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

Single 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
AP HDG NAV APR REV
1. The aircraft is well off the ground and estab-
lished at a desired 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 mode
and maintains the selected heading of 080°.
AP
Note: Press and hold the button for 0.25
seconds to engage the autopilot (applicable
only to software version 03/01 and later).
32
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
AP HDG NAV APR REV
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.
Note: The autopilot controls only the roll axis. The PILOT must maintain control of
the pitch and yaw axis.
Rev. 1
Apr/02
1 2
080°
L
R
GS GS
OR
PUSH
ı
HDG NAV APR REV
4. The autopilot has completed the turn and is
now established on a 010° heading.
KAP 140 AUTOPILOT SYSTEM
Single Axis Operation
3 4
D.C. ELEC.
TURN COORDINATOR
R
2 MIN.
NO PITCH
INFORMATION
GS GS
OR
ı
G
KAP 140
AP HDG NAV APR REV
33