Honeywell MKXXII installation manual Configuration Selection Tables

Step

(Category)

Signal

Selection

Honeywell

MK XXII EGPWS Installation Manual

Instruction

Ident No.

9

10

11

12

13

14

15

Selects:

a)Glideslope and/or Localizer Source

Selects:

a)Attitude Source

Selects:

a)Magnetic Heading Source

Selects:

Selects:

a)Input Discrete Functions

b)Output Discrete Functions

Selects:

a)Audio Output Level

Selects:

a)Autorotation Threshold

Using Table 5.3.9, and any sub-tables contained within, locate the desired Navigation signal type.

Using Table 5.3.10, and any sub-tables contained within, locate the desired Attitude signal type.

Using Table 5.3.11, and any sub-tables contained within, locate the desired Magnetic Heading signal type.

Using Table 5.3.12, no Windshear is available for helicopter applications. Please select ID 0.

Using Table 5.3.13, and any sub-tables contained within, locate the desired I / O Discrete type.

Using Table 5.3.14, and any sub-tables contained within, locate the desired Volume type.

Using Table 5.3.15, locate the desired Autorotation Threshold. This Category is used on helicopters only.

Record the Ident (ID No.) on the space available on Ident column of this table.

Record the Ident (ID No.) on the space available on Ident column of this table.

Record the Ident (ID No.) on the space available on Ident column of this table.

Record the Ident (ID No.) on the space available on Ident column of this table.

Record the Ident (ID No.) on the space available on Ident column of this table.

Record the Ident (ID No.) on the space available on Ident column of this table.

Record the Ident (ID No.) on the space available on Ident column of this table.

_______

ID #

_______

ID #

_______

ID #

0

_______

ID #

_______

ID #

_______

ID #

_______

ID #

LIMITATIONS: The described use of the configuration module provides for maximum flexibility in selection of input sensors and output behavior. Every attempt has been made to avoid conflicts arising between categories and to reflect the known configurations of aircraft. However in the case of input sensors it should not be construed that all combinations are valid configurations. There may be configurations not supported by the EGPWS software configuration building process (which will cause the EGPWS to fail in an obvious manner). In general you can not have redundancy through the mixing of analog and digital sources, however redundant digital signals on different buses are permissable. As it is not practical to verify all possible sensor combinations, verification of particular sensor combinations is part of the installation certification process. If you intend to implement a sensor configuration not currently identified in Section E 3, please contact Honeywell or an authorized dealer/installer.

E 5.3 CONFIGURATION SELECTION TABLES

Configuration selection is defined by category (or group of functions or inputs). The Category number identifies the subsection where the details are defined. For example Air Data, Category 2, is defined in Section E 5.3.2, and Position Input Source, Category 3, is defined in Section E 5.3.3.

CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 182