T-45C TS, ADV & IUT ENG-27/ENG-28
Engineering Review
b.
Pulling lever up allows throttle to be moved aft
past approach idle stop (if engaged) or idle stop
(throttle off)
NOTE: The stop lever should be gradually
released while moving the throttle from
APPROACH IDLE to IDLE. The lever should
be pulled again to move the throttle past
APPROACH IDLE stop and IDLE stop to OFF.
7.
FUEL SHUTOFF handle (fwd cockpit only)
Sg 1, fr 8
Engine Controls
a.
Down: permits fuel flow to supply engine and
GTS
b.
Pull up: isolates aircraft fuel system from the
engine and GTS
8.
FUEL CONTROL switch (lever-locked)
Sg 1, fr 9
Engine Controls
a.
NORMAL: selects main fuel control system
b.
MANUAL: selects manual fuel control system
9.
Cockpit indicators
a.
M FUEL advisory light: indicates manual fuel
control system selected
Sg 1, fr 10
Engine Indicators, a-d
b.
ECA advisory light: indicates single-lane ECA
failure
c.
ECA 2 caution light: indicates total engine
control amplifier failure (both lanes)
d.
LP PUMP caution light: indicates engine-driven
low pressure fuel pump failure or clogged low
pressure fuel filter (<35 psi)
e.
ACCEL caution light: indicates initial shot
Sg 1, fr 11
solenoid valve and/or steam ingestion bleed
Engine Indicators, e-j
valve is not in the commanded position
(9-98) Original
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