T-45C TS, ADV & IUT ENG-27/ENG-28
Engineering Review
CORRECT ROTATION
INDICATION
RPM
EGT
THROTTLE
EGT/RPM
N1
N2
AIRCRAFT
ENGINE
START
CONTROL
CONTROL
AMPLIFIER
UNIT
RPM
EGT
HP
THERMOCOUPLE
OVERSPEED
JUNCTION BOX
FUEL
GOVERNOR
CONTROL
UNIT
HP FUEL PUMP
TO IGNITION
SYSTEM
T2
P
P1
T
6
0
LEGEND
CONTROL SIGNAL
CONDITION SIGNAL
INDICATION SIGNAL
FUEL
AIR
Figure 3: BASIC ENGINE BLOCK DIAGRAM
(9-98) Original
Page 27-153
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