COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Gulfstream (Rockwell) 114 Series Aeroplanes
AD/ROCK-114/5 Throttle Control Cable - Inspection
and Modification
Applicability: Model 114 with S/Nos. 14000 to 14149. Document: Rockwell International SB No. SB-114-2.
Compliance: Within 100 hours time in service after 30 June 1978.
5/78
Overview
The Civil Aviation Regulations 1998, as amended by F2006B06651, were enacted by the Parliament of Australia to regulate and maintain safety standards in civil aviation within the country. This legislative instrument introduces a specific Airworthiness Directive for Gulfstream (Rockwell) 114 Series Aeroplanes, identified as AD/ROCK-114/5, which pertains to the inspection and modification of the throttle control cable. This directive applies to aircraft models 114 with serial numbers ranging from 14000 to 14149 and mandates compliance within 100 hours of time in service after 30 June 1978, referencing Rockwell International Service Bulletin No. SB-114-2. The overarching policy objective of this regulation is to ensure the safety and reliability of aircraft operations by addressing specific mechanical issues identified in certain aircraft models.
Scope and Application
The Civil Aviation Regulations 1998, as incorporated into Part 39 of the Commonwealth of Australia's legislative framework, specifically address the airworthiness of aircraft through detailed directives. The scope of this particular legislation, as represented by AD/ROCK-114/5, pertains to Gulfstream (Rockwell) 114 Series Aeroplanes with serial numbers ranging from 14000 to 14149. This directive mandates a thorough inspection and modification of the throttle control cable, as outlined in Rockwell International Service Bulletin No. SB-114-2, to ensure continued compliance with safety standards. The directive applies to these specific aircraft models and requires adherence within 100 hours of time in service following the issuance date of 30 June 1978. This regulation is pivotal in maintaining the operational safety of these aircraft within the Australian jurisdiction, ensuring that any aircraft failing to meet these criteria cannot be legally operated until the specified requirements are fulfilled.
Key Provisions
The Civil Aviation Regulations 1998, specifically in Part 39 - 105, include a detailed Schedule of Airworthiness Directives (ADs) that govern the maintenance and operational standards for various aircraft types. One such directive, AD/ROCK-114/5, pertains to Gulfstream (Rockwell) 114 Series Aeroplanes, particularly those with serial numbers (S/Nos.) between 14000 and 14149. This directive mandates the inspection and modification of the throttle control cable. The requirement is to comply with Rockwell International Service Bulletin No. SB-114-2 within 100 hours of time in service after 30 June 1978.
The obligations imposed by AD/ROCK-114/5 are specific and must be adhered to by the aircraft operators or owners of the affected Gulfstream (Rockwell) 114 Series Aeroplanes. They must ensure that the throttle control cable is inspected and, if necessary, modified according to the guidelines set forth in Rockwell International SB-114-2. This involves detailed procedural steps that may include visual inspections, testing, and potential replacement or repair of the throttle control cable to ensure it meets the required safety standards. Operators must maintain accurate records of these inspections and modifications, as these records may be required for compliance verification by the Civil Aviation Safety Authority (CASA).
Failure to comply with AD/ROCK-114/5 can result in significant legal and safety consequences. The regulations do not explicitly state the penalties for non-compliance within the provided text, but general provisions of the Civil Aviation Act 1988 and Civil Aviation Regulations 1998 may apply. Non-compliance could lead to enforcement actions, including fines and potential grounding of the aircraft until the required modifications are completed. Furthermore, there could be severe safety implications, as non-compliance with such a critical directive could compromise the airworthiness of the aircraft, potentially leading to accidents or incidents that endanger lives.
In summary, AD/ROCK-114/5 is a critical directive under the Civil Aviation Regulations 1998, requiring specific inspections and modifications to the throttle control cable of Gulfstream (Rockwell) 114 Series Aeroplanes within a defined timeframe. Operators must meticulously follow these directives to meet safety standards and avoid potential legal and operational repercussions. Although the specific penalties for non-compliance are not detailed in the provided text, the consequences can be severe, highlighting the importance of strict adherence to these regulations.