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Honeywell MK VI MK VIII EGPWS Installation Design Guide Copyright 2003 Honeywell, Inc. All rights reserved. This document and all information and expression contained herein are the property of Honeywell International Inc., and is provided to the recipient in confidence on a “need to know” basis. Your use of this document is strictly limited to a legitimate business purpose requiring the information contained therein. Your use of this document constitutes acceptance of these terms.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Typed names constitute approval signatures. Actual signatures are on file at Honeywell in Redmond, WA.
Honeywell MK VI MK VIII EGPWS Installation Design Guide THIS PAGE INTENTIONALLY LEFT BLANK Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 4
Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE OF CONTENTS SECTION I – GENERAL INFORMATION ..........................................................................................................13 1.1 INTRODUCTION.........................................................................................................................................................13 1.2 APPLICABILITY...........................................................................................................
Honeywell MK VI MK VIII EGPWS Installation Design Guide 2.1 INTRODUCTION .......................................................................................................................................................29 2.2 UNPACKING AND INSPECTING THE EQUIPMENT ......................................................................................................29 2.3 EQUIPMENT INSTALLATION ..............................................................................................................
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.4.6 Instructions .........................................................................................................................................................62 3.5 CATEGORY 3 – POSITION INPUT SELECT ................................................................................................................63 3.5.1 ARINC 743 Format.........................................................................................................
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.11.7 Digital – ARINC 429 Dual IOC buses (Cat. 9 ID 250 - 255) ...........................................................................96 3.11.8 Instructions .......................................................................................................................................................97 3.12 CATEGORY 10 – ATTITUDE INPUT SELECT ...................................................................................................
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.15.2.11 Terrain Display Select #1 & #2 Discrete....................................................................................................................... 111 3.15.2.12 Terrain Pop up Discrete ................................................................................................................................................ 112 3.15.3 Instructions ...............................................................................
Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX A - CUSTOMER WORKSHEET .....................................................................................................137 APPENDIX B - SAMPLE WIRING DIAGRAMS ...............................................................................................141 APPENDIX C – WINVIEWS OPERATION INSTRUCTIONS.........................................................................146 APPENDIX D - VENDOR CONTACT INFORMATION........................
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION I GENERAL INFORMATION Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 11
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION I – GENERAL INFORMATION SECTION I – GENERAL INFORMATION ..................................................................................................................... 13 1.1 INTRODUCTION.............................................................................................................................................................. 13 1.2 APPLICABILITY...........................................................................
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION I – GENERAL INFORMATION 1.1 Introductio n The Honeywell MK VI/MK VIII Enhanced Ground Proximity Warning System (MK VI/MK VIII EGPWS) provides alerts and warnings to prevent controlled flight into terrain (CFIT).
Honeywell MK VI MK VIII EGPWS Installation Design Guide 1.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 1.5 Description of Equipment The MK VI/MK VIII EGPWS is a rack mount ground proximity warning (GPWS) and terrain awareness and warning (Class A TAWS) computer.
Honeywell MK VI MK VIII EGPWS Installation Design Guide approximately 35 days. GPS initialization time should be less than 3 minutes with active RTC data. If the capacitor has discharged then GPS initialization time may be as long as 10 minutes. 1.5.4 GPS Anten na and Cabling EGPWS installations using the internal GPS require a GPS antenna and cabling. The GPS antenna should meet the following qualifications: Frequency: Impedance: Gain: Power: Qualification: 1575.42 MHz 50 ohms 33 dB max, 26.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 1.5.5 OAT Senso r The EGPWS uses a separate OAT sensor (Outside Air Temperature) to measure outside air temperature on aircraft that do not have another compatible source of outside air temperature. Outside Air Temperature is used by the EGPWS along with pressure altitude in the Geometric Altitude computation.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 1.6 Technical C haracteristics MK VI / VIII EGPWS TSO Compliance: Physical size (HxWxD): Weight: Mounting: Temperature (operational): Altitude range: Cooling: Shock: Power Consumption (28 VDC): (MK VI) TSO-C92c, TSO-C151b Class A (MK VIII) TSO-C92c, TSO-C151b Class A, TSO-C117a Application for UKCAA Spec 14 is in process 6.20” x 3.04” x 10.30” 3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide The MK VI EGPWS is normally shipped with an AMERICAS Terrain database. When ordering a MK VI EGPWS that will be operating in the ATLANTIC or PACIFIC1 region the specific Terrain database must be specified with the order. NOTE 1: Terrain Database cards for the ATLANTIC or PACIFIC region are no longer required to be ordered separately. NOTE 2: -XXX defines Application software version. 1.7.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Bendix/King 071-04003-0002 Computer Mounting Tray 1 EA 405-0383-001 1.8.2 RS-232 Cab le The MK VI/MK VIII EGPWS RS-232 Cable can be ordered using the following part numbers: NOTE: The RS-232 Cable can be built by the Installer/Operator per the description in Section 4.4.2. Vendor Name Vendor P/N Description QTY UM Honeywell P/N Honeywell 704-2617-001 RS-232 Cable 1 EA 704-2617-001 1.8.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Pic Wire&Cable Pic Wire&Cable ECS ECS Emteq D5102QX D771553 4122021 312402 D70-022402T-01 M17/176-00002 M83536/6-022M M12883/44-01 Hi Temp Quadraxial MIL-STD 1553 Data Bus ARINC 453 cable (2 shields) ARINC 453 cable (3 shields) ARINC 453 cable Military Specification Relay, 4PDT (Note 1) Relay, Socket (Note 1) A/R A/R A/R A/R A/R A/R A/R A/R EA EA EA EA EA EA EA EA Note 1: Recommended in EFS 40/50 Installation Manual. 1.9.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 1.9.4 Annunciato rs & Switch/Annunciators The devices shown below are West Coast Specialties and Staco switch/annunciators and are representative of those used in some installations. However, there are other comparable devices on the market that may be substituted at the installer/customers choice. The installer/customer is cautioned to verify regulatory approval of the annunciation devices installed. See Appendix D for Vendors. A.
