PIN Function Connection | Honeywell MKXXII guide

Fault Designation: RADIO ALTIMETER BUS

Bus Type: Basic

Honeywell

MK XXII EGPWS Installation Manual

TABLE E 3.1.8-1: RADIO ALTITUDE INPUT SELECT TYPE 1 (ALT 55)

SIGNAL

CONNECTION

SUMMARY DATA

Radio Altimeter #1	(+) = J1-64		Format: Alt 55 with Validity Flag
	(-) = J1-45		Input Type: Basic
			Fault Designation: RADIO ALTIMETER FAULT
			Validity: Radio Altitude Valid Discrete #1 (+28V)
PIN FUNCTION	CONNECTION	PIN TYPE	CHANNEL DESIGNATION				Polarity/Configuration
			REFERENCE
Radio Altitude Validity	J1-29	Input	28V_DISC_07				>+17V = Valid
Discrete #1 (+28V)							<+4.4V = Invalid
DH Discrete (Gnd)	J1-33	Input	GND_DISC_11				Gnd = Below DH
							<not> Gnd = Above DH
CONFIGURATION DATA			Description				Value
Out of Track Maximum		Pseudo altitude is only allowed to operate within					2800
Out of Track Minimum		these limits.				-20
Pseudo Altitude Type		Selects parameters for pseudo altitude engage logic				4
Field Enable Type		Selects pseudo altitude field elevation					2

CHANNEL

429RX_5

TABLE E 3.1.8-2: RADIO ALTITUDE INPUT SELECT TYPE 2 (ARINC 429) CONNECT TO:

Left ( #1) LRRA

(Low Speed)

A = J2-21			Data
B = J2-4		Radio Altitude
PIN FUNCTION			CONNECTION

DH Discrete (Gnd)			J1-33

		Label		Sig. Bits	Range
		164		16	±8192 FT
PIN TYPE			CHANNEL DESIGNATION
				REFERENCE
Input			GND_DISC_11

Signal Type		Resolution
Basic		0.125
Polarity/Configuration
Gnd = Below DH

<not> Gnd = Above DH

Rate (ms)

25-50

SIGNAL

Radio Altimeter #1

TABLE E 3.1.8-3: RADIO ALTITUDE INPUT SELECT TYPE 3 (RT-200/300)

CONNECTION		SUMMARY DATA
(+) = J1-64		Format: DC with Validity Flag (RT-200/300)
(-) = J1-45		Input Type: Basic
		Fault Designation: RADIO ALTIMETER FAULT
		Validity: Radio Altitude Valid Discrete #1 (+28V)

PIN FUNCTION	CONNECTION		PIN TYPE	CHANNEL DESIGNATION		Polarity/Configuration
				REFERENCE
Radio Altitude Validity	J1-29		Input	28V_DISC_07		>+17V = Valid
Discrete #1 (+28V)						<+4.4V = Invalid
DH Discrete (Gnd)	J1-33		Input	GND_DISC_11		Gnd = Below DH
						<not> Gnd = Above DH

CONFIGURATION DATA	Description	Value
Out of Track Maximum	Pseudo altitude is only allowed to operate within	2800
Out of Track Minimum	these limits.	-20
Pseudo Altitude Type	Selects parameters for pseudo altitude engage logic	3
Field Enable Type	Selects pseudo altitude field elevation	2

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

REV: C SHEET 234

Image 234

Honeywell MKXXII installation manual PIN Function Connection, PIN Type Channel Designation Reference

