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KLN 35A SYSTEM COMPONENTS. A basic KLN 35A system consists of a panel mounted KLN 35A GPS and a KA 92 GPS antenna. An altitude input is required ...
62KB taille 6 téléchargements 254 vues
REQUIRED OPTIONAL HSI GS

CDI

HDG

N

3 6

W

W

24

24

15

21

21

S

GRAY CODE

KI 206

89.6nm ∂∆ KOSH 105kt > ««««∑∏π«««« ∫ >Leg DTK343° TK344° NAV 1 >345°To 0:51

AUTOPILOT YD

CRSR

APT VOR NDB SUP ACT NAV FPL CAL SET OTH MSG

D

CLR

ENT

ALT HDG

GS

NAV

APR

NAV

APR

AP

BC

DN KC 193

Pull SCAN

UP

ALT ı

RN

HDG RC

BC PC

TEST

1-0

KLN 35A

GPS

ALTITUDE

S

NRST

12

12

FR

ı

KI 525A Push ON

TO

E

E

OBS

B

3 N A V

GS

ı

AIRCRAFT 14V POWER

N

6

OR

GS

30

33

33 30

NAV

15

KA 92 GPS ANTENNA

006-08791-0000 Rev 0

KLN 35A SYSTEM

AP ENG

REMOTE ANNUNCIATORS

System Components

RS-232 OUTPUT

MOVING MAP DISPLAYS ARTEX ELS-10

Effective Date 5/95

WPT ALERT MESSAGE

System Components Chapter 1

KLN 35A Pilot’s Guide

System Components

A basic KLN 35A system consists of a panel mounted KLN 35A GPS and a KA 92 GPS antenna. An altitude input is required to obtain full navigation and operational capabilities. Additional system components may be added or interfaced to the KLN 35A which increase its features and capabilities. Some of these optional components include an external course deviation indicator (CDI) or horizontal situation indicator (HSI), ARTEX ELS-10 emergency locator transmitter (ELT), autopilot, and external annunciators. The KLN 35A panel mounted unit contains the GPS sensor, the navigation computer, a liquid crystal display (LCD), and all controls required to operate the unit. A KA 92 GPS “patch” antenna is available for use with the KLN 35A. It is designed to always be mounted on the top of the aircraft. The KLN 35A has analog outputs to drive the left-right deviation bar of most mechanical CDIs and HSIs. In addition, the NAV mode of the Bendix/King KFC 150, KAP 150, KAP 150H, KAP 100, KFC 200, KAP 200, KFC 250, KFC 275, KFC 300, and KFC 325 flight control systems may be coupled to the KLN 35A. Many other autopilots may also be coupled to the KLN 35A. Actual autopilot performance and capability when coupled to the KLN 35A may vary significantly from one autopilot model to another. Altitude may be provided to the KLN 35A from an encoding altimeter or blind encoder. Altitude is used as an aid in position determination when not enough satellites are in view. Some installations may require remote annunciators to be mounted in the aircraft panel in order to indicate the status of certain KLN 35A functions, namely waypoint alert and message.

006-08791-0000 Rev 0

1-1

Effective Date 5/95

System Components Chapter 1

1. KLN 35A SYSTEM COMPONENTS