Honeywell MK VI MK VIII EGPWS Installation Design Guide West Coast Spec. West Coast Spec. STACO 90-81401-011 90-81401-012 61406-007 (4) (5) GPWS FLAP OVERRIDE (1) GPWS – BELOW G/S – GPWS FLAP OVRD – G/S CANCLD (2) GPWS – BELOW G/S – GPWS FLAP OVRD – GPWS INOP (3) GPWS FLAP OVRD – G/S CANCLD (4) GPWS INOP – G/S CANCLD – GPWS FLAP OVRD (5) GPWS FLAP OVRD – GPWS INOP 1 1 1 EA EA EA C.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Rosemount Rosemount Rosemount Rosemount Rosemount 102EH2BH 102EH2EB 102JE2FG 129H-500 129G-500 Dual element, heated Dual element, heated Triple element, heated Single element, unheated Dual element, unheated 1 1 1 1 1 EA EA EA EA EA 1.10 Tools Requ ired 1.10.1 Crimping T ool - P1, P2, P3 Description UM QTY Vendor Name & Part Number Hand Crimping Tool Hand Crimping Tool Hand Crimping Tool EA EA EA 1 1 1 Positronic Ind.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 1.10.
Honeywell MK VI MK VIII EGPWS Installation Design Guide THIS PAGE INTENTIONALLY LEFT BLANK Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 26
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION II INSTALLATION Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 27
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION II - INSTALLATION SECTION II - INSTALLATION ........................................................................................................................................ 29 2.1 INTRODUCTION.............................................................................................................................................................. 29 2.2 UNPACKING AND INSPECTING THE EQUIPMENT ...........................................
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION II - INSTALLATION 2.1 Introductio n This section contains suggestions and factors to consider before installing the Enhanced Ground Proximity Warning System. Close adherence to these suggestions will assure satisfactory performance from the equipment. NOTE The conditions and tests performed on this article are minimum performance standards.
Honeywell MK VI MK VIII EGPWS Installation Design Guide installed in a location convenient for operation, inspection, and maintenance, and in an area free from excessive vibration, heat, and noise generating sources. The MK VI and MK VIII EGPWS have an internal heater blanket therefore they can be mounted outside the heated area of the aircraft. The computers have been qualified for operation up to 50,000 feet and -55°C using the heater blanket.
Honeywell MK VI MK VIII EGPWS Installation Design Guide C. Mount the EGPWS mounting tray in the aircraft radio rack or other location using the four screw mounting holes. Match drill the mounting holes using the Mounting Tray as a template. D. Ensure that the mounting tray is electrically bonded (less than 10 milli-ohm to aircraft ground). E. Slide the EGPWS unit in the mounting tray, and secure it using the Hold Down latch. F.
Honeywell MK VI MK VIII EGPWS Installation Design Guide D. Position Slide Lock and Spring Clip onto connector. E. Install Backshell Housing onto connector. The Ground wire (used for ESD discharge) is terminated with shielded pigtails inside the backshell to the P2 connector. F. Organize and dress wire exiting from the backshell, route Configuration Module wires in a coil. Install Cable Clamp, do not tighten Cable Clamp screws. G. Secure the Configuration Module to the connector using screws provided.
