T-45C TS, ADV & IUT ENG-27/ENG-28
Engineering Review
(2) Ram air pressure information: standby
airspeed
(3) Airspeed and altitude information to HUD,
DEU, MFD
d.
(1) Vertical positive-g load
(2) Vertical negative-g load
2.
Systems interface
a.
Airborne data recorder (ADR): monitors
Sg 11, fr 20
structural fatigue of aircraft, engine parameters,
ADR Inputs
and following flight instrument-related
information
(1) Airspeed
(2) Mach number
(3) Altitude (barometric and radar)
(4) Pitch and bank
(5) Heading
(6) Acceleration
NOTE: This is only a partial listing of items
monitored by the ADR.
b.
HUD system: presents the following
Sg 11, fr 21
HUD Indications
information from various pertinent aircraft
systems and instruments via the display
electronic unit (DEU) to the pilot display unit
(PDU) on the HUD: pitch, roll, heading, AOA,
altitude, barometric and radar, airspeed, KIAS,
TAS, and Mach, G load and Peak G, and
vertical speed
(9-98) Original
Page 27-104
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