Outbound On Gps Approach Using Dg - Honeywell KAP 140 Manual

Two Axis/Altitude Preselect Operations

Outbound on GPS Approach 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
APR
1. The aircraft is in mode approaching the
IAF. Approach arm is indicated on the GPS
annunciator.*
104 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
2. Upon waypoint alerting at the IAF, the heading
bug is set to 238°, the GPS's Leg/OBS mode
switching is set to OBS mode and the OBS is
set to 238°. The autopilot initiates a left turn to
track the 238° GPS course.
Rev. 1
Apr/02
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
3. At the desired point, heading mode is used to
initiate the procedure turn. During the procedure
turn outbound, the deviation bar shows that the
aircraft is flying away from the GPS course at a
45° angle on a selected heading of 283°.
* Check the heading displayed on the DG against
the magnetic compass and reset if necessary.
Rev. 1
KAP 140 AUTOPILOT SYSTEM
Apr/02
Two Axis/Altitude Preselect Operations
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
GS
OBS
PUSH
ı
G
ARM BARO
KAP 140
UP
DN
AP HDG NAV APR REV ALT
4. The heading bug has been set to 103° and the
aircraft has made a left turn to this heading.
The GPS's Leg/OBS mode switching is set to
Leg mode and the OBS is set to 058°. Select
APR
approach mode by depressing the
HDG
*The annunciation will flash for five sec-
HDG
onds then extinguish. While the annuncia-
tion is flashing, move the heading bug to 058°.
Since the 45° intercept is 103°, the aircraft will
not turn until the course is captured.
TO
FR
button.
105