Honeywell KAP 140 Pilot's Manual page 69

N
1
080°
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
OR
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 off.
Rev. 1
Apr/02
2
GS GS
ı
UP
DN
REV ALT
KAP 140 AUTOPILOT SYSTEM
Two Axis Operation
3
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
OR
PUSH
G
KAP 140
AP HDG NAV APR
4. The autopilot has completed the turn and is
now established on a 010° heading. Desired
altitude has been reached, altitude hold (ALT)
has been engaged and the aircraft maintains
the reference altitude.
4
GS GS
ı
UP
DN
REV
ALT
61