Accomplishment Instr uctions | Honeywell MKXXII specification

Honeywell

MK XXII EGPWS Installation Manual

4.6.5 Accomplishment Instr uctions

Load the PCMCIA card data as described in paragraphs 4.6.5 A. or 4.6.5 B. below. Loading time will be approximately 70 minutes.

A.Loading the PCMCIA Card Data with the Computer mounted in the Aircraft.

(1)Connect the Smart Cable (Honeywell PN 951-0386-001) to the EGPWC J3 connector.

(2)Ensure that the 28 VDC circuit breaker to the EGPWC is ON and that the COMPUTER OK LED on the EGPWC front panel is on.

(3)Insert the PCMCIA card into the Smart Cable PCMCIA card slot.

NOTE: Precautionary notes on the PCMCIA card, regarding insertion and/or removal while power is applied, should be ignored since the EGPWC automatically handles the application and removal of PCMCIA card power.

(4)While the loading is in progress, the IN PROG LED on the Smart Card remains ON and the COMPUTER OK LED on the EGPWC is OFF.

(5)When loading is complete the XFER COMP LED on the Smart Card turns ON.

(6)Remove the PCMCIA card from the Smart Card slot.

(7)After approximately 15 seconds the COMPUTER OK LED comes ON to indicate that the contents of the PCMCIA card were successfully transferred.

(8)Remove the Smart Card connector from the EGPWC front panel J3 connector.

(9)To perform the verification of the Terrain Database version, go to paragraph 4.6.6 below.

B.Loading the PCMCIA Card Data with the Computer removed from aircraft

(1)Locate a 28 VDC Power Supply with a minimum supply current of 2 amps.

(2)With the Power Supply turned OFF, connect the Power Supply to the J1 connector of the EGPWC as follows:

J1 connector Pin

J1-40, J1-60

J1-41, J1-61

J1-42, J1-53

Pin Nomenclature

28 VDC (+)

28VDC (-) Chassis GND


CAGE CODE:		SCALE: NONE SIZE: A DWG NO: 060-4314-225						REV: C	117
97896		SCALE: NONE SIZE: A DWG NO: 060-4314-225						REV: C		SHEET
97896

