COMMONWEALTH OF AUSTRALIA (Civil Aviation Regulations 1998), PART 39 - 105 CIVIL AVIATION SAFETY AUTHORITY
SCHEDULE OF AIRWORTHINESS DIRECTIVES
Fokker F50 (F27 Mk 50) Series Aeroplanes
AD/F50/62 Lights - Rear Cabin Exit Sign 12/93
Applicability: F27 Mk 050 serial numbers identified in the requirement document. Requirement: Action in accordance with the technical requirements of RLD Airworthiness
Document BLA 93-106 (A).
Note: Fokker Service Bulletin SBF50-33-028 refers.
Compliance: Prior to 11 May 1994.
Background: In some aircraft configurations, the exit sign on the cargo compartment door is obscured from view.
Overview
The Civil Aviation Regulations 1998, enacted by the Australian Parliament, establish the legal framework for the regulation of civil aviation in Australia. Among its various provisions, Part 39 - 105 Civil Aviation Safety Authority Schedule of Airworthiness Directives addresses specific airworthiness directives for aircraft types to ensure safety and compliance. One such directive, AD/F50/62, pertains to the Fokker F50 (F27 Mk 50) Series Aeroplanes, specifically targeting the rear cabin exit sign. This directive was introduced to address the problem of obscured exit signs in certain aircraft configurations, which could potentially compromise safety during an emergency. The policy objective behind this directive is to ensure that all aircraft maintain adequate visibility of emergency exit signs to facilitate safe evacuation. Compliance with this directive was mandated prior to 11 May 1994, in accordance with the technical requirements outlined in RLD Airworthiness Document BLA 93-106 (A) and Fokker Service Bulletin SBF50-33-028.
Scope and Application
The Civil Aviation Regulations 1998, specifically Part 39 - 105, encompasses the scope of airworthiness directives issued by the Civil Aviation Safety Authority, including AD/F50/62 which pertains to Fokker F50 (F27 Mk 50) Series aeroplanes. This particular directive applies to aircraft with serial numbers as identified in the requirement document and mandates compliance with the technical requirements outlined in RLD Airworthiness Document BLA 93-106 (A). It is imperative for the entities or individuals operating these Fokker F50 series aircraft to ensure that the rear cabin exit sign is modified in accordance with the specified technical standards to enhance visibility, as outlined in Fokker Service Bulletin SBF50-33-028. Compliance with this directive is required prior to 11 May 1994, underscoring the urgency and importance of addressing this safety issue. The regulation's jurisdictional reach is nationally consistent with the Civil Aviation Regulations, and it applies uniformly across the Commonwealth of Australia.
Key Provisions
The main operative sections of the AD/F50/62 regulation (part of the Civil Aviation Regulations 1998) focus on ensuring the airworthiness of Fokker F50 (F27 Mk 50) series aeroplanes by mandating specific actions concerning the rear cabin exit sign. Section (12/93) identifies the applicability of this directive to F27 Mk 050 serial numbers listed in the requirement document. The requirement, outlined in section (Requirement), mandates that actions be taken in accordance with the technical specifications of the RLD Airworthiness Document BLA 93-106 (A). This directive is further referenced in Fokker Service Bulletin SBF50-33-028. The compliance deadline for these modifications was set before 11 May 1994.
The AD/F50/62 regulation imposes several obligations and requirements on the operators and maintainers of the affected Fokker F50 aircraft. These obligations include ensuring that the rear cabin exit sign is installed or modified as specified in the RLD Airworthiness Document BLA 93-106 (A). This involves adhering to the technical requirements set forth in the referenced service bulletin to prevent the exit sign from being obscured in certain aircraft configurations. Operators must verify that the modifications are made by the specified compliance date to maintain the aircraft's airworthiness and ensure the safety of passengers and crew.
Failure to comply with the AD/F50/62 regulation can result in serious consequences. The Civil Aviation Safety Authority (CASA) can impose penalties on operators who do not adhere to the mandated modifications. These penalties can include fines and potential grounding of the aircraft. Additionally, non-compliance could lead to safety risks, which might result in more severe civil or criminal consequences. It is crucial for operators to understand and meet the requirements of this directive to avoid these potential repercussions and to ensure the continued safety and compliance of their operations.