SAE ARP5119-1999
用于大角度接近IMC(集成市场通讯)的下视电子飞行显示器的位置和显示器符号要求

Location of and Display Symbology Requirements for Head-Down Electronic Flight Displays for Steep IMC Approaches

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标准号

SAE ARP5119-1999

发布

1999年

发布单位

美国机动车工程师协会

替代标准

SAE ARP5119-2013

当前最新

SAE ARP5119A-2020

 

 

引用标准

SAE ARD 50018-1995 SAE ARP1068 SAE ARP1093 SAE ARP1874-1988 SAE ARP268 SAE ARP4032-1988 SAE ARP4033-1995 SAE ARP4067-1989 SAE ARP41 SAE ARP4102-1988 SAE ARP4102/2-1988 SAE ARP4102/4-1988 SAE ARP4102/7-1988 SAE ARP4102/8-1988 SAE ARP4104-1988

适用范围

The recommendations of this document apply to such aircraft as are able to perform both normal angle and steep IMC approaches, the latter being defined as those approaches having a final approach segment angle greater than 4? Such aircraft can include both conventional and STOL fixed-wing aircraft, commercial air transport and/or utility and normal category helicopters, compound helicopters and powered lift vehicles (tiltrotors, tiltfans, tiltwings, etc.). The purpose of this document is to set forth the recommendations of SAE Committee G-10 Vertical Flight Subcommittee relative to the location, control, and implementation of electronic flight information systems, primary flight displays, secondary (standby flight) displays, engine and instruments displays, crew alert displays and associated required flight deck/cockpit displays. These recommendations are intended to derive intuitive and easily interpretable displays and display locations to minimize confusion, distraction and fatigue, thereby reducing crew workload and increasing crew performance, efficiency, safety and reducing factors detrimental to flight safety. In arriving at these recommendations the committee carefully reviewed the layouts of modern commercial and military aircraft, developmental tiltrotor flight deck/cockpit layouts, the recommendations and requirements of the Federal Aviation Administration Aircraft Certification branch and the requirements of commercial operators and aircraft manufacturers. In cases where conflicting opinions existed, suitable compromises were made. This document applies to all electronic flight instrument display systems, including but not limited to liquid crystal displays (LCD), field emitting diodes (FED), light emitting diodes (LED) or cathode ray tube (CRT) technology.

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