Honeywell MK VI User Manual
Mk vi mk viii, Installation design guide, Enhanced ground proximity warning system
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Table of contents
Document Outline
- TITLE SHEET
- TABLE OF CONTENTS
- SECTION I
- SECTION II
- SECTION III
- SYSTEM PLANNING
- Introduction
- System Wiring/ Electrical Interfaces
- Category 1 - Aircraft / Mode Type Select
- Category 2 – Air Data Input Select
- Category 3 – Position Input Select
- Category 4 – Altitude Callouts
- Category 5 – Audio Menu Select
- Category 6 – Terrain Display Select
- Category 7 – Options Select Group #1
- Category 8 – Radio Altitude Input Select
- Category 9 – Navigation Inputs Select
- Navigation Inputs Select (Glideslope & Localizer Inputs)
- Glideslope Validity
- Localizer Validity
- ILS Tuned Discrete Input #1 (+28V) and #2 (GND)
- Analog Glideslope Interface (Cat. 9 ID 0,1,5)
- Digital Glideslope / Localizer / ILS Select Interface (Cat. 9 ID 2,3,4)
- Digital – ARINC 429 Dual IOC buses \(Cat. 9 ID 2
- Instructions
- Category 10 – Attitude Input Select
- Category 11 – Heading Input Select
- Category 12 – Windshear Input Select
- Category 13 – Input / Output Discrete Type Select
- Input Discretes
- Glideslope Inhibit Discrete
- Landing Flaps Discrete
- Audio Inhibit Discrete
- Landing Gear Discrete
- Glideslope Cancel Discrete
- Momentary Flap Override Discrete
- Mode 6 Low Volume Discrete
- Autopilot Engaged Discrete
- Terrain Awareness and TCF Inhibit Discrete
- Self Test Discrete
- Steep Approach Discrete #2
- GPWS INHIBIT Discrete (alternate action)
- Output Discretes
- Instructions
- Input Discretes
- Category 14 – Audio Output Level
- Category 15 - 17 – Undefined Input Selects
- SYSTEM PLANNING
- SECTION IV
- SECTION V
- SECTION VI
- APPENDIX A
- APPENDIX B
- APPENDIX C
- APPENDIX D
- APPENDIX E
- Interface Description Document
- INTRODUCTION
- REFERENCES
- MECHANICAL INTERFACE
- ELECTRICAL INTERFACE
- Introduction
- Signal Interfaces
- Grounds
- Primary Power Input
- DC Analog Inputs
- AC Analog Inputs
- ARINC 429/575 Digital Serial Bus Inputs
- RS-232 / RS-422 Digital Serial Bus Inputs
- Discrete Inputs
- Configuration Module Interface
- GPS Antenna Input
- OAT Voltage Reference Output
- Lamp Driver Outputs
- Audio Outputs
- ARINC Digital Serial Output Buses
- Front Panel Test Interface
- Front Panel Status Indicators
- AIRCRAFT APPLICATION DATA
- Fault Designation: GPS BUS 2
- Fault Designation: IOC BUS 1
-
- Category 9, Navigation Input Select
- Category 10, Attitude Input Select
- Category 11, Heading Input Select
- Category 12, Windshear Input Select
- Category 13, Input / Output Discrete Type Select
- Category 14, Audio Output Level
- Category 15, Undefined for this software release
- Category 16, Undefined for this software release
- Category 17, Undefined for this software release
-
- CONFIGURABLE INPUT DATA DEFINITION
- Analog Input Data
- ARINC 552 Radio Altimeter
- ALT 55 Radio Altimeter
- Uncorrected Barometric Altitude
- Outside Air Temperature (500 ohm probe)
- Outside Air Temperature (Internal Constant)
- ARINC 547/578-4 Low Level Glideslope Deviation with Discrete Valid
- ARINC 547/578-4 Low Level Glideslope Deviation with Low Level Valid
- Roll Attitude, 3 Wire Synchro (11.8 VAC )
- Magnetic Heading, 5 Wire Synchro
- Uncorrected Barometric Altitude (ADS-65)
- RT-221/300 Radio Altimeter
- Pitch Synchro Attitude, 3 Wire Synchro (11.8 VAC )
- Uncorrected Barometric Altitude (CIC 02702)
- ARINC 547/578-4 Low Level Glideslope Deviation Validity
- Roll Attitude, 3 Wire Synchro (11.8 VAC ) with Validity
- Uncorrected Barometric Altitude (AZ-241, AZ-800)
- ARINC 547 Localizer Deviation with Discrete Valid
- Digital Input Data, ARINC 429
- Uncorrected Barometric Altitude (203)
- Static Air Temperature (213)
- Barometric Altitude Rate (212)
- Altitude (076) - GPS (MSL)
- Horizontal Integrity Limit (130) - GPS
- Ground Speed (112) - GPS
- Latitude (110) - GPS
- Longitude (111) - GPS
- Track Angle (103) - GPS
- Horizontal Figure Of Merit \(247\) – GPS \(AR
- Horizontal Figure Of Merit \(247\) – GPS \(AR
