T-45C TS, ADV & IUT ENG-27/ENG-28
Engineering Review
(2) Uses transmitter/antenna and receiver/
antenna to send signals to the ADR then to
DEU for display readout on the MFD (ADI)
and the HUD
b.
Standby attitude indicator: self-contained, two
Sg 11, fr 34a
colored moving drum indicating aircraft attitude
Standby Attitude
(accurate to 90 degrees nose up and 78
Indicator
degrees nose down in pitch, and 360 degrees in
roll) via an adjustable aircraft symbol
Sg 11, fr 35
c.
Standby turn and slip indicator: self-contained
Standby Turn and Slip
gyro driven rate of turn/slip indicator, with a
Indicator
power warning flag
d.
Standby compass: conventional wet compass
Sg 11, fr 37a
suspended in damping fluid used as a backup
Standby Compass
for heading
Sg 11, fr 37b
e.
Clock: combined mechanical clock/stopwatch
Clock/Stopwatch
with hands for hours, minutes, seconds, and
time elapsed
6.
Standby compass
a.
Location: mounted at top of each canopy bow
b.
Function: conventional wet compass
suspended in damping fluid used as a backup
for heading
(1) Contains compass card graduated in
5 degree divisions with cardinal headings
indicated as N, S, E, and W
(2) Compass card floats horizontally within
case to align itself with earth’s magnetic
field
(3) Magnetic heading read off card under
lubber line engraved upon lens
(4) Two internal bar magnets compensate for
deviation
(9-98) Original
Page 27-107
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