Inbound On Gps Approach Using Dg - Honeywell KAP 140 Manual

Single 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
AP HDG NAV APR REV ALT
1. Continuing the maneuver on page 46,
mode capture occurs. The autopilot initiates a
left turn to track the 058° GPS course.
Approach active is indicated on the GPS
annunciator.*
50
KAP 140 AUTOPILOT SYSTEM
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
GS
OBS
PUSH
G
KAP 140
AP HDG NAV APR REV ALT
APR
2. The autopilot is following the GPS course. The
autopilot will make the bank changes as neces-
sary to maintain the GPS course.
Apr/02
D.C. ELEC.
TURN COORDINATOR
L
2 MIN.
NO PITCH
INFORMATION
TO
FR
PUSH
ı
G
KAP 140
AP
3. At the missed approach point, the pilot disen-
gages the autopilot with the button on the con-
trol wheel. This cancels all operating modes.
The flashing
a disconnect tone will sound.
Rev. 1 Rev. 1
Apr/02
FAF
R L
TO
GS
FR
OBS
PUSH
ı
HDG NAV APR REV ALT
4. The pilot initiates the missed approach and sta-
bilizes the aircraft in the climb. The heading
bug is set to the missed approach heading of
AP
090°. By depressing the HDG button on the
annunciations are displayed and
KAP 140, the autopilot engages into the head-
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
Single Axis Operation
D.C. ELEC.
TURN COORDINATOR
R
2 MIN.
NO PITCH
INFORMATION
TO
GS
FR
OBS
ı
G
KAP 140
AP HDG NAV APR REV ALT
AP
button for 0.25
51