TM 1-1510-225-10
3A-33
on the flight director mode selector panel has been
selected and is engaged.
(c) IAS Mode Annunciator. Illumination
of
the
green
indicated
airspeed
hold
mode
annunciator,
placarded
IAS,
indicates
that
the
indicated airspeed hold mode on the flight director
mode selector panel has been selected and is
engaged.
(d) GS Mode Annunciator. Illumination
of the green glideslope mode annunciator, placarded
GS, indicates that the approach mode on the flight
director mode selector panel has been selected and
has captured the glideslope.
(e) GA Mode Annunciator. Illumination
of the green go-around mode annunciator, placarded
GA, indicates that the GO AROUND switch on the left
power lever or the GA switch on the copilot's control
wheel has been pressed and the go-around mode has
been initiated.
(f) PIT Mode Annunciator. Illumination
of the green pitch mode annunciator, placarded PIT,
indicates that the vertical trim thumbwheel on the
autopilot controller is being operated.
(g) ALTC
Mode
Annunciator.
Illumination of the green altitude hold capture mode
annunciator, placarded ALTC, indicates that the
selected altitude has been captured.
(h) VNAV
Mode
Annunciator.
Illumination of the green vertical navigation mode
annunciator, placarded VNAV, indicates that the
vertical navigation mode on the flight director mode
selector panel has been selected and is engaged.
(i) H / L / N CLB Mode Annunciator.
Illumination of the green high, low, or normal climb
profile mode annunciators, placarded H / L / N CLB,
indicates that the high, low, or normal climb profile
mode on the flight director mode selector panel has
been selected and is engaged.
(j) H / L / N DES Mode Annunciator.
Illumination of the green high, low, or normal descent
profile mode annunciators, placarded H / L / N DES,
indicates that the high, low, or normal descent profile
mode on the flight director mode selector panel has
been selected and is engaged.
(5) Radio Altimeter Digital Altitude Display
and Annunciator. Radio altitude is displayed in the
upper right corner of the EHSI in feet above ground
level.
(6) Radio
Altimeter
Annunciator.
Radio
altimeter operation is indicated by a white RA below
the radio altitude display.
(7) Horizon Line With Heading Scale. The
horizon line displays aircraft pitch and roll attitude with
respect to the earth's horizon.
(8) Airspeed Fast/Slow Or Angle Of Attack
Indicator And Scale. The fast/slow or angle of attack
display is located on the opposite side of the EADI
from the glideslope display, and consists of two
vertical white unfilled diamonds and one white unfilled
circle. The fast/slow scale and indicator will be
displayed when the airspeed is within 10 knots more or
less than the selected hold airspeed. The scale
provides a ± 10 knot airspeed indication range.
(9) Airspeed Fast/Slow or Angle of Attack
Scale Command Bars. If airspeed is the referenced
data, AS will be annunciated on the pointer. If angle of
attack is the referenced data, AN will be annunciated
on the pointer.
(10) Lateral Deviation Scale Annunciator. The
lateral deviation scale annunciator displays LOC to
indicate that localizer information is being provided by
the lateral deviation indicator and scale.
(11) Decision
Height
Annunciator.
The
decision height annunciator, placarded DH, illuminates
when the selected decision height has been reached.
(12) Decision Height Digital Display. The
decision height digital display in the lower right corner
of the EADI indicates selected decision height.
(13) Lateral Deviation Scale. The lateral
deviation scale, located at the bottom center of the
EADI provides a lateral reference for the rising runway
symbol when ILS is selected. As an expanded scale,
it represents 1/2 full-scale deviation as displayed on
the EHSI. When the selected course and aircraft
heading differ by more 105, the left/right sense will be
reversed and BC will be displayed to the left of the
center
diamond
to
indicate
that
back
course
information is being displayed.
(14) Rate Of Turn Scale. The rate and
direction of turn is indicated by the rate turn scale and
pointer and indicator, located at the bottom of the
EADI.
(15) Inclinometer.
Deflection
of
the
inclinometer ball from the center of the inclinometer
tube indicates that the aircraft is in a slipping or
skidding turn depending on turn direction.