AD/F27/134 Amdt 1 - Main Wing Tank and Collector Tank Fuel Line

Overview

The Civil Aviation Regulations 1998, specifically Part 39 - 105, establishes the Civil Aviation Safety Authority Schedule of Airworthiness Directives. One such directive, AD/F27/134 Amendment 1, pertains to the Fokker F27 series aeroplanes, excluding the Fokker F27 Mk 050. The directive was enacted to address issues related to potential fuel leaks caused by damage to the fuel line between the main wing tank and the collector tank, in accordance with the technical requirements of the Netherlands Directive BLA 92-102 Issue 2 dated 23 October 1992. The requirement is to conduct an inspection of this fuel line to ensure compliance, with an effective date of 7 January 1993. This amendment was introduced to ensure the continued airworthiness of the Fokker F27 series aircraft by implementing international safety standards. The enactment of this directive by the Civil Aviation Safety Authority is aimed at maintaining safety standards in civil aviation, ensuring that aircraft meet specific technical requirements to prevent fuel leaks and associated hazards. The directive is a response to identified safety issues and aligns with the overarching policy objective of the Civil Aviation Regulations 1998 to ensure the safety of aircraft and the protection of lives.

Scope and Application

The Civil Aviation Regulations 1998, specifically Part 39 - 105, establish the scope and application of the Civil Aviation Safety Authority's Schedule of Airworthiness Directives concerning Fokker F27 Series Aeroplanes. This legislation applies to all Fokker F27 aircraft, excluding the Mk 050 variant, across all serial numbers, mandating compliance with the technical requirements set forth in the Netherlands Directive BLA 92-102 Issue 2 dated 23 October 1992. This requirement necessitates an inspection of the fuel line between the main wing tank and the collector tank for any damage that could potentially lead to fuel leaks. Compliance with this directive must be achieved as specified in the Requirement Document, with an effective date set for 7 January 1993. Additionally, Fokker Service Bulletin F27/28-61 dated 3 September 1992 provides further context and guidance in this matter. The regulations are enforced under the Commonwealth of Australia and pertain to the operation and maintenance of Fokker F27 aircraft within Australian jurisdiction.

Key Provisions

The Civil Aviation Regulations 1998, specifically in Part 39 - 105, which pertains to the Civil Aviation Safety Authority Schedule of Airworthiness Directives, includes a number of mandatory directives to ensure the safety of aviation operations. One such directive, AD/F27/134 Amendment 1, pertains to the Fokker F27 Series aeroplanes, excluding the Mk 050 model, across all serial numbers. This directive mandates adherence to the technical requirements outlined in the Netherlands Directive BLA 92-102 Issue 2 dated 23 October 1992. For reference, Fokker Service Bulletin F27/28-61 dated 3 September 1992 also provides related information. Compliance with this directive is required as specified in the Requirement Document, effective from 7 January 1993. Operators of Fokker F27 aircraft, except for the Mk 050 model, must ensure that the fuel line between the main wing tank and the collector tank is inspected for any damage that could potentially lead to fuel leaks. This obligation is paramount to maintaining airworthiness and ensuring the safety of the aircraft and its occupants. The inspection and any necessary corrective actions must be carried out in accordance with the technical specifications provided in the Netherlands Directive BLA 92-102 Issue 2. Failure to comply with these requirements could result in serious safety risks and potential regulatory repercussions. Under the Civil Aviation Regulations 1998, non-compliance with airworthiness directives such as AD/F27/134 Amendment 1 can have significant consequences. While the specific offences and penalties for breaching these regulations are not detailed in the provided text, generally, non-compliance with airworthiness directives can result in severe penalties. This may include fines, suspension or revocation of the aircraft’s certificate of airworthiness, and potential criminal charges if the breach leads to an accident or endangers safety. The severity of the penalties often correlates with the degree of negligence and the extent of safety compromised by the breach. Given the critical nature of airworthiness directives, operators must diligently follow the requirements set forth in AD/F27/134 Amendment 1 to avoid any breaches. This involves conducting thorough inspections and repairs as specified, maintaining detailed records of compliance, and ensuring that all personnel involved are adequately trained and informed of the necessary procedures. By adhering to these regulations, operators not only safeguard their operations but also contribute to the overall safety of the aviation industry.