T-45A UJPT, E2-C2, ADV, & IUT Eng-19
Flight Instruments
3.
Pitot static system signals
a.
Static air pressure ratios: airspeed,
VSI, and altimeter
b.
Ram air pressure information:
airspeed
c.
Airspeed and altitude information to
HUD system
4.
Acceleration/accelerometer
a.
Vertical positive-g load
b.
Vertical negative-g load
B.
Systems interface
Sg 7, fr 4
1.
Airborne data recorder (ADR): monitors
structural fatigue of aircraft, engine
parameters, and following flight instrument-
related information
a.
Airspeed
ADR INPUTS
b.
Mach number
c.
Altitude (barometric and radar)
d.
Pitch and bank
e.
Heading
f.
g.
Elapsed time
h.
AOA
i.
Total air temperature
(1) Sensor located on ports side just
in front of canopy
Page 19-32
(8-03) Original
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