Operations With The Kap 140; Takeoff And Climb To Assigned Altitude - Honeywell KAP 140 Manual

Two Axis Operation

OPERATIONS WITH THE KAP 140

Takeoff And Climb To Assigned Altitude

1
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
GS
OR
PUSH
ı
G
KAP 140
UP
DN
AP HDG NAV APR REV ALT
1. The aircraft is well off the ground and estab-
lished at a safe climb rate.
The heading bug on the DG or HSI is turned to
the desired heading of 080° (runway heading).
HDG
By depressing the button on the KAP 140,
the autopilot engages into the heading and ver-
tical speed modes and maintains the selected
heading of 080° and current rate of climb.
AP
Note: Press and hold the button for 0.25
seconds to engage the autopilot (applicable
only to software version 03/01 and later).
60
KAP 140 AUTOPILOT SYSTEM
2 3
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
GS GS
OR
PUSH
G
KAP 140
UP
DN
AP HDG NAV APR REV ALT
2. The heading bug on the DG or HSI is turned to
the new desired heading of 010° and the aircraft
begins to respond with an immediate left turn.
Rev. 1
Apr/02
N
4
D.C. ELEC.
TURN COORDINATOR
L
2 MIN.
NO PITCH
INFORMATION
GS
PUSH
ı
G
KAP 140
AP
3. The autopilot is responding to the heading select
mode with a left bank. The climb rate has been
decreased, using the
for level off.
Rev. 1
Apr/02
1 2
080°
L
R
GS GS
OR
PUSH
ı
UP
DN
HDG NAV APR REV ALT
4. The autopilot has completed the turn and is
now established on a 010° heading. Desired
DN
button, in preparation altitude has been reached, altitude hold (
has been engaged and the aircraft maintains
the reference altitude.
KAP 140 AUTOPILOT SYSTEM
Two Axis Operation
3 4
D.C. ELEC.
TURN COORDINATOR
R
2 MIN.
NO PITCH
INFORMATION
GS GS
OR
ı
G
KAP 140
UP
DN
AP HDG NAV APR REV ALT
ALT
)
61