AD/F28/16 - Escape Chute Operating Strap Attachment - Inspection

Overview

The Civil Aviation Regulations 1998, specifically in PART 39 - 105, establish the Civil Aviation Safety Authority's schedule of airworthiness directives to ensure the safety of aviation operations within Australia. This legislation was enacted to provide a comprehensive framework for the safety of aircraft, including the establishment of airworthiness standards, certification, and ongoing compliance measures. The objective is to maintain a high level of safety in the aviation industry, which is critical given the inherent risks associated with air travel. This particular legislative instrument, F2006B09753, addresses the specific issue of ensuring the safety of Fokker F28 Series Aeroplanes through the issuance of Airworthiness Directive AD/F28/16 concerning the escape chute operating strap and its NK attachment. The directive mandates an inspection of this component within 150 hours of time in service after 30 July 1971 for all models. The Civil Aviation Safety Authority, under the authority of the Australian Parliament, implements these regulations to ensure compliance and thereby mitigate potential safety risks associated with the specified aircraft component.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, pertains to the authority and oversight of the Civil Aviation Safety Authority (CASA) in maintaining airworthiness directives, which are legally binding requirements to ensure the safe operation of aircraft. The scope of this legislation applies to all Fokker F28 Series aeroplanes, mandating that these aircraft must comply with the directive concerning the escape chute operating strap and NK attachment inspection. This applies to all models of the Fokker F28 aircraft series and necessitates compliance within 150 hours of time in service after 30 July 1971. The regulation is geographically applicable within the Commonwealth of Australia and extends to any Fokker F28 Series aeroplanes operating under Australian jurisdiction, irrespective of where they are registered. The directive does not explicitly state any exclusions or exemptions, implying that all Fokker F28 Series aeroplanes must adhere to the stipulated inspection requirements. The application of this directive may be extended or detailed further through subordinate instruments or notices issued by CASA.

Key Provisions

The Civil Aviation Regulations 1998, specifically under PART 39 - 105, include a Schedule of Airworthiness Directives that govern the maintenance and operational standards for various aircraft. One such directive, AD/F28/16, pertains to the Fokker F28 Series Aeroplanes and mandates an inspection of the escape chute operating strap’s NK attachment. This directive applies universally across all models of the Fokker F28 (Section 105). It is imperative that compliance with this directive is achieved within 150 hours of time in service after the specified date of 30 July 1971. The directive imposes a clear obligation on the operators of Fokker F28 Series Aeroplanes to ensure that the escape chute operating strap’s NK attachment is inspected in accordance with the requirements outlined in Fokker SB F28/25-25 (Section 105). This inspection must be conducted within the stipulated timeframe to maintain the airworthiness of the aircraft. Failure to comply with these requirements can lead to serious safety concerns and may render the aircraft non-compliant with civil aviation safety standards. In addition to these operational mandates, the Act stipulates that any non-compliance with the airworthiness directives, including AD/F28/16, may result in severe consequences. Civil aviation authorities have the power to enforce penalties against operators who fail to adhere to these requirements. The potential consequences include fines, suspension of operations, or even revocation of the aircraft’s certificate of airworthiness. These measures are designed to ensure that all parties involved in the operation of Fokker F28 Series Aeroplanes take their safety obligations seriously and comply with all mandated inspections and maintenance procedures. The maximum penalties for non-compliance with airworthiness directives can be substantial. Under the Civil Aviation Act 1988, operators may face fines up to a significant amount, depending on the severity and frequency of the breach. Additionally, criminal charges may be brought against individuals responsible for non-compliance, resulting in further legal ramifications. These penalties underscore the importance of adhering to airworthiness directives and highlight the serious nature of any breaches that could compromise the safety of aviation operations.