Two axis/altitude preselect operations, Two axis/altitude preselect operations 98 99, Kap 140 autopilot system – BendixKing KAP 140 User Manual

Page 80

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KAP 140 AUTOPILOT SYSTEM

Two Axis/Altitude Preselect Operations

Two Axis/Altitude Preselect Operations

98

99

KAP 140 AUTOPILOT SYSTEM

Rev. 1
Apr/02

Rev. 1

Apr/02

3. At the desired point, H

DG mode is used to initi-

ate the procedure turn. During the procedure
turn outbound, the deviation bar shows that the
aircraft is flying away from the localizer center-
line at a 45° angle on a selected heading of
283°.

4. Now you have reset the heading bug to 103°

and made a 180° turn to this heading. The
103° heading will intercept the front course of
058°. You must now select the approach mode
by depressing the

APR button on the KAP 140.

Automatic capture of the localizer will occur.

L

R

2 MIN.

TURN COORDINATOR

NO PITCH

INFORMATION

D.C. ELEC.

GS

GS

N

33

30

W

24

2

1

S

15

12

E

6

3

ı

AP

G

KAP 140

HDG

NAV

APR

REV

ALT

DN

UP

ARM

BARO

L

R

2 MIN.

TURN COORDINATOR

NO PITCH

INFORMATION

D.C. ELEC.

GS

GS

N

33

30

W

24

21

S

15

12

E

6

3

ı

AP

G

KAP 140

HDG

NAV

APR

REV

ALT

DN

UP

ARM

BARO

N

1

2

3

4

270

°

058

°

238

°

283°

103°

1. The aircraft is heading 270° with heading and

altitude hold engaged. To intercept and fly the
ILS front course outbound, set the front course
on the HSI and depress the back course (

REV)

button. The back course (

REV) mode is

selected to go outbound on the front course.
The capture point is now being computed
based on closure rate.

2. When the computed capture point is reached,

HDG mode is cancelled and reverse localizer

mode is automatically activated and a left turn
outbound on the localizer is initiated by the
autopilot.

Note: The left-right deviations of the HSI course

needle operate just as though you were flying a

front course approach

.

Outbound On Front Course For Procedure Turn To ILS Approach Using HSI

L

R

2 MIN.

TURN COORDINATOR

NO PITCH

INFORMATION

D.C. ELEC.

GS

GS

N

33

30

W

24

21

S

15

12

E

6

3

ı

AP

G

KAP 140

HDG

NAV

APR

REV

ALT

DN

UP

ARM

BARO

L

R

2 MIN.

TURN COORDINATOR

NO PITCH

INFORMATION

D.C. ELEC.

GS

GS

N

33

30

W

24

21

S

15

12

E

6

3

ı

AP

G

KAP 140

HDG

NAV

APR

REV

ALT

DN

UP

ARM

BARO

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