T-45C TS, ADV & IUT ENG-06
Engine System Malfunctions
2.
Possible surging and chugging
3.
Probable increase in EGT
4.
Loss of airspeed
B.
Verifications: visually check for ice accumulation on intakes/airframe
C.
Effects on flight safety
NOTE: Departure from icing conditions should soon restore the
engine to normal operation.
1.
Engine performance degraded
2.
Engine stall possible
3.
Engine damage possible
Fig 5: LP Pump
IV.
Low pressure fuel pump failure 1.8.1.2.3.1
Failure
A.
Indications
1.
MASTER ALERT flashes
2.
Caution tone sounds
3.
LP PMP caution light illuminates
B.
Verifications--same as indications
C.
Effects on flight safety
1.
High pressure fuel pump cavitation possible
2.
Abrupt throttle movements may cause flameout
3.
Unusual attitudes may cause flameout
Fig 6: Oil Pressure
V.
Oil pressure failure 1.8.1.1.16.1
Failure
A.
Indications
1.
MASTER ALERT flashes
2.
Warning tone sounds
3.
OIL PRESS warning light illuminates
B.
Verifications
NOTE: T-45C is not equipped with oil pressure gauge.
Original (9-98)
Page 6-4
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