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公开(公告)号:EP3356231B1
公开(公告)日:2020-08-12
申请号:EP16781562.0
申请日:2016-09-22
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公开(公告)号:EP3356231A1
公开(公告)日:2018-08-08
申请号:EP16781562.0
申请日:2016-09-22
摘要: A method of and a system for presenting an operating status of an aircraft engine. The method comprises accessing a first indication indicative of a position of an aircraft engine start switch and accessing a second indication indicative of an aircraft engine start operating mode, the second indication having been generated based on an analysis of a parameter associated with an operating condition of the aircraft engine. The method, upon determining that the position of the aircraft engine start switch is an “on” position and the aircraft engine start operating mode is a healthy start causes the display of a visual indication indicative of the healthy start. The method upon determining that the position of the aircraft engine start switch is an “on” position and the aircraft engine start operating mode is an abnormal start causes the display of a visual indication indicative of the abnormal start.
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