A method of presenting an operating status of an aircraft engine, the method comprising: accessing, from a non-transitory computer-readable medium, a first indication indicative of a position of an aircraft engine start switch; accessing, from the non-transitory computer-readable medium, a second indication indicative of an aircraft engine start operating mode, the second indication having been generated based on an analysis of parameters associated with an operating condition of the aircraft engine, wherein the parameters are a rotation speed of the aircraft engine and at least one of an exhaust gas temperature of a combustion chamber of the aircraft engine, a fuel flow of the aircraft engine, an oil pressure of the aircraft engine, an oil temperature of the aircraft engine, an altitude of the aircraft and an air speed of the aircraft, a turbine temperature and a synthesized parameter; upon determining, by a processing unit, based on the first indication and the second indication, that the position of the aircraft engine start switch is an "on" position and the aircraft engine start operating mode is a healthy start which does not require a specific crew action which would have otherwise been required if the starting phase was not progressing normally: causing the display of a first visual indication indicative of the healthy start of the aircraft engine; and upon determining, by the processing unit, based on the first indication and the second indication, that the position of the aircraft engine start switch is an "on" position and the aircraft engine start operating mode is an abnormal start which requires a specific crew action and/or specific crew attention: causing the display of a second visual indication indicative of the abnormal start of the aircraft engine. accessing, from a non-transitory computer-readable medium, a first indication indicative of a position of an aircraft engine start switch; accessing, from the non-transitory computer-readable medium, a second indication indicative of an aircraft engine start operating mode, the second indication having been generated based on an analysis of parameters associated with an operating condition of the aircraft engine, wherein the parameters are a rotation speed of the aircraft engine and at least one of an exhaust gas temperature of a combustion chamber of the aircraft engine, a fuel flow of the aircraft engine, an oil pressure of the aircraft engine, an oil temperature of the aircraft engine, an altitude of the aircraft and an air speed of the aircraft, a turbine temperature and a synthesized parameter; upon determining, by a processing unit, based on the first indication and the second indication, that the position of the aircraft engine start switch is an "on" position and the aircraft engine start operating mode is a healthy start which does not require a specific crew action which would have otherwise been required if the starting phase was not progressing normally: causing the display of a first visual indication indicative of the healthy start of the aircraft engine; and upon determining, by the processing unit, based on the first indication and the second indication, that the position of the aircraft engine start switch is an "on" position and the aircraft engine start operating mode is an abnormal start which requires a specific crew action and/or specific crew attention: causing the display of a second visual indication indicative of the abnormal start of the aircraft engine.