Contents

Release Date 12/14/00 REV C Sheet ALL Revisions REV Description Honeywell MK Xxii Egpws Installation Manual Table of Contents Honeywell MK VI MK Viii Egpws Installation Design Guide Honeywell MK VI MK Viii Egpws Installation Design Guide 104 Section V Certification 158 143149 160 Aircraft Application Data Section General Information Honeywell MK Xxii Egpws Installation Manual Section I General Information License Requirements How To Use This Docu ment IntroductionApplicability Reference Documents Description of Equipm ent GPS Antenna MK Xxii Egpws Comp uterMK Xxii Egpws Conf iguration Module OAT Sensor Smart Cable Pcmcia Interface MK Xxii Egpws Smart Cable Technical Characteris tics Configuration Module Units SuppliedMK Xxii Egpws Honeywell MK Xxii Egpws Installation Manual 2 RS-232 Cable Installation and Acces sories KitsNew Egpws installation with Internal GPS Smart Cable Terrain Database Card s Flight History Card GPS Antenna & cable Circuit BreakerAnnunciators & Switc h/Annunciators Cockpit Speaker Opti onal Insertion/Removal Too l P1, P2, P3 Tools Required Crimping Tool P1, P 2, P3Contact Positioner P 1, P2, P3 Spare Contacts P1, P 2, P3 Honeywell MK Xxii Egpws Installation Manual Section Installation Honeywell MK Xxii Egpws Installation Manual Section II Installation Equipment Installation 2.3.1 General Unpacking and Inspec ting the Equipment MK Xxii Computer Loc ation MK Xxii Computer Ins tallation Configuration Module Location Configuration Module Installation Configuration Module Assembly Required Installation Assembly Sequence 1 MK Xxii Egpws Configuration Module 2 MK Xxii Egpws Configuration Module 3 MK Xxii Egpws Configuration Module 4 MK Xxii Egpws Configuration Module 5 MK Xxii Egpws Configuration Module 6 MK Xxii Egpws Configuration Module 7 MK Xxii Egpws Configuration Module Cockpit Annunciators / Switches GPS Antenna Installat ionOAT Sensor Installatio n GPS Antenna location Description Egpws cautionGPWS G/S Cancld Location Gpws warning red & Gpws alert amber 8 MK Xxii Egpws Annunciators/Switches Location Terrain Inhibit Inhibit Switch Functio ns and SelectionLow Altitude Mode Audio Inhibit Timed MK Xxii Egpws Outline MK Xxii Egpws Mounting Tray Honeywell P/N 405-0383-001 Honeywell MK Xxii Egpws Installation Manual Section System Planning Honeywell MK Xxii Egpws Installation Manual Section III System Planning Category 8 Radio Altitude Input Select Category 14 Audio Output Level System Wiring/ Electr ical Interfaces Primary Power InputChassis Ground Analog and Digital Inp uts Discrete InputsSerial Outputs Audio Output Discrete Outputs Aircraft / Mode Type Configurable Interface sCategory 1 Aircraft / Mode Type Select Instructions Category 2 Air Data Input Select Examples Analog altitude and 500 ohm OAT Egpws MK Digital Arinc 429 Cat ID 5, 1 Digital -ARINC 575 Cat ID Arinc Shadin 2000 Cat ID Digital Arinc 429 Dual IOC Buses Cat . ID Category 3 Position Input Select Arinc 743 Format Examples Arinc 429 BUS Cat ID 0,1,4,5 3.2 RS-232 Transmit-Receive, 9600 baud Cat ID Dual Arinc 429 BUS Cat ID Category 4 Altitude Callouts Category 5 Audio Menu Select Category 6 Terrain Display Select TAD Selection Terrain Display Configuration Group Type of sweep used for terrain data fan, standard, etc 6-1 Single Tube Wx/Terrain Display Display Input Control Group Output 429 Bus GroupExample Egpws TRA-45A J101 Egpws Avidyne FSD Honeywell Radar Indicator Honeywell WRX R/T Avtech DSU