Honeywell BENDIX/KING KAP 140 Maintenance Manual page 52

Flight control system
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ITEM
APR Switch
REV Switch
ALT Switch
UP Switch
DN Switch
ALT ARM Switch
BARO Switch
INC/DEC Inner Knob
Revision 2, Dec/2002
CS:15574F02
BENDIX/KING
KAP 140
DESCRIPTION
Momentary pushbutton on front panel of the FCC
used to engage/disengage Approach Arm and
Tracking mode. 'YES' implies switch is pressed.
'NO' implies switch is not pressed.
Momentary pushbutton on front panel of the FCC
used to engage/disengage Reverse Localizer
Tracking mode. 'YES' implies switch is pressed.
'NO' implies switch is not pressed.
Momentary pushbutton on front panel of the FCC
used to engage/disengage Alt Hold mode. 'YES'
implies switch is being pressed. 'NO' implies switch
is not pressed.
Momentary pushbutton on front panel of the FCC
used to change vertical speed or altitude reference
to cause aircraft to nose upward.
switch is pressed. 'NO' implies switch is not pressed.
Momentary pushbutton on front panel of the FCC
used to change vertical speed or altitude reference
to cause aircraft to nose downward. 'YES' implies
switch is pressed. 'NO' implies switch is not pressed.
Momentary pushbutton on front panel of the FCC
used to engage/disengage Altitude Arm mode.
'YES' implies switch is being pressed. 'NO' implies
switch is not pressed.
Momentary pushbutton on front panel of the FCC
used with rotary knobs to adjust baro setting. Also
toggles baro units between hPa and Hg.
implies switch is pressed. 'NO' implies switch is not
pressed.
Rotary switch used to adjust baro setting by 0.01 in
Hg / 10 hPa increments or change selected altitude
in 100 ft steps.
diagnostic screen represents the current position of
the switch. As the switch is rotated clockwise the
value will change according to the sequence 0, 2, 3,
1, 0, 2, 3, 1 and continue to repeat.
counter--clockwise rotation will produce the reverse
sequence 0, 1, 3, 2, 0, 1, 3, 2 and repeat.
'YES' implies
The value displayed on the
Page 3--8
'YES'
A

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