A simulation evaluation of the engine monitoring and control system displayNational Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990 - Airplanes - 35 pages |
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16 Number aircraft engine Aircraft Simulator caution area caution region cockpit control and monitoring control engine Critical Engine Parameters current thrust value degraded conditions detect degraded deviation column digital presentation digital readout display format allowed E-MACS display relative easier EICAS engine control engine display format Engine Monitoring EPR dial EPR pointer EPR predictor EPR reference EPR warning Extremely Fairly easy Fairly easy easy Figure find the display inflight scenarios Initial Subjective Evaluation Langley Research Center left engine maximum-continuous modern display 16 Modern format Modern No Advanced monitoring task NASA normal operations Number of 12 Number of responses oil pressure OIL TEMPERATURE operating limits operating range operational conditions out-of-tolerance conditions percent performance power setting quantitative evaluation quantitative test questionnaire range marker reference value Responses to question responses with modern set engine power takeoff task thrust indicator Thrust predictor traditional display turbofan U.S. Air Force warning region