GPS Antenna location, GPS Antenna Installat ion | Honeywell MKXXII

Honeywell

MK XXII EGPWS Installation Manual

2.3.6 GPS Antenna location

The antenna must be mounted on top of the fuselage. Avoid mounting the antenna near any projections such as the rotor mast, or engine exhaust, where shadows could occur or high heat could damage the antenna. It is recommended that there be a separation of at least 3 feet between the GPS antenna and any VHF Comm antenna on the aircraft. The antenna baseplate must be level within ± 5° in both axis when the aircraft is level (level is defined as the aircraft attitude required when weighing the aircraft for weight and balance). If the antenna is tilted more than 5° or is mounted close to other objects that shadow it, loss of some of the satellites will occur and system performance may be degraded. See manufacturer’s drawing in Appendix D for specifications of antenna, antenna cables, and connector information.

2.3.7 GPS Antenna Installat ion

Refer to manufacturer’s procedures or applicable STC documentation.

2.3.8 OAT Sensor Location

The OAT sensor (CIC 05257) should be mounted on the underside (belly) of the aircraft or other convenient location meeting the following conditions. Avoid mounting the sensor where it can be affected by direct sunlight, or exhaust gases from engines or heaters. The probe tip should extend beyond the aircraft boundary layer into the turbulent airflow. See manufacturer’s drawing in Appendix D for specifications.

2.3.9 OAT Sensor Installatio n

Refer to manufacturer’s procedures or applicable STC documentation.

2.3.10 Cockpit Annunciators / Switches

This section provides information for selecting, locating and mounting of the MK XXII EGPWS Lighted annunciators / switches. NOTE: The nomenclature given for each lamp is an example only. Other manufacturers use nomenclature that is also acceptable. Refer to Honeywell Product Specification 965- 1590-601 for additional information and for electrical loads specification

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

REV: C SHEET 44

Image 44

Honeywell MKXXII GPS Antenna location, GPS Antenna Installat ion, OAT Sensor Location, OAT Sensor Installatio n

