Engine Start Procedures
T-45A UJPT, E2-C2, ADV, & IUT Eng-24
PRESENTATION
I.
Engine start controls and indicators 1.4.1.1.2.1,
Sg 1, fr 1
Lesson Organization
1.4.1.1.2
LECTURE NOTES
Refer students to NATOPS graphic foldouts, T-45A
FORWARD COCKPIT (FO-3 and/or FO-4) throughout
this lesson.
A.
Controls
Sg 1, fr 2
1.
IGNITION switch
a.
Location: left console, aft of throttle,
fwd cockpit only
b.
Description: two-position switch
marked IGNITION - NORMAL/
ENGINE CONTROLS (FWD COCKPIT)
ISOLATE
Sg 1, fr 3
(1) NORMAL (guarded): controls
electrical power supply to ignition
system (both GTS igniter and
engine igniters)
(2) ISOLATE: deenergizes ignition
system (both GTS and engine)
NOTE: Battery switches must be
IGNITION AND ENGINE SWITCHES
on or external power must be
applied to the aircraft for power to
be present on the 28 VDC
essential services bus.
(8-03) Original
Page 24-3
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