Honeywell MK VI MK VIII EGPWS Installation Design Guide INSTALLATION ASSEMBLY SEQUENCE STEP 1 Install all MK VI/MK VIII system aircraft wiring to this connector using items 1.2 (Crimp Contacts) and item 1.1 (Connector). See figure 2.1-1 below. FIGURE 2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide STEP 2 Wire item 2.0 (Configuration Module). This part will replace item 1.4 (Backshell plate). Install the pre-crimped colored wires into item 1.1 (Connector) as shown in figure 2.1-2 below. FIGURE 2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide STEP 3 Position item 1.7 (Slide lock) onto wired connector as shown in figure 2.1-3 below: FIGURE 2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide STEP 4 Install item 1.3 (Backshell Housing) onto connector using item 1.8 (Screws) as shown in figure 2.1-4 below: Ground Wire (used for electrostatic discharge {ESD} protection) is terminated with shielded pigtails of wires at this connector. FIGURE 2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide STEP 5 Install item 1.6 (Spring Clip) as shown figure 2.1-5 below: FIGURE 2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide STEP 6 Organize and dress wiring exiting from backshell. Route Configuration Module wires exiting from connector, then coil as shown in figure 2.1-6 below. Install item 1.9 (Cable Clamp) as shown. Do not tighten screws yet. FIGURE 2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide STEP 7 Secure Configuration Module to connector assembly using item 1.5 (Screws) as shown in figure 2.1-7 below. Tighten Cable Clamp screws as required. FIGURE 2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 2.3.6 GPS Anten na location The GPS antenna should be mounted on top of the fuselage in the centerline of the aircraft. Avoid mounting the antenna near any projections, the propeller, and the T-tail of the aircraft, where shadows could occur. 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.
Honeywell MK VI MK VIII EGPWS Installation Design Guide NOTE: All lights 1. Refer to Honeywell Product Specification 965-1176-601 for additional information and for electrical loads specification. 2. All lights are +28 VDC, dual bulb, sun light readable, non-flashing. 3. In the “OFF” condition, all lights have dark background with visible nomenclature for action. 4. If desired the lights may be put on a “dimmer” circuit for night operation. 2.3.10.
Honeywell MK VI MK VIII EGPWS Installation Design Guide This assembly is illuminated with white background and activated after the flight crew has initiated the manual selection of the EGPWS terrain display for the associated cockpit display. This assembly also includes a momentary switch that will activate EGPWS Terrain display feature.
Honeywell MK VI MK VIII EGPWS Installation Design Guide TERR FAIL This light should be located within at least one crew member’s “field of view” or with other system INOP lights of similar importance. Note: Annunciators are available with split legend GPWS FAIL / TERR FAIL in one assembly. It is recommended that this light not be located in the flight crew’s “primary field of view”.
Honeywell MK VI MK VIII EGPWS Installation Design Guide FIGURE 2-2 MK VI/MK VIII EGPWS OUTLINE Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 44
Honeywell MK VI MK VIII EGPWS Installation Design Guide FIGURE 2-3 MK VI/MK VIII EGPWS MOUNTING TRAY Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 45
Honeywell MK VI MK VIII EGPWS Installation Design Guide THIS PAGE INTENTIONALLY LEFT BLANK Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 46
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION III SYSTEM PLANNING Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 47
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION III – SYSTEM PLANNING SECTION III – SYSTEM PLANNING..............................................................................................................................51 3.1 INTRODUCTION.............................................................................................................................................................. 51 3.2 SYSTEM WIRING/ ELECTRICAL INTERFACES ................................................
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.8.2 Terrain Display Configuration Group ..................................................................................................................70 3.8.3 Display Input Control Group ................................................................................................................................70 3.8.4 Output 429 Bus Group .........................................................................................................
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.14.2 Dual ARINC 429 BUS (Cat. 14 ID 253,254,255)..............................................................................................102 3.14.3 Instructions........................................................................................................................................................102 3.15 CATEGORY 13 – INPUT / OUTPUT DISCRETE TYPE SELECT ..............................................................................