Arinc 429 Range #1 Arinc 429 Range #2 Kcpb Video #1 Out Category 7 Options Select Group #1 Steep Approach Not Available in the Mk7.3 TA&D Alternate Pop-up Peaks Mode Obstacle AwarenessBank Angle Callout Enabling WOW Reversal GPS Altitude Reference Category 8 Radio Altitude Input Select Example Digital Radio Altitude Interface DH Discrete Gnd Valid Radio Altimeter Indicator Analog Radio Altitude Interface Category 9 Navigation Inputs Select Example Analog Glideslope Interface cat ID 0,1,5 RNA-34A Digital Glideslope/Localizer Interface Dual Glideslope Receiver Attitude Signals Category 10 Attitude Input Select Example Analog Roll Angle Synchro Vertical Gyro Digital Arinc 429 High Speed Ahrs Category 11 Heading Input Select Magnetic Heading Example Analog Heading Synchro CAT ID Directional Gyro Heading High Speed Category 12 Windshear Input Select Instruction Category 13 Input / Output Discrete Type Select Input/Output Discretes Weight on Wheels WOW Discrete Audio Inhibit DiscreteLanding Gear Discrete Glideslope Cancel Discrete Mode 6 Low Volume DiscreteAutopilot Engaged Discrete Terrain Awareness Inhibit Self Test DiscreteGlideslope Inhibit Discrete Output Discretes Low Altitude Mode Select DiscreteTimed Audio Inhibit Discrete Lamp Format Gpws Warning Discrete Gpws Inop DiscreteTAD Inop Discrete Gpws Alert Discrete Low Altitude Mode Discrete Terrain Display Select #1 & #2 Discrete REV C Sheet Category 14 Audio Output Level Ohm Category 15, Autorotation Threshold Autorotation Threshold 107 108 Egpwc Initialization a nd Configuration Harness Checkout and Power CheckUnit Installation 1 RS-232 Communicatio n with the MK Xxii Egpws Egpwc Front Panel T est Connector WinVIEWS Configuration Module Programming WinVIEWS Operation 112 CUW and CMR Comm ands CFG CUW 0/15 128 3 2 134 128 3 29 1 0 2 0 0 129 0 Configuration Module Reprogramming CATspacecategory #spaceID#spaceT or FEnter Regional Terrain Data base Loading 4.6.1 Effectivity Approval Material Cost and Av ailability Accomplishment Instr uctions Verification of the Ter rain Database Version END of Test 120 Section Certification Honeywell MK Xxii Egpws Installation Manual Section V Certification FAA Requirements Certification Procedur e Equipment Compatibi lityEquipment Location Ground Test Pilots Guide Failure Modes, Effects , and Safety AnalysisFlight Test Existing STC’s Honeywell MK Xxii Egpws Installation Manual Appendix a Customer Worksheet Honeywell MK Xxii Egpws Installation Manual MK Xxii Egpws Cockpit Displays GPS Discrete Inputs Parameter Generic Model Information System REV C Sheet REV C Sheet REV C Sheet REV C Sheet REV C Sheet Appendix B Sample Wiring Diagrams DWG no 060-4314-225 Revc Sheet Honeywell MK Xxii Egpws Installation Manual Honeywell MK Xxii Egpws Installation Manual Appendix C Honeywell MK Xxii Egpws Installation Manual RS-232 Communication with the Egpws Baud, No Parity, 8 bits, and 1 stop bit REV C Sheet REV C Sheet Honeywell MK Xxii Installation Manual Appendix D Vendor Drawings Honeywell MK Xxii Egpws Installation Manual Vendor Contact Information AMP For orders and AOG requirements, contact D1-1 Edmo GPS RF Cable Sets D1-2 Emteq Per 100 ft Inches Bend Radius Minimum 1 Connectors for Tflx cable series GPS 1 Connectors for Pflx cable series GPS Tool Frame and Die Part Numbers Installation Considerations Aerospace Optics Inc D1-3 Aerospace Optics Mail switches@vivisun.com StacoSwitch Honeywell MK Xxii Egpws Installation