What are the power and thrust increases when moving the throttle from MIL to MAX?
50% thrust increase for 300% fuel flow increase
What area is not stall/flameout prone?
Above Mach 0.6 and 28,000’
In what area can maneuvers with rapid climbs and decelerations with rapid throttle movement and AB cancellation increase compressor stall potential?
Above 15,000’ pressure altitude and 200 KCAS
What is T2 cutback?
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What is EGT droop?
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What happens at high altitude and low airspeed?
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