T-45C TS, ADV & IUT ENG-19
Flight Instruments
3.
Pitot static system signals
a.
Static air pressure ratios: standby airspeed,
VSI, and altimeter
b.
Ram air pressure information: standby
airspeed
c.
Airspeed and altitude information to HUD, DEU,
MFD
4.
Acceleration from ADR
a.
Vertical positive-g load
b.
Vertical negative-g load
Sg 3, fr 5
B.
Systems interface
ADR Inputs
1.
Airborne data recorder (ADR): monitors structural
fatigue of aircraft, engine parameters, and following
flight instrument-related information
a.
Airspeed
b.
Mach number
c.
Altitude (barometric and radar)
d.
Pitch and bank
e.
Heading
f.
NOTE: This is only a partial listing of items
monitored by the ADR.
Sg 3, fr 6
2.
HUD system: presents the following information
HUD Indications
from various pertinent aircraft systems and
instruments via the display electronic unit (DEU) to
Fig 13: HUD
the pilot display unit (PDU) on the HUD
Original (9-98)
Page 19-30
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