Manual Appendix E Interface Description Document Honeywell MK Xxii Egpws Installation Manual Connector Interface Introduction Part Number PurposeSystem Overview Electrical Interface Introduction Signal InterfacesPrimary Power Input Chassis Ground LOW Level Glideslope DC Analog InputsRadio Altitude Localizer Deviation or LOW Level Glideslope Validity 2.4 Outside AIR TemperatureConfiguration Defined DC Inputs Barometric Altitude Synchro Roll Attitude AC Analog Inputs2.7.1 2.7.2 Configuration Defined Synchro Inputs Signal Timing Reference Inputs 2.9 Arinc 429/575 Digital Serial BUS Inputs 2.9.1 RS-232 / RS-422 Digital Serial BUS Inputs GPS RS-232 Digital Serial BUS Serial PortGPS RS-422 Digital Serial BUS Serial Port AIR Data RS-422 Digital Serial BUS Serial Port +28 VDC Discrete CharacteristicsAIR Data RS-232 Digital Serial BUS Serial Port SCI Range RS-422 Digital Serial BUS Serial Port Configuration Module Interface Ground Discrete CharacteristicsGPS Antenna Input OAT Voltage Reference Output Monitor Output CharacteristicsDiscrete Output Characteristics Lamp Driver Outputs Arinc Digital Serial Output Busses High Level Speaker Audio OutputLOW Level Interphone Audio Output Arinc 429 Output BUS 2.18.1 RS-232 Maintenance Port Serial Port Arinc 453 Output BUSFront Panel Test Interface Front Panel Status Indicators Pcmcia / Smartcable PortGSE Present Discrete Input Configuration Types Configuration SelectionAircraft Application Data Signal Selection Table E 3 Category ID Selection ProcedureInstruction Configuration Selection Tables Category 1, Aircraft / Mode Type Select Torque Type Table E Effectivity App Cfg Fault Designation Engine 1 BUS Bus Type Basic Fault Designation Engine 2 BUS Bus Type BasicEngine Torque Data Selection Fault Designation Engine 1 BUS Bus Type RS-422 9600 baud Fault Designation Engine 2 BUS Bus Type RS-422 9600 baud Torque Data Select 10 Bell Summary Data Torque Data Select 8 AS365 Dauphin N3Torque Data Select 9 Bell Torque Data Select 11 Bell 212/412 Summary Data Torque Data Select 16 Common DC Torque Fault Designation Engine 1 BUSTorque Data Select 14 Coast Guard HH-65 Summary Data Connection Summary Data Category 2, AIR Data Input Select Table E DescriptionTable E 3.1.2 AIR Data Input Select for Egpws Mkxxii Configuration Data Fault Designation AIR Data BUS Bus Type BasicType Summary Data Table E 3.1.2-3 AIR Data Input Select #3 Summary Data Table E 3.1.2-4 AIR Data Input Select #4 Summary Data Table E 3.1.2-5 AIR Data Input Select #5Connect to Channel Channel Connect to Channel 429RX2Table E 3.1.2-6 AIR Data Input Select #6 Table E 3.1.2-10 AIR Data Input Select #10 Table E 3.1.2-11 AIR Data Input Select #11 Summary Data 3.3 Category 3, Position Input SelectPosition Input Type TableE Description Fault Designation GPS BUS Bus Type Basic UTC Fault Designation Internal GPS Bus Type Basic Internal Fault Designation GPS BUS Bus Type Basic Category 4, Altitude Callouts App CfgTable E 3.1.4 Altitude Callouts for Egpws Mkxxii Honeywell MK Xxii Egpws Installation Manual Table E 3.1.5 Audio Menu Type Category 5, Audio Menu SelectEffectivity App Cfg 006 Table E 3.1.5-128 Audio Menu Type 128 Basic Helicopter Section Overview IDand TCF Disable Application NotesCategory 6, Terrain Display Select Defined By Honeywell MK Xxii Egpws Installation Manual Table E KC Picture Bus Table Table E 3.1.6-1 No Display TAD and TCF Enabled Table Table E 3.1.6-2 TA&D / TCF DisabledChannel Table Table