BendixKing KLX 135A Quick Reference Guide

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BendixKing KLX 135A Quick Reference Guide

Quick Reference KLX 135A

B

GPS/COMM

These simplified operating instructions are only to familiarize you with the

KLX 135A. For detailed operating instructions, please refer to the

KLX 135A Pilot's Guide P/N 006-08789-0000.

B

 

 

 

 

KLX 135

VOL

Pull

118®00

 

∂∆ KOSH

 

TEST

 

 

OFF

 

136.97 > ««««∫∏π««««

 

 

 

 

 

 

 

 

 

>Leg

 

89.6nm

105kt

CRSR

 

 

 

 

COMM

 

NAV 1

>345°To

0:51

GPS

 

 

 

 

 

 

Pull

APT VOR NDB

SUP ACT NAV FPL

CAL SET OTH

Pull

 

25K

MSG

D

CLR

ENT

SCAN

 

 

 

GPS

The two concentric knobs and functions of the KLX 135A. should be pushed in.

Bbutton on the right are used to control the GPS The right inner knob can be pulled out, but for now it

When the cursor is off

 

, the right outer knob changes the page type (APT to VOR to

NDB, etc.) and the right inner knob changes the page number (APT 1 to APT 2).

When the cursor is on

 

, the right outer knob moves the cursor and the right inner knob

changes the data under the cursor.

 

To change a cyclic field:

1.

Turn on the cursor (by pressing the

Bbut-

 

ton) and place it over a cyclic field, which is

 

always preceded by a carat (>).

 

2.

Press the

Ebutton to change the cyclic

 

field. One example is the NAV 1 page, which

 

can display a D-bar (Figure 1) or numerical

 

course deviation (Figure 2).

 

To display the Nearest Airport:

 

1.

Press

Cthen press

Ftwice .

118®00

 

 

 

 

∂∆ KOSH

 

 

 

 

 

 

136.97

>

««««∫∏π««««

 

 

 

 

 

>Leg

 

 

89.6nm

105kt

 

 

 

 

 

 

NAVCRSR1

 

 

>345°To

0:51

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

APT VOR NDB SUP ACT NAV FPL CAL SET OTH

 

MSG

D

 

 

 

CLR

ENT

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Figure 1

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

118.00

 

 

 

 

∂∆ KOSH

 

 

 

 

 

 

136.97

>

Fly L

1.1nm

 

 

 

 

>Leg

 

 

89.4nm

105kt

 

 

 

CRSR

 

 

>345°To

0:51

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

APT VOR NDB SUP ACT NAV FPL CAL SET OTH

 

MSG

D

 

 

 

CLR

ENT

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

 

Figure 2

 

 

 

 

2.The waypoint page for the nearest airport will now be displayed on the screen.

The right inner knob (in the “pulled out” position), may be used in the normal manner to scan the other nearest airports. With the right inner knob in the “in” position, you may view all four airport pages for a specific airport.

-1-

DTo go Direct To a waypoint:

1.Press the Dbutton. The Direct To (DIR) page will be displayed with a waypoint field.

2.Enter desired waypoint using right concentric knobs.

3. Press

Fto view waypoint information. Press

Fagain to confirm. This initi-

ates the Direct To—your D-bar will be centered, and you’re on your way!

 

4. Alternatively, display desired waypoint on APT, VOR, NDB or SUP page, or move

the cursor over desired waypoint in the active flight plan, then press

D, then

press

Fto confirm.

 

To create a Flight Plan:

1.Select the active Flight Plan (FPL 0) or one of the stored Flight Plans (FPL 1 through FPL 9) on the screen.

2.Delete existing waypoints from the Flight Plan as necessary by placing the cursor

(B) over the identifier, pressing

E, and then pressing

F.

3.If you wish to insert a waypoint identifier between two other waypoints, place the cursor ( B) over the waypoint you wish for the new waypoint to precede.

4. With the cursor on, enter the desired waypoint identifier and press

F.

5. The waypoint page for the selected identifier will be displayed. If this is the way-

 

point you intended to enter, press

Fagain.

 

6. Repeat the waypoint entry process as needed for your Flight Plan.

To calculate the winds aloft:

1.Use the CAL 3 page to calculate the present pressure altitude.

2.Use the CAL 5 page to calculate the present true airspeed (TAS).

3.Turn to the CAL 6 page and enter the present aircraft heading. The headwind or tailwind component of the wind, and the wind vector (direction and speed) will be displayed on the last two lines of the CAL 6 page.

-2-

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