Inbound On Gps Approach Using Dg - Honeywell KAP 140 Manual

Two Axis Operation

Inbound 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
KAP 140
UP
DN
AP HDG NAV APR REV ALT
1. Continuing the maneuver on page 74,
mode capture occurs. The autopilot initiates a
left turn to track the 058° GPS course.
* Approach active is indicated on the GPS
annunciator.
78
KAP 140 AUTOPILOT SYSTEM
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
GS
OBS
PUSH
G
KAP 140
UP
DN
AP HDG NAV APR REV ALT
APR ALT
2. At the FAF, is depressed to activate vertical
speed mode. The desired descent rate is
DN
obtained using the button.
Remember, speed needs to be controlled with
the throttle.
Apr/02
D.C. ELEC.
TURN COORDINATOR
L
2 MIN.
NO PITCH
INFORMATION
TO
FR
PUSH
ı
G
KAP 140
AP
3. At the MDA, the
ing the autopilot to level off and maintain a con-
stant altitude. At the MAP the pilot disengages
the autopilot with the button on the control
wheel. A flashing
and a distinctive tone will sound.
Rev. 1 Rev. 1
Apr/02
FAF
R L
TO
GS
FR
OBS
PUSH
ı
UP
DN
HDG NAV APR REV ALT
ALT
4. The pilot initiates the missed approach and sta-
button is depressed caus-
bilizes the aircraft in the climb. The heading
bug is set to the missed approach heading of
090°. By depressing the
AP
KAP 140, the autopilot engages into the head-
annunciation is displayed
ing mode, commencing a right turn to a head-
ing of 090°.
Note: Press and hold the
seconds to engage the autopilot (applicable
only to software version 03/01 and later).
KAP 140 AUTOPILOT SYSTEM
Two Axis Operation
D.C. ELEC.
TURN COORDINATOR
R
2 MIN.
NO PITCH
INFORMATION
TO
GS
FR
OBS
ı
G
KAP 140
UP
DN
AP HDG NAV APR REV ALT
HDG
button on the
AP
button for 0.25
79