Honeywell

MK XXII EGPWS Installation Manual

SECTION III – SYSTEM PLANNING

 

SECTION III – SYSTEM PLANNING

57

3.1 INTRODUCTION

57

3.2 SYSTEM WIRING/ ELECTRICAL INTERFACES

57

3.2.1 Primary Power Input

57

3.2.2 Chassis Ground

57

3.2.3 GPS Antenna

58

3.2.4 Analog and Digital Inputs

58

3.2.5 Discrete Inputs

58

3.2.6 Serial Outputs

58

3.2.7 Audio Output

59

3.2.8 Discrete Outputs

59

3.2.9 Configuration Module

59

3.3 CONFIGURABLE INTERFACES

60

3.3.1 Category 1 - Aircraft / Mode Type Select

60

3.3.1.1 Aircraft / Mode Type

60

3.3.1.2 Instructions

60

3.3.1.3 Generic Helicopter with and without Torque

60

3.3.2 Category 2 – Air Data Input Select

61

3.3.2.1 Instructions

61

3.3.2.2 Examples

62

3.3.2.3 Analog altitude and 500 ohm OAT

62

3.3.2.4 Digital – ARINC 429 (Cat. 2 ID 5, 1, 6)

63

3.3.2.5 Digital –ARINC 575 (Cat. 2 ID 2)

64

3.3.2.6 Shadin 2000 (Cat. 2 ID 10)

65

3.3.2.7 Digital – ARINC 429 Dual IOC Buses (Cat. 2. ID 255)

66

3.3.3 Category 3 – Position Input Select

67

3.3.3.1 Instructions

67

3.3.3.2 ARINC 743 Format

67

3.3.3.Examples

68

3.3.3.1 ARINC 429 BUS (Cat. 3 ID 0,1,4,5)

68

3.3.3.2 RS-232 Transmit-Receive, 9600 baud (Cat. 3 ID 3)

68

3.3.3.3 Dual ARINC 429 BUS (Cat. 3 ID 255)

69

3.3.4 Category 4 – Altitude Callouts

70

3.3.4.1 Instructions

70

3.3.5 Category 5 – Audio Menu Select

71

3.3.5.1 Instructions

71

3.3.6 Category 6 – Terrain Display Select

72

3.3.6.1 Instructions

72

3.3.6.2 TAD Selection

72

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

REV: C

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Honeywell MKXXII installation manual Section III System Planning