Introduction to T-45C Configuration
T-45C TS, ADV & IUT ENG-01
O.
Environmental control system (ECS) 1.4.15.3.1.1
Sg 3, fr 18
Fig 16: Environmental
1.
Description: consists of the air conditioning system,
Control System
the cockpit pressurization system, and the avionics
equipment cooling system
2.
Function
a.
Converts engine compressor bleed air to
conditioned air and distributes it to cockpit
ventilation, pressurization, and defog systems
b.
Provides cooled bleed air to avionics bay for
equipment cooling
3.
Control location: right console, aft of interior
lights control panel, fwd cockpit only
P.
Flight instruments 1.4.5.3.1.1
Sg 3, fr 19
Flight Instruments
1.
Description: consist of airspeed, vertical speed,
compass, altimeter, and attitude indicating systems
Fig 19: Display and
System Controls
2.
Function
a.
Provide primary flight performance data
b.
Provide navigation information
c.
Provide backup instrumentation
3.
Control location: throughout cockpit with associated
system operation
4.
Indication location: on center instrument panel
a.
AOA indicator
b.
AOA indexer
c.
Airspeed indicator
d.
Multi function display (MFD)
(9-98) Original
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