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 143 149158 160 Aircraft Application Data Section General Information Honeywell MK Xxii Egpws Installation Manual Section I General Information License Requirements Applicability How To Use This Docu mentIntroduction Reference Documents Description of Equipm ent MK Xxii Egpws Comp uter MK Xxii Egpws Conf iguration ModuleGPS Antenna OAT Sensor Smart Cable Pcmcia Interface MK Xxii Egpws Smart Cable Technical Characteris tics MK Xxii Egpws Configuration ModuleUnits Supplied Honeywell MK Xxii Egpws Installation Manual Installation and Acces sories Kits New Egpws installation with Internal GPS2 RS-232 Cable Smart Cable Terrain Database Card s Flight History Card Annunciators & Switc h/Annunciators GPS Antenna & cableCircuit Breaker Cockpit Speaker Opti onal Tools Required Crimping Tool P1, P 2, P3 Contact Positioner P 1, P2, 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 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 GPS Antenna Installat ion OAT Sensor Installatio nCockpit Annunciators / Switches GPS Antenna location Description Egpws cautionGPWS G/S Cancld Location Gpws warning red & Gpws alert amber 8 MK Xxii Egpws Annunciators/Switches Location Inhibit Switch Functio ns and Selection Low Altitude ModeTerrain Inhibit 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 Chassis Ground System Wiring/ Electr ical InterfacesPrimary Power Input Serial Outputs Analog and Digital Inp utsDiscrete Inputs Audio Output Discrete Outputs Configurable Interface s Category 1 Aircraft / Mode Type SelectAircraft / Mode Type 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 Example Display Input Control GroupOutput 429 Bus Group 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 7.3 TA&D Alternate Pop-up Category 7 Options Select Group #1Steep Approach Not Available in the Mk Bank Angle Callout Enabling Peaks ModeObstacle Awareness 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 Landing Gear Discrete Weight on Wheels WOW DiscreteAudio Inhibit Discrete Autopilot Engaged Discrete Glideslope Cancel DiscreteMode 6 Low Volume Discrete Glideslope Inhibit Discrete Terrain Awareness InhibitSelf Test Discrete Low Altitude Mode Select Discrete Timed Audio Inhibit DiscreteOutput Discretes Lamp Format Gpws Inop Discrete TAD Inop DiscreteGpws Warning 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 Harness Checkout and Power Check Unit InstallationEgpwc Initialization a nd Configuration 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 Certification Procedur e Equipment Compatibi lity Equipment LocationFAA Requirements Ground Test Failure Modes, Effects , and Safety Analysis Flight TestPilots Guide 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 System Overview Introduction Part NumberPurpose Signal Interfaces Primary Power InputElectrical Interface Introduction Chassis Ground DC Analog Inputs Radio AltitudeLOW Level Glideslope Localizer Deviation or LOW Level Glideslope Validity Outside AIR Temperature Configuration Defined DC Inputs2.4 Barometric Altitude AC Analog Inputs 2.7.1Synchro Roll Attitude 2.7.2 Configuration Defined Synchro Inputs Signal Timing Reference Inputs 2.9 Arinc 429/575 Digital Serial BUS Inputs GPS RS-422 Digital Serial BUS Serial Port 2.9.1 RS-232 / RS-422 Digital Serial BUS InputsGPS RS-232 Digital Serial BUS Serial Port +28 VDC Discrete Characteristics AIR Data RS-232 Digital Serial BUS Serial PortAIR Data RS-422 Digital Serial BUS Serial Port SCI Range RS-422 Digital Serial BUS Serial Port GPS Antenna Input Configuration Module InterfaceGround Discrete Characteristics Monitor Output Characteristics Discrete Output CharacteristicsOAT Voltage Reference Output Lamp Driver Outputs High Level Speaker Audio Output LOW Level Interphone Audio OutputArinc Digital Serial Output Busses Arinc 429 Output BUS Front Panel Test Interface 2.18.1 RS-232 Maintenance Port Serial PortArinc 453 Output BUS GSE Present Discrete Input Front Panel Status IndicatorsPcmcia / Smartcable Port Aircraft Application Data Configuration TypesConfiguration Selection Instruction Signal SelectionTable E 3 Category ID Selection Procedure Configuration Selection Tables Category 1, Aircraft / Mode Type Select Torque Type Table E Effectivity App Cfg Engine Torque Data Selection Fault Designation Engine 1 BUS Bus Type BasicFault Designation Engine 2 BUS Bus Type Basic 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 8 AS365 Dauphin N3 Torque Data Select 9 BellTorque Data Select 10 Bell Summary Data Torque Data Select 11 Bell 212/412 Summary Data Fault Designation Engine 1 BUS Torque Data Select 14 Coast Guard HH-65 Summary DataTorque Data Select 16 Common DC Torque Connection Summary Data Table E 3.1.2 AIR Data Input Select for Egpws Mkxxii Category 2, AIR Data Input SelectTable E Description Type Summary Data Configuration DataFault Designation AIR Data BUS Bus Type Basic Table E 3.1.2-3 AIR Data Input Select #3 Summary Data Connect to Channel Table E 3.1.2-4 AIR Data Input Select #4 Summary DataTable E 3.1.2-5 AIR Data Input Select #5 Channel 429RX2 Table E 3.1.2-6 AIR Data Input Select #6Channel 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 Position Input Type TableE Description 3.3Category 3, Position Input Select Fault Designation GPS BUS Bus Type Basic UTC Fault Designation Internal GPS Bus Type Basic Internal Fault Designation GPS BUS Bus Type Basic Table E 3.1.4 Altitude Callouts for Egpws Mkxxii Category 4, Altitude CalloutsApp Cfg Honeywell MK Xxii Egpws Installation Manual Category 5, Audio Menu Select Effectivity App Cfg 006Table E 3.1.5 Audio Menu Type Table E 3.1.5-128 Audio Menu Type 128 Basic Helicopter IDand TCF Disable Application Notes Category 6, Terrain Display SelectSection Overview Defined By Honeywell MK Xxii Egpws Installation Manual Table E KC Picture Bus Channel Table Table E 3.1.6-1 No Display TAD and TCF EnabledTable Table E 3.1.6-2 TA&D / TCF Disabled Fault Designation Display BUS Bus Type Basic Display Configuration Group 6 Collins PRO-LINE IITable Table E 3.1.6-3 Collins ProLine 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 Table E 3.1.6-10 Integrated Efis 40/50 Honeywell/Bendix Peaks Always EnabledDisplay Configuration Group 8 Integrated Efis 40/50 Honeywell MK Xxii Egpws Installation Manual Table E 3.1.6-12 Collins WXI-701/711, without Auto Range Integration note Pins Terrain Display BUS #1 453TX1Terrain Display BUS #2 Reference Name Table E 3.1.6-14 Bendix PPI-4A/4B without Auto Range Terrain Display BUS #2 453TX2 6.3-0OUTPUT 429 BUS Group Traceability 6.2-3 Display Input Control GroupReference Name PIN Function Table E 3.1.6-16 Bendix IN182A/IN812A Radar display RDR Reference section Pins Comments Output 429 Bus Group Table E Bendix IN842A/IN862A Radar display RDR Function ValueCategory 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 #2 Connect to DC811 #1 Display Input Control GroupChannel 422RX2 Honeywell MK Xxii Egpws Installation Manual SCI Bus RS-422 12K baud Table E 317 Options Select Group #1 Category 7, Options 1 SelectAltitude Reference6 Effectivity App Cfg True False WGS-84 Description Value Category 8, Radio Altitude Input SelectRadio Altitude Type Table E Description PIN Function Connection PIN Type Channel Designation Reference Table E 3.1.8-5 Radio Altitude Input Select Type 5 ALT Reference Summary Data Category 9, Navigation Input Select Table E 3.1.9 Navigation Input Select for Egpws MkxxiiTable E 3.1.9-0 Navigation Inputs Select Summary Data Connection PIN Type Fault Designation ILS BUS Bus T ype Basic Fault Designation ILS BUS Category 10, Attitude Input Select Attitude Input SelectTable E 3.1.10 Attitude Input Select for Egpws MK Table E 3.1.10-0 Attitude Input Select Type Table E 3.1.10-128 Attitude Input Select Type Connect to Fault Designation Ahrs BUSTable E 3.1.10-4 Attitude Input Select Type Fault Designation Ahrs BUS Bus Type Basic Category 11, Heading Input SelectHeading Input Select Table E Description Table E 3.1.11 Heading Input Select for Egpws MK Category 12, Windshear Input Select No WindshearEffectivity App Cfg 003 Table E 3.1.12 Windshear Input Select Category 13, Input / Output Discrete Type Select Input/Output Discrete Type Table E Table E 3.1.13-128 INPUT/OUTPUT Discrete Type Configuration Data Possible StatesState Table E 3.1.13-129 INPUT/OUTPUT Discrete Type Table E 3.1.14 Audio Output Level Volume SelectCategory 14, Audio Output Level Table E 3.1.15 Autorotation Threshold for Egpws MK Category 15, Autorotation ThresholdAutorotation Threshold Torque 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