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION III – SYSTEM PLANNING 3.1 Introductio n This section provides information for selecting features and wiring the electrical interfaces of the MK VI/MK VIII EGPWS. Appendix E Section 5.2 groups features (functions) into sets called Categories. This document follows the Category structure of the Appendix E. It provides descriptions of the features and instructions for selecting features and for determining the correct wiring.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.2.2 Chassis Gr ound Chassis ground provides a redundant metal connection and should not be used as a normal current carrying conductor. Chassis ground should be connected as follows: Pin Signal J1-42, J1-53 GND Pins J1-42 and J1-53 are both connected to chassis ground internally. It is not necessary to tie them both to ground in the aircraft wiring.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.2.7 Audio Outp ut The audio outputs consist of both an 8-ohm amplifier and a transformer isolated 600-ohm output. Audio output messages are provided as specified in the selected Audio Menu (Category 5) when inputs are valid and the audio inhibit discretes are not active. When audio inhibit is enabled, the output discrete(s) associated with suppressed message(s) are active. 3.2.8 Discrete Ou tputs The MK VI/MK VIII EGPWS provides for up to twelve 0.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.3 Category 1 - Aircraft / Mode Type Select Category 1 specifies the general aircraft type, warning mode differences, bank angle alert curve, fixed or retractable gear, and 3500 ft or 2000 ft min runway length (as an option for MK VIII EGPWS only). Appendix E Tables 5.2 and 5.3.1 include some information required by MK VI/MK VIII EGPWS development personnel and not pertinent to the installation design process.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.3.4 Mode 3 typ e Two Mode 3 alert curves are defined, GA (Turboprop) and Bizjet (Turbofan). The GA (Turboprop) Mode 3 curve is equivalent to the (classic) MK VI Mode 3 curve. The Bizjet (Turbofan) Mode 3 curve is equivalent to the MK V and MK VII EGPWS Mode 3 curves. 3.3.5 Mode 4 typ e Mode 4A (Too Low Gear) expanded alert transition occurs at 178 knots for GA Fast aircraft, 148 knots for GA Slow aircraft, and 190 knots for Bizjet aircraft.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.3.7 Runway Le ngth (MK VIII EGPWS only) Two minimum runway length options are defined for Bizjet (Turbofan) aircraft. A 2000 ft minimum runway length or a 3500 ft minimum runway length may be chosen based on aircraft type as is identified in Appendix E Table 5.3.1. This option does not effect the mode curves as discussed above, and it is only available on MK VIII EGPWS. 3.3.8 Instruction s Using Appendix E Tables 5.2 and 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.4 Category 2 – Air Data Input Select Category 2 defines the Air Data interface. The Air Data input currently defines 4 analog and 6 digital air data types. Appendix E Table 5.3.2 defines the Air Data interface options and identifies the first MK VI/MK VIII EGPWS version in which the option was available (see the Effectivity entry). Appendix E Tables 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide EGPWS MK VI / MK VIII Uncorrected Barometric Altitude J1 Analog Air Data Computer (+) 62 Altitude Out (-) 43 Signal Common Baro Altitude Valid +28V BIT Out 9 +5V Excitation 25 Temp. Input (+) 63 500 ohm Temperature Probe (-) 44 Chassis Ground 53 Analog-ADC.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.4.2 Digital – AR INC 429 (Cat. 2 ID 5, 1, 6, 13) Air Data Type 1 is a low speed, digital ARINC 429 signal having the air data labels 203, 206, 212, and 213. Air Data Type 5 is a low speed, digital ARINC 429 signal having the air data labels 203, 204, 206, 212, and 213. Air Data Type 6 is a low speed, digital ARINC 429 signal having the air data labels 203, 206, and 213.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.4.3 Digital –AR INC 575 (Cat. 2 ID 2) Air Data Type 2 (ADC-80 or equivalent) is a low speed, digital ARINC 575 signal having the air data labels 203, 206, 212, and 213. EGPWS MK VI / MK VIII ARINC 575 Air Data Bus J2 ARINC 575 Air Data A 39 A ARINC 575 Bus - Hi B 38 B ARINC 575 Bus - Lo ARINC575-ADC.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.4.4 Shadin 200 0 (Cat. 2 ID 10) Air Data Type 10 (Shadin 2000 or equivalent) is a low speed, digital ARINC 429 signal having the air data labels 203, 204, 206, and 212. Total Air Temperature is from a dedicated (EGPWS) 500-ohm probe using +5 volt excitation from the MK VI/MK VIII EGPWC.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.4.5 Digital – AR INC 429 Dual IOC Buses (Cat. 2. ID 255) Air Data Type 255 (IOC bus or equivalent) is a dual, high speed, digital ARINC 429 signal having the air data labels 203, 204, 206, 210, 212, and 213. ID 255 may only be used in conjunction with other IOC bus selections for categories 6, 8, 9, 10, 11 and 12.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.5 Category 3 – Position Input Select Category 3 defines the Global Position System bus type and interface. The EGPWS requires a GPS with 8 channels minimum and RAIM capability. Appendix E Table 5.3.3 defines the Position Input Select options and identifies the first MK VI/VIII EGPWS version in which the option was available (see the Effectivity entry). Appendix E Tables 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.5.4 ARINC 429 BUS (Cat. 3 ID 0,1,4,5,10-13) EGPWS MK VI / MK VIII ARINC 429 GPS Bus J2 ARINC 429 GPS A 25 A ARINC 429 Bus - Hi B B ARINC 429 Bus - Lo 8 ARINC429-GPS.vsd Vendor Model Collins GNLU-910A Collins GPS-4000 Cat 3 429 GPS Alt ARINC Bus 1 Bus 2 ID Speed Ref.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.5.5 RS-232 Tra nsmit-Receive, 9600 baud (Cat. 3 ID 3) EGPWS MK VI / MK VIII RS – 232 GPS Bus J2 RS-232 GPS NC TX 45 RX 29 TX – Transmit Out CM 28 GND RX – Receive In RS232-GPS.vsd Vendor Model GARMIN GNS430/530 2 GPS Alt ARINC NS3 Ref. 743/743A EW MSL N/A MSL MSL RS-232 RX TX GND Note 3 P4001-56 Chassis N/A OK P9002-13 Chassis N/A OK P941-6 Chassis Software Version 2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.5.6 Dual ARINC 429 BUS (Cat. 3 ID 253 & 255) NOTE: If GPS #2 is not installed in the aircraft, then use ID 4 or GPS bus #1 must be connected in parallel to both EGPWS GPS input ports. NOTE: Non-IOC aircraft can use ID 253 or 255 to activate dual GPS inputs for redundancy and improved system availability, but the interface must have dual High Speed 743A GPS, and this cannot be used if using Category 10 ID 5 or Category 11 ID 2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.6 Category 4 – Altitude Callouts Category 4 defines the Altitude Callout menu choices and Smart ‘500’ Callout selection. Appendix E Table 5.3.4 defines the Altitude Callout Menu options and identifies the first MK VI/MK VIII EGPWS version in which the option was available (see the Effectivity entry).
