Honeywell KAP 140 Pilot's Manual page 81

D.C. ELEC.
TURN COORDINATOR
L
NO PITCH
INFORMATION
GS
ı
G
KAP 140
AP HDG NAV APR
3. At the middle marker, the pilot disengages the
autopilot with the button on the control wheel.
This cancels all operating modes. The flashing
AP annunciations are displayed and a discon-
nect tone will sound.
Rev. 1
Apr/02
R
2 MIN.
GS
UP
DN
REV
ALT
KAP 140 AUTOPILOT SYSTEM
Two Axis Operation
D.C. ELEC.
TURN COORDINATOR
L
2 MIN.
NO PITCH
INFORMATION
GS
ı
G
KAP 140
AP HDG NAV APR
4. The pilot initiates the missed approach and sta-
bilizes the aircraft in the climb. The heading
bug is set to the missed approach heading of
090°. By depressing the HDG button on the
KAP 140, the autopilot engages into the head-
ing and vertical speed modes, commencing a
right turn to a heading of 090° and maintaining
the rate of climb existing at engagement.
Note: Press and hold the AP button for 0.25
seconds to engage the autopilot (applicable
only to software version 03/01 and later).
R
GS
UP
DN
REV
ALT
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