E 3.1.6-3 Collins ProLine II Fault Designation Display BUS Bus Type BasicDisplay Configuration Group 6 Collins PRO-LINE II Integration note Display Configuration Group 1 Bendix RDR 4A/B PPI with MOD Table Table E 3.1.6-4 Bendix PPI-4A/4B Display Configuration Group 2 Collins Proline II Table E Collins ProLine II Display Configuration Group 3 Collins Proline II, 5X4 Table E Collins ProLine II 5x4,5x5 Display Configuration Group 7 NON-INTEGRATED Efis 40/50 Table E Non-Integrated Efis 40/50 Honeywell/Bendix Peaks Always Enabled Display Configuration Group 8 Integrated Efis 40/50Table E 3.1.6-10 Integrated Efis 40/50 Honeywell/Bendix Honeywell MK Xxii Egpws Installation Manual Table E 3.1.6-12 Collins WXI-701/711, without Auto Range Terrain Display BUS #2 Integration note PinsTerrain Display BUS #1 453TX1 Reference Name Table E 3.1.6-14 Bendix PPI-4A/4B without Auto Range Terrain Display BUS #2 453TX2 6.2-3 Display Input Control Group Reference Name PIN Function6.3-0OUTPUT 429 BUS Group Traceability Table E 3.1.6-16 Bendix IN182A/IN812A Radar display RDR Reference section Pins Comments Output 429 Bus Group Category 7, Options Select Group #1 Table E Bendix IN842A/IN862A Radar display RDRFunction Value TA&D Alternate Pop Up False TA&D Alternate Pop Up True Display Input Control Group Display Input Control Group Honeywell Fault Designation IOC BUS Table E3.1.6-236 Display Configuration Collins ProLine IV Honeywell Channel 429RX8 Table E 3.1.6-246 Non-Integrated Efis 10 Bendix/Honeywell Connect to DC811 #1 Display Input Control Group Channel 422RX2Connect to DC811 #2 Honeywell MK Xxii Egpws Installation Manual SCI Bus RS-422 12K baud Category 7, Options 1 Select Altitude Reference6 Effectivity App CfgTable E 317 Options Select Group #1 True False WGS-84 Category 8, Radio Altitude Input Select Radio Altitude Type Table E DescriptionDescription Value PIN Function Connection PIN Type Channel Designation Reference Table E 3.1.8-5 Radio Altitude Input Select Type 5 ALT Reference Summary Data Table E 3.1.9-0 Navigation Inputs Select Summary Data Category 9, Navigation Input SelectTable E 3.1.9 Navigation Input Select for Egpws Mkxxii Connection PIN Type Fault Designation ILS BUS Bus T ype Basic Fault Designation ILS BUS Table E 3.1.10 Attitude Input Select for Egpws MK Category 10, Attitude Input SelectAttitude Input Select Table E 3.1.10-0 Attitude Input Select Type Fault Designation Ahrs BUS Table E 3.1.10-4 Attitude Input Select TypeTable E 3.1.10-128 Attitude Input Select Type Connect to Heading Input Select Table E Description Fault Designation Ahrs BUS Bus Type BasicCategory 11, Heading Input Select Table E 3.1.11 Heading Input Select for Egpws MK Effectivity App Cfg 003 Category 12, Windshear Input SelectNo Windshear Table E 3.1.12 Windshear Input Select Category 13, Input / Output Discrete Type Select Input/Output Discrete Type Table E Configuration Data Possible States StateTable E 3.1.13-128 INPUT/OUTPUT Discrete Type Table E 3.1.13-129 INPUT/OUTPUT Discrete Type Volume Select Category 14, Audio Output LevelTable E 3.1.14 Audio Output Level Category 15, Autorotation Threshold Autorotation Threshold TorqueTable E 3.1.15 Autorotation Threshold for Egpws MK SYN1X SYN1Z SYN2Z Connector Pin Refer to Category 13 where multiple uses are possible Honeywell MK Xxii Egpws Installation Manual Figure E 4.1, Connector Pin References J1, J2, J3 AcronymInterpretation Definitions Acronym Interpretation Pcmcia