do not specify penalties or offences directly within the directive but non-compliance with airworthiness directives generally can lead to enforcement actions by the Civil Aviation Safety Authority (CASA). Such actions might include fines, suspension or revocation of aircraft certificates, and other regulatory sanctions. The specific penalties can vary but are designed to ensure the highest safety standards are maintained in civil aviation operations.