COMMONWEALTH OF AUSTRALIA CIVIL AVIATION ORDERS CIVIL AVIATION SAFETY AUTHORITY PART 105 SCHEDULE OF AIRWORTHINESS DIRECTIVES
GULFSTREAM (GRUMMAN) G.159 SERIES AEROPLANES
AD/G159/31 Engine Fire Extinguisher Switch - Inspection 5/77
Applicability: All Gulfstream 1 and TC4C aircraft. Document: Grumman Customer Bulletin No. 292.
Compliance: Within 100 hours time in service after 31 May 1977.
Overview
The Civil Aviation Orders, enacted in 1988, establish a regulatory framework for civil aviation in Australia, ensuring safety, efficiency, and environmental protection within the sector. The Civil Aviation (Airworthiness of Aircraft) Regulations 2008, under Part 105, specifically address the airworthiness directives that are essential for maintaining the safety standards of aircraft. One such directive, AD/G159/31, pertains to the inspection of engine fire extinguisher switches on Gulfstream (Grumman) G.159 Series aeroplanes. This directive was introduced to address the risk of fire extinguisher switches inadvertently opening during flight, which could lead to significant safety hazards. The policy objective of the Civil Aviation Orders is to safeguard the public by ensuring that aircraft meet specific safety and airworthiness standards, thereby mitigating risks associated with civil aviation activities.
Scope and Application
The Civil Aviation Orders, specifically Part 105 Schedule of Airworthiness Directives, apply to all Gulfstream 1 and TC4C aircraft, imposing mandatory compliance requirements for these aircraft operators. This legislative instrument, identified as AD/G159/31, pertains to the inspection of the engine fire extinguisher switch on the Gulfstream (Grumman) G.159 series aeroplanes, referencing Grumman Customer Bulletin No. 292. The directive mandates that the specified inspection must be completed within 100 hours of time in service following the date of 31 May 1977. This requirement applies at the Commonwealth level, impacting all relevant aircraft within the Australian jurisdiction, thereby ensuring adherence to stringent safety standards in the civil aviation sector. There are no exclusions or exemptions mentioned in this directive, underscoring the importance of timely and precise compliance to maintain airworthiness.
Key Provisions
The Civil Aviation Orders (CAO) establish a comprehensive regulatory framework governing civil aviation in Australia, with specific provisions detailed in the Civil Aviation Safety Authority (CASA) Part 105 Schedule of Airworthiness Directives. One such directive, AD/G159/31, pertains to the Gulfstream (Grumman) G.159 series aeroplanes and specifically addresses the inspection of the engine fire extinguisher switch (paragraph 5/77). This directive applies to all Gulfstream 1 and TC4C aircraft and references Grumman Customer Bulletin No. 292 as the governing document for compliance.
The main operative section of AD/G159/31 requires operators of the specified Gulfstream aircraft to inspect the engine fire extinguisher switch within 100 hours of time in service following 31 May 1977. This inspection is mandatory to ensure the continued airworthiness and safety of the aircraft. It is imperative that the inspection is carried out in accordance with the guidelines set forth in Grumman Customer Bulletin No. 292, which provides detailed instructions on the necessary procedures and checks.
Compliance with AD/G159/31 imposes specific obligations on the parties governed by this directive. Operators of the affected Gulfstream 1 and TC4C aircraft must ensure that the engine fire extinguisher switch is inspected by qualified personnel within the specified timeframe. Additionally, operators are required to maintain records of the inspections conducted and ensure that any necessary repairs or replacements are performed in accordance with the directive. The directive also mandates that operators must keep abreast of any updates or additional instructions issued by CASA or Grumman to address this safety concern.
Failure to comply with AD/G159/31 can result in significant civil and criminal consequences. Non-compliance with airworthiness directives is considered a serious breach of aviation safety regulations. The Civil Aviation Act 1988 imposes penalties for such breaches, which can include fines and, in severe cases, imprisonment. The specific penalties for non-compliance with this directive are not detailed in the legislative text but are subject to the broader provisions of the Act, which can include substantial monetary fines and imprisonment for individuals and corporations found guilty of failing to adhere to safety directives. The seriousness of these consequences underscores the importance of strict compliance with the AD/G159/31 directive to maintain the highest standards of aviation safety.