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.7 Category 5 – Audio Menu Select Category 5 defines four Audio Menu options. Retractable Gear aircraft, Type 0 (basic) and Type 1 (alternate) and Fixed Gear aircraft, Type 2 (basic) and Type 3 (alternate). Appendix E Table 5.3.5 defines the Audio Menu select options and identifies the first MK VI/MK VIII EGPWS version in which the option was available (see the Effectivity entry). Appendix E Tables 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.8 Category 6 – Terrain Display Select Category 6 defines the Terrain Display options available. TA&D and TCF mode enabling/disabling is controlled by Category 6. Peaks mode availability is controlled by Category 6 since its availability is determined by the display configuration. Peaks mode enabling/disabling is controlled by Category 7. Each of the options controlled by Category 6 is described below. Appendix E Table 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.8.2 Terrain Dis play Configuration Group This option provides the ability to specify the type of Terrain Display compatible with the aircraft configuration. A definition of each of the entries in the Display Configuration Group tables is provided in the table below. Function Value Reference section Display Type Display manufacturer, model, etc. Sweep Type The type of sweep used for terrain data (fan, standard, etc.
Honeywell MK VI MK VIII EGPWS Installation Design Guide In some installations where the Radar (Terrain) displays are controlled from one source, the Range input buses into the EGPWS must be paralleled to satisfy EGPWS dual input requirements. CONN PIN # REFERENCE NAME PIN FUNCTION J1-32 GND_DISC_12 Reference 6.6.18 J1-31 GND_DISC_13 Reference 6.6.
CAGE CODE: 97896 SCALE: NONE SIZE: A No connection 28V Lamp Dimming Bus N6 B B 36 B 57 A 56 B 59 A 58 DWG NO: 060-4314-150 REV: MK VI 965-11X0-020 or later. MK VIII 965-12X0-020 or later. Terrain INOP (out) 55 TERR INHIB TERR INOP Note: GNS-XLS will not perform auto pop-up during Alert.
CAGE CODE: 97896 SCALE: NONE SIZE: A B 57 A 56 B 59 A 58 J1 B 40 A 41 No connection DWG NO: 060-4314-150 REV: MK VI 965-11X0-020 or later. MK VIII 965-12X0-020 or later. Terrain INOP (out) 55 28V Lamp Dimming Bus TERR INHIB TERR INOP Note: For interface and operation of the Honeywell KMD 540/550/850 see Honeywell Installation Manual P/N 006-10608-0001 Alternate Action Lamp Test 429 Out Honeywell KMD 540/ 550/850 KMD540-1.
CAGE CODE: 97896 SCALE: NONE SIZE: A Lamp Test 28V Lamp Dimming Bus DWG NO: 060-4314-150 REV: MK VI 965-11X0-020 or later. MK VIII 965-12X0-020 or later. Terrain INOP (out) 55 Note: For interface and operation of the Honeywell Grimes TRA-45A see Honeywell TRA-45A Equipment Installation Manual P/N 34-40-01 Alternate Action 80-5145-X-2 TRA45.
CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 open TERR momentary A B 57 A 56 REV: MK VI 965-11X0-020 or later. MK VIII 965-12X0-020 or later.
CAGE CODE: 97896 SCALE: NONE SIZE: A NC B 57 A 56 B 59 A 58 DWG NO: 060-4314-150 REV: MK VI 965-11X6-004 or later. MK VIII 965-12X6-004 or later.
CAGE CODE: 97896 SCALE: NONE SIZE: A B 40 DWG NO: 060-4314-150 REV: MK VIII 965-12X0-020 or later. Terrain Inhibit (in) 12 58 ARINC 453 Symbol A Generator Out B 59 ARINC 429 Range #2 In A 41 J1 Lamp Test 28V Lamp Dimming Bus Alternate Action TERR INHIB 25 B B 36 PILOT 7017000 EGPWS Cont 429 Out 453 Bus In 7014300 453 Bus In 7014300 25 B 12 A 42 B 41 A Honeywell Primus 1000 Primus1000.
