T-45C TS, ADV & IUT EMFP-05
Engine and Hydraulic Emergency Procedures
2.
Increase airspeed and reduce altitude with throttle at
idle if rpm stagnates at 30 to 40% during satisfactory
relight at high altitude low airspeed
XII. Recall procedures for Engine Vibrations 1.8.1.1.10.2
A. Indications
1.
Feel vibration in airframe
2.
Possible increase in EGT and decrease in rpm
B. Procedures - Refer to Part V, Chapter 15, In-Flight
Emergencies, of the T-45C NATOPS
XIII. Recall procedures for Oil Pressure Failure 1.8.1.1.16.2
A. Indications
1.
OIL PRESS warning illuminates
2.
Warning tone sounds
3.
MASTER ALERT flashes
4.
Possible aircraft vibrations if malfunction associated
with bearing failure
5.
Possible engine overtemp
6.
Wingman may see leaking oil or excessive
exhaust smoke
B. Procedures - Refer to Part V, Chapter 12, General
Emergencies, of the T-45C NATOPS
XIV. Recall procedures for GTS Fire (in flight) 1.8.1.1.11.2
A. Indications
1.
GTS FIRE warning illuminates
2.
Warning tone sounds
Original (9-98)
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