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                                歐洲航空安全局認證規范定義和縮寫

                                時間:2011-10-20 00:58來源:藍天飛行翻譯 作者:航空 點擊:


                                 
                                ‘External load attaching means’ means the structural components used to attach an external load to an aircraft, including external-load containers, the backup structure at the attachment points, and any quick-release device used to jettison the external load.  
                                 
                                ‘Fault (or) Failure’ means an occurrence which affects the operation of a component, part, or element such that it can no longer function as intended.
                                [Amdt. No.:Def/1]
                                 
                                ‘Fault (or) Failure Accommodation’ means the capability to mitigate, either wholly or in part, the effects of a Fault or Failure.
                                [Amdt. No.:Def/1]
                                 
                                ‘Final take-off speed’ means the speed of the aeroplane that exists at the end of the take-off path in the en-route configuration with one engine inoperative. 
                                 
                                ‘Fireproof.’ With respect to materials, components and equipment, means the capability to withstand the application of heat by a flame, for a period of 15 minutes without any failure that would create a hazard to the aircraft. The flame will have the following characteristics:
                                 
                                Temperature 1100°C ± 80°C
                                 
                                Heat Flux Density 116 KW/m2 ± 10 KW/m2  
                                For materials this is considered to be equivalent to the capability of withstanding a fire at least as well as steel or titanium in dimensions appropriate for the purposes for which they are used.  
                                 
                                ‘Fire-resistant.’ With respect to materials, components and equipment, means the capability to withstand the application of heat by a flame, as defined for ‘Fireproof’, for a period of 5 minutes without any failure that would create a hazard to the aircraft.
                                For materials this may be considered to be equivalent to the capability of withstanding a fire at least as well as aluminium alloy in dimensions appropriate for the purposes for which they are used.  
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