CAGE CODE: 97896 SCALE: NONE SIZE: A B 57 A 56 B 59 A 58 DWG NO: 060-4314-150 REV: MK VI 965-11X0-020 or later. MK VIII 965-12X0-020 or later.
CAGE CODE: 97896 SCALE: NONE SIZE: A B 57 A 56 B 59 A 58 DWG NO: 060-4314-150 REV: MK VI 965-11X0-020 or later. MK VIII 965-12X0-020 or later. Terrain INOP (out) 55 Terrain Inhibit (in) 12 Terrain Display Select (out) 54 NC J1 B 40 A 41 Alternate Action ON TERR TERR INHIB TERR INOP momentary Lamp Test 28V Lamp Dimming Bus H T/R Data Bus L T/R Data Bus PPI4A4B.
CAGE CODE: 97896 SCALE: NONE SIZE: A 51 TERRAIN POP-UP OUT DWG NO: 060-4314-150 REV: 12 32 TERRAIN INOP TERRAIN INHIBIT SWITCH IN TERRAIN SELECT SWITCH IN 54 TERRAIN SELECT RELAY OUT 55 60 40 +28VDC POWER IN +28VDC POWER IN SEE NOTE 3. 58 59 J1 41 37 36 40 J2 KCPB A OUT KCPB B OUT NO. 2 DISPLAY RANGE 429 A IN NO. 1 DISPLAY RANGE 429 A IN NO. 1 DISPLAY RANGE 429 B IN NO.
CAGE CODE: 97896 SCALE: NONE 51 60 40 54 TERRAIN POP-UP OUT +28VDC POWER IN +28VDC POWER IN TERRAIN SELECT RELAY OUT SIZE: A 55 12 32 TERRAIN INOP TERRAIN INHIBIT SWITCH IN TERRAIN SELECT SWITCH IN SEE NOTE 3. 58 59 J1 41 37 36 40 J2 KCPB A OUT KCPB B OUT NO. 2 DISPLAY RANGE 429 A IN NO. 1 DISPLAY RANGE 429 A IN NO. 1 DISPLAY RANGE 429 B IN NO.
CAGE CODE: 97896 SCALE: NONE SIZE: A B 57 A 56 B 59 A 58 DWG NO: 060-4314-150 REV: MK VI 965-11X0-020 or later. MK VIII 965-12X0-020 or later. Terrain INOP (out) 55 Terrain Inhibit (in) 12 Terrain Display Select (out) 54 NC J1 B 40 A 41 Alternate Action ON TERR 8 TERR INHIB TERR INOP momentary 6B 9 Lamp Test 28V Lamp Dimming Bus H T/R Data Bus L T/R Data Bus WXI-701.
J1 CAGE CODE: 97896 B 59 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: J1 B 57 A 56 MK VI 965-11X0-020 or later. MK VIII 965-12X0-020 or later. Terrain Display Select (out) 49 ARINC 453 Video #2 To WX R/T 28V EGPWS PWR Bus Note: For interface and operation of the Collins Proline II displays see Collins SIL 2-99 ON ARINC 429 Range CollinsP2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide HONEYWELL MK VI-VIII EGPWS 965-1XXX-0XX PROLINE 4 INTERFACE MK VI-VIII EGPWS Category 6, ID 5 or 6 #1 - IOC (ICC-4000) J2 P1 P * ICC-851A pins 13 & 14 P RANGE INPUT (A) 37 3* RANGE INPUT (B) 36 4* LA-GP-5 bus (Label 271) #2 - IOC (ICC-4000) P1 P * ICC-851A pins 13 & 14 P RANGE INPUT (A) 41 3* RANGE INPUT (B) 40 4* RA-GP-5 bus (Label 271) +28 VDC TERR J1 MOM TERR SELECT #1 32 70!* * In the OEM installations a single weather radar 4
DC-810 J1 CAGE CODE: 97896 J1A 1 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: +28V GND PN 7003400-802 Radar Serial Data WX/TERR PICTURE BUS IN 3 5 J2A 22 23 1 2 J1B 78 Controller Serial Data 77 LEFT SYMBOL GENERATOR SG-802 GND WX pushbutton 23 34 Controller Serial Data 35 LEFT DISPLAY CONTROLLER L H L H L H L H L-EFIS +28 VDC TERR L-EFIS +28 VDC L H L H RT RELAY SELECT RT DISP SELECT DISPLAY BUS #2 Radar R/T WU-650 (HPN 7008470-XXX) Right EFIS Control Bus e f q
J1 CAGE CODE: 97896 J1A 1 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: +28V GND PN 7013788-806 Radar Serial Data WX/TERR PICTURE BUS IN 1 8 J2A 32 33 30 31 J2B 67 Controller Serial Data 68 LEFT SYMBOL GENERATOR SG-806 GND WX pushbutton 23 34 Controller Serial Data 35 LEFT DISPLAY CONTROLLER DC-811 L H L H L H L H L-EFIS +28 VDC TERR L-EFIS +28 VDC L H L H TERRAIN 58 DISPLAY 59 BUS #1 LT DISP Right EFIS Control Bus e f q Picture Bus Shield m Left EFIS n Control B
CAGE CODE: 97896 SCALE: NONE SIZE: A B 57 A 56 B 59 DWG NO: 060-4314-150 Terrain INOP (out) 55 NC J1 A 58 B 42 A 43 B 40 A 41 Lamp Test 28V Lamp Dimming Bus REV: Note: For interface and operation of the Universal MFD-640 see Universal Avionics Multi-Function Disaply Installation Manual 34-20-02 Alternate Action TERR INHIB TERR INOP B 36 Video in * Display Control In * Range out * MFD-640 6402-1XXX1-0X Universal MFD-640 * configurable by MFD-640 67 80 B 68 70 ohm termination 81
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.9 Category 7 – Options Select Group #1 Category 7 enables/disables the following Options: Steep Approach, TA&D Alternate Pop Up, Peaks Mode, Obstacle Awareness, Bank Angle, Flap Reversal, and GPS Altitude Reference. Appendix E Table 5.3.7 defines the Options Select group and identifies the first MK VI/VIII EGPWS version in which the option was available (see the Effectivity entry). 3.9.
Honeywell MK VI MK VIII EGPWS Installation Design Guide alerts if the boundaries of these envelopes conflict with obstacle elevation data in the obstacle database (similar to the Terrain Awareness function). Obstacle data is currently available for North America and parts of the Caribbean and Europe. 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 & TCF must be enabled if Obstacle Awareness is enabled. 3.9.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.9.8 Instruction s Review the sections above for information on Steep Approach, TA&D Pop Up, Peaks Mode, Obstacle Awareness, Bank Angle, Flap Reversal, and GPS Altitude Reference. Using Appendix E Tables 5.2 and 5.3.7 as described above, select the preferred Category 7 (Options Select Group #1) ID that matches the aircraft configuration, features preferences and version (part number) being installed.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.10 Category 8 – Radio Altitude Input Select Category 8 defines the Radio Altitude and Decision Height interface. 3.10.1 Radio Altitu de Input Appendix E Table 5.3.8 defines the Radio Altitude Types and identifies the first MK VI/MK VIII EGPWS version in which the option was available (see Effectivity entry). Appendix E Tables 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.10.4 Analog Rad io Altitude Interface (Cat. 8 ID 0,1,3,4) J1 EGPWS MK VI / MK VIII Analog Radio Altitude Radio Altimeter R/T + ARINC 552, ALT 55, - RT-200/300 (+) 64 (-) 45 Valid Radio Altitude Valid +28V 29 Radio Altimeter Indicator DH wiper DH Discrete (Gnd) 33 DH out Analog-RA.vsd Vendor Model R/T Collins ALT 55 Honeywell HG7502(BC) Cat. Ind.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.10.6 Instruction s Using Appendix E Tables 5.2, 5.3.8 and 5.3.8-x as described above, select the Radio Altitude Input Type that matches the aircraft configuration, features preferences and version (part number) being installed. Record the ID number for the Radio Altitude Type from Appendix E Table 5.3.8 under the Ident No. heading for Step (Category) 8 in Appendix E Table 5.2. Using the Radio Altitude Type number from Appendix E Table 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.11 Category 9 – Navigation Inputs Select Category 9 selects the Glideslope and Localizer Deviation interfaces and Glideslope Validity and ILS Tuned discretes. Appendix E Table 5.3.9 defines the Category 9 Navigation Inputs Select options (called Navigation Inputs Select Types) and identifies the first MK VI/VIII EGPWS version in which the option was available (see the Effectivity entry). Appendix E Tables 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.11.5 Analog Glid eslope Interface (Cat.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.11.6 Digital Glid eslope / Localizer / ILS Select Interface (Cat. 9 ID 2,3,4) EGPWS MK VI / MK VIII J2 ARINC 429 ILS ILS 429 Bus A ARINC 429 B Low Speed A 22 B 5 Digital-ILS.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.11.8 Instruction s Using Appendix E Tables 5.2, 5.3.9 and 5.3.9-x as described above, select the Navigation Input Select Type that matches the aircraft configuration, feature preferences, and version (part number) being installed. Record the ID number for the Navigation Inputs Select Type from Appendix E Table 5.3.9 under the Ident No. heading for Step (Category) 9 in Appendix E Table 5.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.12 Category 1 0 – Attitude Input Select Category 10 defines the Roll Angle interface. Appendix E Table 5.3.10 defines the Attitude Input Select type and identifies the first MK VI/VIII EGPWS version in which the option was available (see the Effectivity entry). Appendix E Tables 5.3.10-x, where x is the Attitude Input Select Type number, define the format and electrical interfaces required to support each Attitude Input Select Type. 3.12.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.12.3 Digital Pitc h & Roll Angle (ARINC 429 High Speed) (Cat. 10 ID 5 & 6) EGPWS MK VI / MK VIII J2 ARINC 429 AHRS AHRS 429 Bus A ARINC 429 B High Speed A 23 B 6 Digital-AHRS.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.13 Category 1 1 – Heading Input Select Category 11 defines the Magnetic Heading interface. Appendix E Table 5.3.11 defines the Heading Input Select types and identifies the first MK VI/VIII EGPWS version in which the option was available (see the Effectivity entry). Appendix E Tables 5.3.11-x, where x is the Heading Input Select number, define the format and electrical interfaces required to support each Heading Input Select Type. 3.13.