COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Gulfstream (Grumman) G1159 and G-IV Series Aeroplanes
AD/G1159/28 Control Column Wheel Attaching Shaft - Inspection 7/80
Applicability: All models G1159.
Document: Gulfstream American Customer Bulletin No. 295. Compliance: Within 100 hours time in service after 31 July 1980.
Background: A pilot’s control wheel separated from the control column of a G1159 during a landing approach in an overseas operation.
Overview
The Civil Aviation Regulations 1998, as amended, were enacted to ensure the safety and efficiency of civil aviation in Australia. Part 39 of these regulations includes the Airworthiness Directives that are binding on aircraft operators to maintain the safety of their aircraft. Specifically, AD/G1159/28 addresses an issue identified with the control column wheel attaching shaft on Gulfstream (Grumman) G1159 and G-IV series aeroplanes. This directive was introduced to rectify a problem that arose when a control wheel detached from its column during a landing approach, as reported in Gulfstream American Customer Bulletin No. 295. The policy objective behind this directive is to prevent a recurrence of such incidents by mandating inspections and timely compliance within 100 hours of the aircraft’s time in service after 31 July 1980. These regulations are enacted by the Australian Parliament to uphold the highest standards of aviation safety and are enforced by the Civil Aviation Safety Authority.
Scope and Application
The Civil Aviation Safety Authority (CASA) has issued an Airworthiness Directive (AD) under the Civil Aviation Regulations 1998, specifically within Part 39 - 105, which governs the scheduling of airworthiness directives. This particular directive, AD/G1159/28, pertains to Gulfstream (Grumman) G1159 and G-IV Series aeroplanes and mandates the inspection of the control column wheel attaching shaft. The directive applies to all models G1159 and requires compliance within 100 hours of time in service after 31 July 1980, following the documented incident where a pilot’s control wheel detached from the control column during a landing approach in an overseas operation. The AD is a regulatory measure to ensure the continued airworthiness of the specified aircraft models, necessitating compliance by the aircraft operators and owners to maintain safety standards. The directive’s scope is confined to the specified Gulfstream aircraft models, and no exclusions or exemptions are stated in the text provided.
Key Provisions
The Civil Aviation Regulations 1998, specifically Part 39 - 105, contain detailed directives concerning the airworthiness of certain aircraft models. Section (AD/G1159/28) pertains to Gulfstream (Grumman) G1159 and G-IV Series Aeroplanes, mandating an inspection of the control column wheel attaching shaft. This directive was issued following an incident where the control wheel of a G1159 detached during a landing approach, highlighting a critical safety concern. The requirement is for an inspection to be conducted within 100 hours of time in service after 31 July 1980, and it references Gulfstream American Customer Bulletin No. 295 as the document containing the necessary inspection procedures.
Under this legislation, the primary obligation imposed on the operators and owners of the G1159 and G-IV Series Aeroplanes is to ensure that the specified inspection of the control column wheel attaching shaft is carried out in accordance with the stipulated timeframe. This means that the aircraft must be grounded and the inspection must be completed by a qualified individual who is familiar with the procedures outlined in Gulfstream American Customer Bulletin No. 295. The inspection must be thorough and meet the safety standards set forth to prevent any recurrence of the detachment incident.
Failure to comply with the inspection requirements outlined in Section (AD/G1159/28) of the Civil Aviation Regulations 1998 can result in serious consequences. Operationally, non-compliance may lead to the grounding of the aircraft until the required inspection is performed. From a legal perspective, there are potential civil penalties for breaches of these regulations. The specific penalties are not detailed in the provided text, but generally, they can include fines and other civil sanctions. In more severe cases, criminal charges might also be pursued, leading to imprisonment or substantial fines, depending on the severity of the breach and its impact on aviation safety.