T-45C TS, ADV & IUT ENG-05
Engine and Related Systems Malfunctions
3. Decreasing rpm
4. As rpm decreases, MASTER ALERT flashes
5. Warning/caution tone sounds
6. Appropriate warning and caution advisory panel lights illuminate
a. GENERATOR warning light
b. F PRES caution light
c.
OIL PRESS warning light
d. HYD 1 caution light (windmilling engine may prevent light from
illuminating)
e. HYD 2 caution light
f.
C AUG caution light
g. OXYGEN warning light
h. CABIN ALT warning light (if altitude < 24,500 ft MSL)
i.
RAT caution light (when RAT extends)
C.
Effects on flight safety
1. During airstart procedure, altitude and/or airspeed lost
2. After airstart, engine performance may be degraded
IX. ECA failure (full trim) 1.8.1.1.9.1.1
NOTE: Loss of one of the dual ECA systems/lanes will cause the ECA
advisory light to illuminate with no loss of performance. Loss of both ECA
systems/lanes will cause the ECA advisory light and the ECA-2 caution light
to illuminate, and you will lose automatic overspeed/overtemp control of the
engine.
A. Indications
1. ECA advisory light
2. MASTER ALERT light
3. Caution tone sounds
4. ECA 2 caution light
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