COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters
AD/HU 369/95 Main Rotor Transmission - Clutch
Bearing - Outer Race Change
8/98
DM
Applicability: Model 369, 369A, 369D,369E, 369F, 369FF, 369H, 369HE, 369HM, 369HS, 500N,
YOH-6A and OH-6A helicopters.
Requirement: Inspect the overrunning clutch assembly outer race, part number (P/N) 369A5352, to determine its serial number (S/N) in accordance with paragraphs A thru’ C of the Accomplishment Instructions contained in McDonnell Douglas Helicopter Systems Service Information Notice HN-215.2, DN-156.2, EN-46.2, FN-34.2, NN-010, dated March 18 1997 (service information notice). Remove any overrunning clutch outer race, P/N 369A5352 having a serial number S/N of 0692 through 0927, and replace it with an airworthy overrunning clutch outer race P/N 369A5352-5, together with a wave washer, P/N W1593-018, in accordance with the service information notice.
Note: FAA AD 98-09-02 Amdt 39-10481 refers.
Compliance: Within 50 hours time in service from the effective date of this directive.
This airworthiness directive becomes effective on 20 May 1998.
Background: This AD supersedes AD/HU 369/75. The requirement of the directive is extended to replace all outer races with a certain serial number regardless of heat treatment code. The previous AD merely inspected the races and replaced a limited number subject to the heat treatment code. Experience in the USA has shown that failures have occurred regardless of heat treatment code and the FAA has now mandated that all outer races of a certain batch require replacement.
Overview
The Civil Aviation Regulations 1998 (Civil Aviation Act 1988) introduced a comprehensive regulatory framework to ensure the safety and efficiency of civil aviation in Australia. Specifically, Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives, addresses the critical need to mandate specific maintenance actions to ensure the continued airworthiness of aircraft. The Civil Aviation Safety Authority, acting under the authority of the Commonwealth Parliament, established these regulations to address identified safety gaps and ensure compliance with international standards. The policy objective is to enhance aviation safety by enforcing regular inspections and necessary repairs on aircraft components that have demonstrated potential safety risks. This particular legislative instrument, concerning the McDonnell Douglas (Hughes) and Kawasaki 369 Series Helicopters, was enacted to mandate the inspection and replacement of specific main rotor transmission clutch bearing outer races to mitigate the risk of failure, thereby protecting the safety of all those involved in aviation operations.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105 and the Airworthiness Directives issued under it, govern the airworthiness of aircraft registered in Australia and operated within Australian airspace. The regulation in question, AD/HU 369/95, applies to a specific series of McDonnell Douglas (Hughes) and Kawasaki helicopters, including models 369, 369A, 369D, 369E, 369F, 369FF, 369H, 369HE, 369HM, 369HS, 500N, YOH-6A, and OH-6A. The directive mandates that operators inspect the overrunning clutch assembly outer race of these helicopters and replace any part with a serial number between 0692 and 0927 to ensure safety. This directive is effective from 20 May 1998 and compliance is required within 50 hours of the directive's effective date. It supersedes previous directives and extends the requirement to all specified serial numbers regardless of heat treatment code, based on experience in the United States where similar failures occurred. The directive is applicable nationally and is enforced by the Civil Aviation Safety Authority (CASA).
Key Provisions
The key operative sections of this Civil Aviation Regulations 1998 directive (AD/HU 369/95) pertain to the inspection and replacement of the overrunning clutch outer race for specific models of McDonnell Douglas (Hughes) and Kawasaki helicopters. Section 1 outlines the applicability of the directive, which includes models 369, 369A, 369D, 369E, 369F, 369FF, 369H, 369HE, 369HM, 369HS, 500N, YOH-6A, and OH-6A helicopters. Section 2 mandates that the outer race of the overrunning clutch assembly, part number 369A5352, must be inspected to determine its serial number in accordance with the Accomplishment Instructions detailed in specified McDonnell Douglas Helicopter Systems Service Information Notices (paragraphs A through C of HN-215.2, DN-156.2, EN-46.2, FN-34.2, NN-010 dated March 18, 1997). Section 3 requires the removal and replacement of any overrunning clutch outer race with a serial number between 0692 and 0927 with a specified airworthy version, part number 369A5352-5, along with a wave washer, part number W1593-018, following the instructions provided in the service information notice.
The obligations imposed by this directive are primarily on the operators and maintenance personnel of the specified helicopter models. Operators must ensure that the inspection and, if necessary, the replacement of the overrunning clutch outer race are carried out within 50 hours of time in service from the effective date of the directive, which is 20 May 1998. Maintenance personnel must follow the detailed instructions in the referenced service information notices to perform these tasks correctly and safely. These obligations are intended to ensure the continued airworthiness and safety of the helicopters in question by addressing a known issue with the clutch outer races.
Failure to comply with the requirements of this airworthiness directive may result in significant legal and safety consequences. While the specific legislative instrument does not detail penalties, non-compliance with Civil Aviation Regulations 1998 directives can result in enforcement actions by the Civil Aviation Safety Authority (CASA). These actions may include fines, operational restrictions, or even the grounding of the affected aircraft until the directive is complied with. In severe cases, non-compliance could lead to criminal charges if it is found to have contributed to an aviation accident or incident. The potential penalties underscore the importance of adhering to the directive to maintain the safety and regulatory compliance of the helicopters involved.