AD/SAAB/2 - Fuel Pump Actuating System

Overview

The Civil Aviation Regulations 1998, under Part 39 - 105, address safety concerns in civil aviation through Airworthiness Directives (ADs). Specifically, AD/SAAB/2 pertains to the Saab Safir Series Aeroplanes and mandates actions concerning the fuel pump actuating system to ensure safety. Enacted by the Commonwealth of Australia, this legislation was introduced to address the problem of fuel pump cable failure during emergency situations, as reported by the manufacturer. The policy objective is to ensure that any identified safety issues are promptly addressed, thereby maintaining the airworthiness of aircraft and protecting passengers and crew. This legislation is a legislative instrument issued by the Civil Aviation Safety Authority under the authority of the Civil Aviation Act 1988. The directive requires compliance within 100 hours of time in service following its issuance on 31 May 1986, aligning with the Swedish AD No 1-017 to maintain consistency in safety standards across jurisdictions.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, mandates the application of Airworthiness Directives (AD) for certain aircraft, including the Saab Safir Series aeroplanes, to ensure ongoing airworthiness and safety. The legislation requires that models Saab Safir 91B, 91B-2, 91C, and 91D must comply with the directive regarding the fuel pump actuating system, as stipulated in AD/SAAB/2. This compliance is necessitated by the requirement to address the issue of the manually actuated fuel pump cable assembly failing during operation in an emergency, as reported by the manufacturer. Compliance must be achieved within 100 hours of time in service following 31 May 1986. The directive references Swedish AD No 1-017 for further guidance on the necessary actions, which should be implemented in accordance with SAAB SB 91.4.003. The scope of this legislation is confined to the specified Saab Safir models, and it applies nationally, overseen by the Civil Aviation Safety Authority. There are no exclusions or exemptions mentioned in the provided text, and the regulation does not explicitly extend or restrict its application through subordinate instruments.

Key Provisions

The main operative sections of the Civil Aviation Regulations 1998, specifically within Part 39 - 105, detail the Airworthiness Directives (ADs) concerning the Saab Safir Series Aeroplanes. Section AD/SAAB/2 mandates that aircraft models SAAB Safir 91B, 91B-2, 91C, and 91D must comply with the action outlined in Saab SB 91.4.003. This requirement was prompted by a reported instance where the cable assembly of the manually actuated fuel pump failed during an emergency, as referenced by Swedish AD No 1-017. Compliance with this directive must be achieved within 100 hours of the aircraft being in service after 31 May 1986. The obligations imposed by this regulation are primarily on the operators and maintenance personnel of the specified Saab aircraft models. They must ensure that the action specified in Saab SB 91.4.003 is implemented within the stipulated timeframe to maintain airworthiness. This entails conducting a thorough inspection and, if necessary, replacing or repairing the fuel pump actuating system to prevent any potential failures during critical operations. Operators must document compliance and retain records of any actions taken to meet this requirement. Failure to comply with AD/SAAB/2 could lead to significant consequences. The Civil Aviation Safety Authority (CASA) may take enforcement action against the operator for not adhering to airworthiness directives. Under the Civil Aviation Act 1988, non-compliance can result in penalties, including fines or other civil actions. Additionally, the operator could face criminal charges if the failure to comply is deemed to have caused an aviation accident or serious incident, potentially resulting in more severe penalties. The exact penalties are determined based on the severity of the breach and the impact on aviation safety.