Honeywell

MK XXII EGPWS Installation Manual

E 5.3.10 CATEGORY 10, ATTITUDE INPUT SELECT

The following table provides identification of the Roll Attitude Angle type. corresponds to a table that provides detailed information on the configuration. Select #1 are found in 0-1.

In this category, only the following signals are defined:

The entry in the Attitude Input Select For example, the details for Attitude Input

Roll Attitude

Pitch Attitude

TABLE E 3.1.10: ATTITUDE INPUT SELECT FOR EGPWS MK XXII

ID

0

2

4

128

Attitude Input

Select

(Table 0-x)

0

2

4

128

Description

Analog Roll (3-Wire Synchro) without validity

Analog Pitch and Roll (3-Wire Synchro)

Analog Roll(3-Wire Synchro) with validity (Note 1)

Digital Pitch, Roll, Pitch Rate and Roll Rate (High Speed ARINC 429) (Note 3)

Effectivity

 

 

 

 

 

 

App.

 

Cfg.

 

 

-001

-001

 

 

-003

-003

 

 

-003

-003

 

 

-006

-006

 

 

 

 

 

 

Note 1: ID 4 may not be used with Category 13 (I/O Discrete Type) ID’s 2, or 3. This is due to a conflict with the validity discrete. ID 0 may be used instead with the Validity discrete left unconnected. Also, ID 4 are intended to be used with helicopter types that do not have the tail strike functionality (currently the MD-900 only).

Note 2: ID 128 may only be used in conjunction with Category 11 (Magnetic Heading) ID 2.

SIGNAL

Roll Attitude

SIGNAL

Roll Attitude

Pitch Attitude

 

TABLE E 3.1.10-0: ATTITUDE INPUT SELECT TYPE 0

CONNECTION

 

 

 

 

SUMMARY DATA

 

 

 

 

Format: 3 Wire Synchro

(X) = J1-1

 

 

 

Input Type: Basic

(Y) = J1-21

 

 

 

Fault Designation: ROLL FAULT

(Z) = J1-2

 

 

 

Validity: None

 

 

 

 

Reference: None

 

T

ABLE E 3.1.10-2:

ATTITUDE INPUT SELECT TYPE 2

CONNECTION

 

 

 

 

SUMMARY DATA

 

 

 

 

Format: 3 Wire Synchro with Validity Flag

(X) = J1-1

 

 

 

Input Type: Basic

(Y) = J1-21

 

 

 

Fault Designation: ROLL FAULT

(Z) = J1-2

 

 

 

Validity: Attitude Validity Discrete #1

 

 

 

 

Reference: None

 

 

 

 

Format: 3 Wire Synchro with Validity Flag

(X) = J1-5

 

 

 

Input Type: Basic

(Y) = J1-7

 

 

 

Fault Designation: PITCH FAULT

(Z) = J1-6

 

 

 

Validity: Attitude Validity Discrete #1

 

 

 

 

Reference: None

PIN FUNCTION

CONNECTION

PIN TYPE

CHANNEL DESIGNATION

REFERENCE

Polarity/Configuration

References

Attitude Validity Discrete #1

J1-68

Input

28V_DISC_12

>+17V = Valid <+4.4V = Invalid

6.6.24

4.2.7

CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225

REV: C SHEET 238

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Image 238
Honeywell MKXXII installation manual Category 10, Attitude Input Select, Table E 3.1.10 Attitude Input Select for Egpws MK