Image 117

Honeywell MKXXII installation manual Accomplishment Instr uctions

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 149 143158 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 MK Xxii Egpws Conf iguration Module MK Xxii Egpws Comp uterGPS Antenna OAT Sensor Smart Cable Pcmcia Interface Technical Characteris tics MK Xxii Egpws Smart Cable Configuration Module Units SuppliedMK Xxii Egpws Honeywell MK Xxii Egpws Installation Manual New Egpws installation with Internal GPS Installation and Acces sories Kits2 RS-232 Cable Smart Cable Flight History Card Terrain Database Card s GPS Antenna & cable Circuit BreakerAnnunciators & Switc h/Annunciators Cockpit Speaker Opti onal Contact Positioner P 1, P2, P3 Tools Required Crimping Tool P1, P 2, P3Insertion/Removal Too l P1, 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 Unpacking and Inspec ting the Equipment Equipment Installation 2.3.1 General MK Xxii Computer Ins tallation MK Xxii Computer Loc ation Configuration Module Installation Configuration Module Location Required Configuration Module Assembly 1 MK Xxii Egpws Configuration Module Installation Assembly Sequence 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 OAT Sensor Installatio n GPS Antenna Installat ionCockpit Annunciators / Switches GPS Antenna location Egpws cautionGPWS G/S Cancld Description Gpws warning red & Gpws alert amber Location 8 MK Xxii Egpws Annunciators/Switches Location Low Altitude Mode Inhibit Switch Functio ns and SelectionTerrain Inhibit Audio Inhibit Timed MK Xxii Egpws Outline Honeywell P/N 405-0383-001 MK Xxii Egpws Mounting Tray 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 Discrete Outputs Audio Output Category 1 Aircraft / Mode Type Select Configurable Interface sAircraft / Mode Type Instructions Category 2 Air Data Input Select Egpws MK Examples Analog altitude and 500 ohm OAT Digital Arinc 429 Cat ID 5, 1 Arinc Digital -ARINC 575 Cat ID Shadin 2000 Cat ID Digital Arinc 429 Dual IOC Buses Cat . ID Arinc 743 Format Category 3 Position Input Select 3.2 RS-232 Transmit-Receive, 9600 baud Cat ID Examples Arinc 429 BUS Cat ID 0,1,4,5 Dual Arinc 429 BUS Cat ID Category 4 Altitude Callouts Category 5 Audio Menu Select TAD Selection Category 6 Terrain Display Select Type of sweep used for terrain data fan, standard, etc Terrain Display Configuration Group 6-1 Single Tube Wx/Terrain Display Display Input Control Group Output 429 Bus GroupExample TRA-45A Egpws J101 Egpws Avidyne FSD Honeywell WRX R/T Honeywell Radar Indicator Arinc 429 Range #1 Arinc 429 Range #2 Kcpb Video #1 Out Avtech DSU 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 GPS Altitude Reference WOW Reversal Example Digital Radio Altitude Interface Category 8 Radio Altitude Input Select Analog Radio Altitude Interface DH Discrete Gnd Valid Radio Altimeter Indicator Category 9 Navigation Inputs Select RNA-34A Example Analog Glideslope Interface cat ID 0,1,5 Dual Glideslope Receiver Digital Glideslope/Localizer Interface Category 10 Attitude Input Select Attitude Signals Vertical Gyro Example Analog Roll Angle Synchro Ahrs Digital Arinc 429 High Speed Magnetic Heading Category 11 Heading Input Select Directional Gyro Example Analog Heading Synchro CAT ID Heading High Speed Instruction Category 12 Windshear Input Select Input/Output Discretes Category 13 Input / Output Discrete Type Select 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 Timed Audio Inhibit Discrete Low Altitude Mode Select DiscreteOutput Discretes Lamp Format TAD Inop Discrete Gpws Inop DiscreteGpws Warning Discrete Gpws Alert Discrete Terrain Display Select #1 & #2 Discrete Low Altitude Mode Discrete REV C Sheet Ohm Category 14 Audio Output Level Category 15, Autorotation Threshold Autorotation Threshold 107 108 Unit Installation Harness Checkout and Power CheckEgpwc Initialization a nd Configuration 1 RS-232 Communicatio n with the MK Xxii Egpws WinVIEWS Egpwc Front Panel T est Connector WinVIEWS Operation Configuration Module Programming 112 CFG CUW 0/15 128 3 2 134 128 3 29 1 0 2 0 0 129 0 CUW and CMR Comm ands CATspacecategory #spaceID#spaceT or FEnter Configuration Module Reprogramming Approval Regional Terrain Data base Loading 4.6.1 Effectivity 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 Equipment Location Certification Procedur e Equipment Compatibi lityFAA Requirements Ground Test Flight Test Failure Modes, Effects , and Safety AnalysisPilots Guide Existing STC’s Honeywell MK Xxii Egpws Installation Manual Appendix a Customer Worksheet Honeywell MK Xxii Egpws Installation Manual Cockpit Displays MK Xxii Egpws GPS Parameter Discrete Inputs 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 Baud, No Parity, 8 bits, and 1 stop bit RS-232 Communication with the Egpws REV C Sheet REV C Sheet Honeywell MK Xxii Installation Manual Appendix D Vendor Drawings Honeywell MK Xxii Egpws Installation Manual AMP Vendor Contact Information For orders and AOG requirements, contact D1-1 Edmo D1-2 Emteq GPS RF Cable Sets Inches Bend Radius Minimum Per 100 ft 1 Connectors for Tflx cable series GPS 1 Connectors for Pflx cable series GPS Tool Frame and Die Part Numbers Installation Considerations D1-3 Aerospace Optics Aerospace Optics Inc Mail switches@vivisun.com StacoSwitch Appendix E Interface Description Document Honeywell MK Xxii Egpws Installation Manual Honeywell MK Xxii Egpws Installation Manual Connector Interface Introduction Part Number PurposeSystem Overview Primary Power Input Signal InterfacesElectrical Interface Introduction Chassis Ground Radio Altitude DC Analog InputsLOW Level Glideslope Localizer Deviation or LOW Level Glideslope Validity Configuration Defined DC Inputs Outside AIR Temperature2.4 Barometric Altitude 2.7.1 AC Analog InputsSynchro Roll Attitude 2.7.2 Signal Timing Reference Inputs Configuration Defined Synchro Inputs Arinc 429/575 Digital Serial BUS Inputs 2.9 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-232 Digital Serial BUS Serial Port +28 VDC Discrete CharacteristicsAIR Data RS-422 Digital Serial BUS Serial Port SCI Range RS-422 Digital Serial BUS Serial Port Configuration Module Interface Ground Discrete CharacteristicsGPS Antenna Input Discrete Output Characteristics Monitor Output CharacteristicsOAT Voltage Reference Output Lamp Driver Outputs LOW Level Interphone Audio Output High Level Speaker Audio OutputArinc Digital Serial Output Busses 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 Effectivity App Cfg Torque Type Table E Fault Designation Engine 1 BUS Bus Type Basic Fault Designation Engine 2 BUS Bus Type BasicEngine Torque Data Selection Fault Designation Engine 2 BUS Bus Type RS-422 9600 baud Fault Designation Engine 1 BUS Bus Type RS-422 9600 baud Torque Data Select 9 Bell Torque Data Select 8 AS365 Dauphin N3Torque Data Select 10 Bell Summary Data Torque Data Select 11 Bell 212/412 Summary Data Torque Data Select 14 Coast Guard HH-65 Summary Data Fault Designation Engine 1 BUSTorque Data Select 16 Common DC Torque 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 Table E 3.1.2-6 AIR Data Input Select #6 Channel 429RX2Channel Connect to 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 UTC Fault Designation GPS BUS Bus Type Basic Internal Fault Designation Internal GPS Bus Type Basic Bus Type Basic Fault Designation GPS BUS Category 4, Altitude Callouts App CfgTable E 3.1.4 Altitude Callouts for Egpws Mkxxii Honeywell MK Xxii Egpws Installation Manual Effectivity App Cfg 006 Category 5, Audio Menu SelectTable E 3.1.5 Audio Menu Type Table E 3.1.5-128 Audio Menu Type 128 Basic Helicopter Category 6, Terrain Display Select IDand TCF Disable Application NotesSection Overview 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 Display Configuration Group 6 Collins PRO-LINE II Fault Designation Display BUS Bus Type BasicTable Table E 3.1.6-3 Collins ProLine II Integration note Table Table E 3.1.6-4 Bendix PPI-4A/4B Display Configuration Group 1 Bendix RDR 4A/B PPI with MOD Table E Collins ProLine II Display Configuration Group 2 Collins Proline II Table E Collins ProLine II 5x4,5x5 Display Configuration Group 3 Collins Proline II, 5X4 Table E Non-Integrated Efis 40/50 Honeywell/Bendix Display Configuration Group 7 NON-INTEGRATED Efis 40/50 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 #1 453TX1 Integration note PinsTerrain Display BUS #2 Reference Name Terrain Display BUS #2 453TX2 Table E 3.1.6-14 Bendix PPI-4A/4B without Auto Range 6.2-3 Display Input Control Group Reference Name PIN Function6.3-0OUTPUT 429 BUS Group Traceability Reference section Table E 3.1.6-16 Bendix IN182A/IN812A Radar display RDR Output 429 Bus Group Pins Comments Function Value Table E Bendix IN842A/IN862A Radar display RDRCategory 7, Options Select Group #1 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 Type Channel Designation Reference PIN Function Connection Reference Summary Data Table E 3.1.8-5 Radio Altitude Input Select Type 5 ALT Table E 3.1.9 Navigation Input Select for Egpws Mkxxii Category 9, Navigation Input SelectTable E 3.1.9-0 Navigation Inputs Select Summary Data Connection PIN Type Fault Designation ILS BUS Fault Designation ILS BUS Bus T ype Basic Attitude Input Select Category 10, Attitude Input SelectTable E 3.1.10 Attitude Input Select for Egpws MK 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 Category 11, Heading Input Select Fault Designation Ahrs BUS Bus Type BasicHeading Input Select Table E Description Table E 3.1.11 Heading Input Select for Egpws MK No Windshear Category 12, Windshear Input SelectEffectivity App Cfg 003 Table E 3.1.12 Windshear Input Select Input/Output Discrete Type Table E Category 13, Input / Output Discrete Type Select 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 Definitions AcronymInterpretation Acronym Interpretation Pcmcia