Inbound On Gps Approach Using Dg - Honeywell KAP 140 Manual

Two Axis/Altitude Preselect Operations

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
ARM BARO
KAP 140
UP
DN
AP HDG NAV APR REV ALT
1. Continuing the maneuver on page 104,
mode capture occurs. The autopilot initiates a
left turn to track the 058° GPS course.
* Approach active is indicated on the GPS
annunciator.
108 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
ARM BARO 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. 2
May/02
Two Axis/Altitude Preselect Operations
FAF
R L
TO
GS
FR
OBS
PUSH
ı
ARM BARO
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 and vertical speed modes, commencing a
right turn to a heading of 090° and maintaining
the rate of climb existing at engagement.
Note: Press and hold the
seconds to engage the autopilot (applicable
only to software version 03/01 and later).
KAP 140 AUTOPILOT SYSTEM
D.C. ELEC.
TURN COORDINATOR
R
2 MIN.
NO PITCH
INFORMATION
TO
GS
FR
OBS
ı
G
ARM BARO
KAP 140
UP
DN
AP HDG NAV APR REV ALT
HDG
button on the
AP
button for 0.25
109