Peaks Mode, Obstacle Awareness | Honeywell MKXXII specification

Honeywell

MK XXII EGPWS Installation Manual

For Helicopters TA&D Alternate Pop Up should always be set to False.

3.3.7.4 Peaks Mode

Peaks mode is an alternate means of displaying terrain data. The standard terrain display mode displays terrain relative to the aircraft altitude that is within the aircraft envelope (the terrain is above or not more than 2000 feet below the aircraft). The terrain display is typically blank during the cruise portion of a flight. Peaks mode provides increased situational awareness by providing the same information as the standard display mode as well as displaying terrain outside of the aircraft envelope and the highest and lowest elevations of terrain displayed. Peaks mode displays terrain based on the absolute terrain elevations.

Disabling peaks mode is not an option in the Mk XXII. Peaks Mode is always selected.

3.3.7.5 Obstacle Awareness

The Obstacle Awareness feature adds a database of (man-made) obstacles that are greater than 100 feet taller than the surrounding terrain to the Terrain Awareness Alerting calculations. (The Terrain Awareness Alerting feature continuously computes terrain clearance envelopes ahead of the aircraft and issues alerts if the boundaries of these envelopes conflict with terrain elevation data in the terrain database.) Obstacle data is currently available for North America and parts of the Caribbean. Not all obstacles will be contained in the database.

Category 7 enables Obstacle Awareness if TA&D is not disabled in Category 6.

Note: TAD must be enabled if Obstacle Awareness is enabled.

Honeywell strongly recommends the selection of Obstacle Awarness.

3.3.7.6 Bank Angle Callout Enabling

The Bank Angle feature provides protection for over banking during maneuvering on approach or climb-out and while at altitude.. The Bank Angle callout can be enabled or disabled as appropriate for this installation.

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

REV: C SHEET 82

Image 82

Honeywell MKXXII installation manual Peaks Mode, Obstacle Awareness, Bank Angle Callout Enabling

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 Introduction How To Use This Docu mentApplicability 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 Units Supplied Configuration ModuleMK 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 Circuit Breaker GPS Antenna & cableAnnunciators & 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 Primary Power Input System Wiring/ Electr ical InterfacesChassis Ground Discrete Inputs Analog and Digital Inp utsSerial 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 Output 429 Bus Group Display Input Control 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 Steep Approach Not Available in the Mk Category 7 Options Select Group #17.3 TA&D Alternate Pop-up Obstacle Awareness Peaks ModeBank 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 Audio Inhibit Discrete Weight on Wheels WOW DiscreteLanding Gear Discrete Mode 6 Low Volume Discrete Glideslope Cancel DiscreteAutopilot Engaged Discrete Self Test Discrete Terrain Awareness InhibitGlideslope 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 Purpose Introduction Part NumberSystem 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 GPS RS-232 Digital Serial BUS Serial Port 2.9.1 RS-232 / RS-422 Digital Serial BUS InputsGPS 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 Ground Discrete Characteristics Configuration Module InterfaceGPS 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 Arinc 453 Output BUS 2.18.1 RS-232 Maintenance Port Serial PortFront Panel Test Interface Pcmcia / Smartcable Port Front Panel Status IndicatorsGSE Present Discrete Input Configuration Selection Configuration TypesAircraft Application Data Table E 3 Category ID Selection Procedure Signal SelectionInstruction Configuration Selection Tables Category 1, Aircraft / Mode Type Select Torque Type Table E Effectivity App Cfg Fault Designation Engine 2 BUS Bus Type Basic Fault Designation Engine 1 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 Table E Description Category 2, AIR Data Input SelectTable E 3.1.2 AIR Data Input Select for Egpws Mkxxii Fault Designation AIR Data BUS Bus Type Basic Configuration DataType Summary Data Table E 3.1.2-3 AIR Data Input Select #3 Summary Data Table E 3.1.2-5 AIR Data Input Select #5 Table E 3.1.2-4 AIR Data Input Select #4 Summary DataConnect 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 Category 3, Position Input Select 3.3Position 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 App Cfg Category 4, Altitude CalloutsTable 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 3.1.6-2 TA&D / TCF Disabled Table Table E 3.1.6-1 No Display TAD and TCF EnabledChannel 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 Display Configuration Group 8 Integrated Efis 40/50 Peaks Always EnabledTable 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 Reference Name PIN Function 6.2-3 Display Input Control Group6.3-0OUTPUT 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 Channel 422RX2 Connect to DC811 #1 Display Input Control GroupConnect to DC811 #2 Honeywell MK Xxii Egpws Installation Manual SCI Bus RS-422 12K baud Altitude Reference6 Effectivity App Cfg Category 7, Options 1 SelectTable E 317 Options Select Group #1 True False WGS-84 Radio Altitude Type Table E Description Category 8, Radio Altitude Input SelectDescription 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 Table E 3.1.10-4 Attitude Input Select Type Fault Designation Ahrs BUSTable 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 State Configuration Data Possible StatesTable E 3.1.13-128 INPUT/OUTPUT Discrete Type Table E 3.1.13-129 INPUT/OUTPUT Discrete Type Category 14, Audio Output Level Volume SelectTable E 3.1.14 Audio Output Level Autorotation Threshold Torque Category 15, Autorotation ThresholdTable 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