Aircraft application data, Configuration types, Configuration selection – Honeywell MK VI User Manual

Page 174

Advertising
background image

Honeywell

MK VI MK VIII EGPWS Installation Design Guide

Proprietary notice on title page applies

CAGE CODE: 97896

SCALE: NONE

SIZE: A

DWG NO: 060-4314-150

REV:

SHEET

174

5

AIRCRAFT APPLICATION DATA

This section describes the MK VI and MK VIII EGPWS interfaces for aircraft applications. Section 5.1 is a listing of the
selection categories defining the various aircraft sensor interfaces and EGPWS functional options. Section 5.2 describes
how the Category ID’s are selected and programmed for the interface to aircraft sensors and EGPWS functional options.
Section 5.3 and its sub-sections define the specific aircraft interfaces available for the MK VI and MK VIII EGPWS.

5.1 Configuration

Types

The selection of the basic interfaces to the MK VI and MK VIII EGPWS can be found in the following categories:

Aircraft / Mode Type Select

Category 1

Air Data Input Select

Category 2

Position Input Select

Category 3

Altitude Callouts

Category 4

Audio Menu Select

Category 5

Terrain Display Select

Category 6

Options Select Group 1

Category 7

Radio Altitude Input Select

Category 8

Navigation Input Select

Category 9

Attitude Input Select

Category 10

Heading Input Select

Category 11

Windshear Input Select

Category 12

I / O Discretes Select

Category 13

Audio Output Level

Category 14

Future Configuration Category

Category 15

Future Configuration Category

Category 16

Future Configuration Category

Category 17

5.2 Configuration

Selection

Each category provides information relative to aircraft interfaces or EGPWS functional options required or used for
EGPWS operation. Each category must be defined for the specific aircraft application according to the available aircraft
sensors or equipment and the intended EGPWS function. The choices provided are available in each category identified
by an “ID” number. The ID number is selected for each category and is used to load the selected configuration in a
configuration module installed in the aircraft wiring (physically part of one of the EGPWC mating connectors). For
example, selecting Category 2, ID 1 defines the Air Data Input as ARINC 429 per Table 5.3.2-1 in Category 2. With this
ID programmed into the configuration module the EGPWC will look for and use the interface defined for this ID. Table
5.2 can be used to record the selected ID for each category for later reference when programming the configuration
module. This programming is accomplished using a programming software tool available from Honeywell or generating a
data text string and transferring this data (in either case) via the EGPWC RS-232C (see 4.3.1) to the configuration module.
Once programmed, the configuration is available and read by any installed EGPWC on power up.

Advertising
This manual is related to the following products: