Which statement is correct for a gas turbine engine with a constant speed propeller and free power turbine when the power setting is decreased I The HP spool speed decreases II The EGT decreases ? Students > orientation
![exemple question 170](https://www.furious-atpl.com/documents/IMG_170.jpg)
The FADEC of a gas turbine engine consists of ?
![exemple question 171](https://www.furious-atpl.com/documents/IMG_171.jpg)
The bypass ratio I is the ratio of inlet air mass flow to exhaust air mass flow II can be determined from the bypass air mass flow and the HP compressor mass flow ?
![exemple question 172](https://www.furious-atpl.com/documents/IMG_172.jpg)
![exemple question 173](https://www.furious-atpl.com/documents/IMG_173.jpg)
![exemple question 174](https://www.furious-atpl.com/documents/IMG_174.jpg)
![exemple question 175](https://www.furious-atpl.com/documents/IMG_175.jpg)
![exemple question 176](https://www.furious-atpl.com/documents/IMG_176.jpg)
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