Honeywell KAP 140 Pilot's Manual page 99

N
1
080°
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
PUSH
G
KAP 140
AP HDG NAV APR
3. The autopilot is responding to the heading select
mode with a left bank. The climb rate has been
decreased, using the DN button, in preparation
for level out. The vertical speed value will be
displayed upon selection of the DN button and
will remain for three seconds.
Rev. 1
Apr/02
2
GS GS
OR
ı
ARM BARO
UP
DN
REV ALT
KAP 140 AUTOPILOT SYSTEM
Two Axis/Altitude Preselect Operations
3
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
PUSH
G
KAP 140
AP HDG NAV
4. Desired altitude has been reached and auto-
matic altitude capture occurs. The autopilot has
completed the turn and is now established on a
010° heading.
4
GS GS
OR
ı
ARM BARO
UP
DN
APR REV
ALT
91