Gps Capture Using Dg - Honeywell KAP 140 Manual

Two Axis/Altitude Preselect Operations

GPS Capture Using DG

* Description of GPS operation based on Bendix/King GPS receiver. Others may
require different operation.
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
TO
GS
FR
OBS
PUSH
ı
G
ARM BARO
KAP 140
UP
DN
AP HDG NAV APR REV ALT
1. Continuing on heading 010°, a GPS waypoint is
established. A 30° intercept is desired.
92 KAP 140 AUTOPILOT SYSTEM
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
TO
GS
FR
OBS
PUSH
ı
G
ARM BARO
KAP 140
UP
DN
AP HDG NAV APR REV ALT
HDG
2. The button is depressed to select
mode which will allow an "all angle intercept".
GPS data is selected for the CDI and the OBS is
NAV
set to 040°. The button is depressed and
NAV ARM ROL
is annunciated. will change to
HDG ROL
and flash for five seconds. will then
HDG
be redisplayed. While the annunciation is
flashing, move the heading bug to the desired
course of 040°. The aircraft will remain wings
level until the capture point.
Rev. 1
Apr/02
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
PUSH
G
KAP 140
AP HDG NAV
ROL
3. When the computed capture point is reached,
ROL
the annunciation changes to
right turn is initiated by the autopilot.
Rev. 1
Apr/02
Two Axis/Altitude Preselect Operations
D.C. ELEC.
TURN COORDINATOR
L
2 MIN.
NO PITCH
INFORMATION
TO
GS
FR
OBS
PUSH
ı
G
ARM BARO
KAP 140
UP
DN
APR REV ALT AP
4. The turn is complete and the autopilot is track-
NAV
and a ing the GPS course.
KAP 140 AUTOPILOT SYSTEM
R
TO
GS
FR
OBS
ı
ARM BARO
UP
DN
HDG NAV APR REV ALT
93