COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Schweizer (Hughes) 269 Series Helicopters
AD/HU 269/44 Tail Rotor Control Stop - Inspection 8/72
Applicability: Model 269A with S/Nos. 0011 to 0314.
Model 269A (TH- 55A) with S/Nos. 0315 and subsequent. Model 269B with S/Nos. 0001 to 0457.
Model 269C with S/Nos. 0001 to 0104.
Document: Hughes SIN No. N-98.
Compliance: Within 100 hours time in service after 31 August 1972.
Overview
The Civil Aviation Regulations 1998, which are administered by the Civil Aviation Safety Authority, were enacted to ensure the safety of civil aviation within Australia. One of the legislative instruments, F2006B10608, specifically addresses the airworthiness of Schweizer (Hughes) 269 Series Helicopters. This legislation was introduced to address the need for regular inspections of the tail rotor control stop in specified Schweizer (Hughes) 269 Series Helicopters to ensure continued compliance with safety standards. The policy objective is to prevent potential safety issues by requiring compliance within 100 hours of time in service after 31 August 1972, as outlined in Hughes SIN No. N-98. This instrument is essential in maintaining the integrity and safety of these aircraft models within the Australian civil aviation framework.
Scope and Application
The Civil Aviation Regulations 1998, as specified in PART 39 - 105, govern the safety directives for Schweizer (Hughes) 269 Series Helicopters under the Civil Aviation Safety Authority (CASA) schedule of airworthiness directives. This particular legislation applies to specific models of Schweizer (Hughes) 269 Series Helicopters, including Model 269A with serial numbers ranging from 0011 to 0314, Model 269A (TH-55A) with serial numbers 0315 and subsequent, Model 269B with serial numbers from 0001 to 0457, and Model 269C with serial numbers from 0001 to 0104. The regulation mandates compliance with a specific inspection directive for the tail rotor control stop, as outlined in Hughes SIN No. N-98, within 100 hours of time in service following 31 August 1972. The geographic reach of this legislation extends across the Commonwealth of Australia, ensuring uniform safety standards are met throughout the nation. This regulation does not explicitly mention any exclusions, exemptions, or thresholds, and its application may be further detailed or modified through subordinate instruments issued by CASA.
Key Provisions
The Civil Aviation Regulations 1998, specifically under Part 39, includes a series of directives aimed at ensuring the safety and airworthiness of aircraft. One such directive, AD/HU 269/44, pertains to the tail rotor control stop inspection for Schweizer (Hughes) 269 series helicopters (section 39-105). This directive applies to certain models and serial numbers of the Schweizer (Hughes) 269 series, including Model 269A with serial numbers 0011 to 0314 and 0315 and subsequent, Model 269B with serial numbers 0001 to 0457, and Model 269C with serial numbers 0001 to 0104. The directive requires a thorough inspection of the tail rotor control stop within 100 hours of time in service after 31 August 1972 (section 39-105). Compliance with this directive is to be documented using Hughes SIN No. N-98.
Entities and individuals governed by this directive must ensure that the specified inspection is conducted within the stipulated timeframe. This involves meticulous examination of the tail rotor control stop to identify any potential issues that might compromise the aircraft's safety. The obligation lies with the aircraft operators, maintenance personnel, and other relevant parties to adhere to this requirement diligently. Failure to conduct the required inspection within the prescribed timeframe can lead to serious safety implications and potential non-compliance with aviation safety standards.
Breaches of the airworthiness directive AD/HU 269/44 can have significant consequences. While the specific penalties for non-compliance are not detailed in the legislative instrument, it is generally understood that failure to adhere to such directives can result in enforcement actions by the Civil Aviation Safety Authority (CASA). These actions can include fines, suspension or revocation of aircraft operating certificates, and other regulatory penalties. The severity of these consequences underscores the importance of strict compliance with the stipulated inspection requirements to ensure the continued safety and airworthiness of the Schweizer (Hughes) 269 series helicopters.