Front Course Ils Approach Using Hsi - Honeywell KAP 140 Manual

Two Axis/Altitude Preselect Operations

Front Course ILS Approach Using HSI

D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
GS GS
ı
G
ARM BARO
KAP 140
UP
DN
AP HDG NAV APR REV ALT
1. Continuing the maneuver on page 98, APR cou-
HDG
pling occurs ( annunciation changes to
APR
), and the glideslope mode is automatically
armed. The autopilot will capture the localizer
and the CDI course index will center.
102 KAP 140 AUTOPILOT SYSTEM
D.C. ELEC.
TURN COORDINATOR
L R
2 MIN.
NO PITCH
INFORMATION
GS GS
ı
G
ARM BARO
KAP 140
UP
DN
AP HDG NAV APR REV ALT
2. The autopilot is following the localizer. At the
outer marker, the glideslope deviation needle is
at midscale. Altitude hold is automatically disen-
gaged when the glideslope is captured. The
GS
annunciation extinguishes and is displayed.
The autopilot will make pitch and bank changes
as necessary to maintain localizer and glides-
lope.
Rev. 1
Apr/02
TURN COORDINATOR
L
GS
G
KAP 140
AP HDG NAV
3. At the middle marker, the pilot disengages the
autopilot with the button on the control wheel.
This cancels all operating modes. The flashing
ALT
AP
annunciations are displayed and a discon-
nect tone will sound.
Rev. 1
Apr/02
Two Axis/Altitude Preselect Operations
D.C. ELEC.
R
2 MIN.
NO PITCH
INFORMATION
GS
ı
G
ARM BARO
KAP 140
UP
DN
APR REV ALT AP
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
090°. By depressing the
KAP 140, the autopilot engages into the head-
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
L R
2 MIN.
NO PITCH
INFORMATION
GS GS
ı
ARM BARO
UP
DN
HDG NAV APR REV ALT
HDG
button on the
AP
button for 0.25
103