- Horizontal Figure Of Merit from HDOP \(101\) –
- Vertical Figure Of Merit \(136\) – GPS \(ARIN
- Vertical Figure Of Merit \(136\) – GPS \(ARIN
- Vertical Figure Of Merit from VDOP \(102\) –
- Sensor Status (273) - GPS
- Universal Time Correlation (125) - GPS
- Date (260) - GPS
- Control Word (154) - MFD
- Control Word 2 (271/273)
- Discrete Word (155 or 176) - MFD
- Hazard Range Output (077)
- Range (050) - Multifunction Signal Generator (MG) or IC600
- Query / Continuous Response (011) - KCPB
- Key Press Data \(012\) – KCPB
- Control Word 1 (270)
- Discrete Word \(273\) – Bendix Weather Radar V
- Discrete Word \(275\) – IC600 only
- Radio Altitude (164)
- Glideslope Deviation (174 or 117)
- Roll Angle (325)
- Magnetic Heading (320)
- Localizer Deviation (173 or 116)
- Pitch Angle (324)
- Range (271) - KCPB
- DSU Status Word (350)
- True Heading (314)
- Corrected Barometric Altitude (204)
- Computed Airspeed (206)
- True Airspeed (210)
- Decision Height \(370\) – IOC Scaling
- Normal Acceleration (333)
- Longitudinal Acceleration (331)
- Left Body Angle of Attack (224)
- Right Body Angle of Attack (225)
- VOR/ILS Frequency (034)
- PFD Mode Select Word (163)
- FWC & GP Discrete Word (171)
- Body Pitch Rate (326)
- Body Roll Rate (327)
- Minimum Descent Altitude \(170\) – IOC Scaling
- Normal Angle of Attack (236)
- North/South Velocity (166) - GPS
- East/West Velocity (174) - GPS
- Discrete Word (017) - KMD 550/850
- Inertial Vertical Speed (365)
- Inertial Altitude (361)
- Vertical Velocity (165) - GPS
- Latitude Fine (120) - GPS
- Longitude Fine (121) - GPS
- Selected Course (100) - IOC
- DH/MDA Selected \(170\) – DAU Scaling
- Digital Data, ARINC 575
- Digital Data, RS-232
- Digital Data, RS-422
- Discrete Inputs
- Analog Radio Altitude Validity Flags
- GND Landing Gear Discrete
- +28V Landing Gear Discrete
- GND Landing Flap Discrete
- +28V Landing Flap Discrete
- Momentary Flap Override Discrete
- Self-Test Discrete
- GND ILS Tuned Discrete #1
- +28V ILS Tuned Discrete #1
- Glideslope Validity Discrete #1
- GND Glideslope Inhibit Discrete
- +28 V Glideslope Inhibit Discrete
- Glideslope Cancel Discrete
- Decision Height Discrete
- Mode 6 Low Volume Discrete
- GND Audio Inhibit Discrete
- +28V Audio Inhibit Discrete
- Display Select Discrete #1
- Display Select Discrete #2
- Terrain Awareness & TCF Inhibit Discrete
- Autopilot Engaged Discrete #1
- Barometric Altitude Validity Discrete
- Magnetic Heading Validity Discrete
- Attitude Validity Discrete
- Steep Approach Discrete #2
- Timed Audio Inhibit Discrete
- GPWS Inhibit Discrete
- Localizer Validity Discrete #1
- Analog Input Data
- OUTPUT DATA DEFINITION
- ARINC 429 Output Data
- Discrete Output Words
- Internal Data Outputs
- Geometric Altitude VFOM (135)
- Terrain Clearance (164)
- Geometric Altitude (261)
- Computed Terrain Clearance (067)
- Latitude – Selected EGPWS \(310\)
- Longitude – Selected EGPWS \(311\)
- Body Angle of Attack—Right \(223\) – MKVIII EG
- Body Angle of Attack—Left \(224\) – MKVIII EGP
- Corrected Airspeed \(242\) – MKVIII EGPWS w/ W
- Windshear Warning Threshold \(331\) – MKVIII E
- Corrected Longitudinal Acceleration \(332\) –
- Raw Total Shear \(362\) – MKVIII EGPWS w/ Wind
- Corrected Normal Acceleration \(364\) – MKVIII
- Computed Flight Path Angle \(375\) – MKVIII EG
- Scaled Total Shear \(376\) – MKVIII EGPWS w/ W
- Terrain Display Outputs
- Equipment Identification
- Fault Summary Words (for Proline 4/21)
- Peak Binary Labels
- ARINC 708A Output
- Audio Output
- Discrete Outputs
- Ground Proximity Alerts Discrete (Lamp) Outputs
- Audio On Discrete
- Monitor Discretes (GPWS INOP & Terrain INOP or Terrain Not Available)
- Terrain Display Switching Discretes (WxR/EGPWS Display Select)
- Flap Override Discrete
- Glideslope Cancel Discrete
- Terrain / Obstacle Awareness Alert Discretes
- Terrain Pop Up
- Windshear INOP Monitor Discretes
- Windshear Warning
- Windshear Caution
- Steep Approach Discrete
- System Configuration Status
- ARINC 429 Output Data
- CONNECTOR INTERFACE
- DEFINITIONS