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Note 3: 2 #2 Heading Output 3 Do not use #2 output, reserved for autopilot only. The KI-525 must have the proper mod for HEADING TRANSMITTER output. The Heading valid output at J2-P needs to be converted from ground active output to +28V active output using a external relay for use with EGPWS. 3.13.3 Digital – AR INC 429 AHRS Input (Cat.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.14 Category 1 2 – Windshear Input Select Category 12 defines the Windshear interface. Appendix E Table 5.3.12 defines the Windshear Input Select options and identifies the first MK VI/VIII EGPWS version in which the option was available (see the Effectivity entry). 3.14.1 No Windsh ear Select ID 0 (No Windshear) for all aircraft configurations without Windshear. Windshear options will be added as new installations types are propagated. 3.14.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.15 Category 1 3 – Input / Output Discrete Type Select Category 13 defines the input and output discretes not defined as part of any of the other Categories. Appendix E Table 5.3.13 defines the Input/Output discretes options and identifies the first MK VI/VIII EGPWS version in which the option was available (see the Effectivity entry). 3.15.1 Input Discr etes The discrete inputs are defined in Appendix E Section 6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Ground seeking Landing Flap discrete active position: Flap Reversal (Category 7) False True Flap Discrete (J1-18) Landing Flap discrete = GND Flaps Up Flaps Down Flaps Down Flaps Flap Override = OVRD GND GND Flap Override = NORM Open Open Landing Flap Discrete = Open (or +28V) Cat. 13 ID 254/255 only * * Category 13 ID 254/255 must use this method for Flap Override. 3.15.1.
Honeywell MK VI MK VIII EGPWS Installation Design Guide FIXED LANDING GEAR/FLOAT AIRCRAFT ALTERNATE AIR SWITCH ARRANGEMENT (Example Shown: Twin Otter) Not LANDING P1 J1 FULL LANDING FLAP POSITION (16°-18°) 18 MK VI EGPWS COMPUTER Landing Flap Discrete (Gnd) LANDING FLAPS UP APPROACH FLAP POSITION (5°-7°) APPROACH FLAPS EGPWS 35 Landing Gear Discrete (+28) 40 60 Power Input: +28VDC AIRCRAFT +28VDC 3 AMP KRA 405B Adjustable Trip W* * KRA 405B Adjustable Trip pins W,V, & F.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.15.1.5 Glideslope Cancel Discrete The Glideslope Cancel discrete provides the crew with the capability to manually cancel Mode 5 alerts during an approach. The Glideslope Cancel latch is automatically reset when the aircraft descends below 30 feet or ascends above 2000 feet or by selecting a non-ILS frequency.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Discrete Position / Status Connector Pin Mode 6 Low Volume Low Volume = Gnd Not Low Volume = Open J1-13 3.15.1.8 Autopilot E ngaged Discrete For airplanes fitted with an Autopilot, additional Bank Angle mode protection is provided when the Autopilot is engaged. If the Autopilot is engaged the Bank Angle roll angle limit advances to 33 degrees from 50 degrees.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.15.1.11 Steep Appr oach Discrete #2 For some installations a Steep Approach bias can be optionally applied to the Mode 1 curves. If Steep Approach is enabled (Category 7) and the Steep Approach discrete is selected (Category 13), then fixed positive biases are added to both the Sinkrate curve (500 fpm), and the Pull Up curve (200 fpm). Category 7 enables the Steep Approach function for the installation.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Short-term current limit protection is provided on all drivers for output shorting conditions. Ground going output discretes may be connected together to produce a ‘wired OR’ function for the active low state of the outputs. If output discretes are ‘wire OR’d’ then diodes must be installed for isolation. Output discretes are intended to operate with +28 VDC lamp sources and will not operate with +5 VDC lamp sources. 3.15.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide (Lamp Format Type 2 definition) GPWS Warning discrete (J1-78) will activate during any Mode 1 or 2 Pull Up warning, Terrain Awareness warning, or Obstacle Awareness warning. This feature activates a ‘GPWS’ lamp located in the cockpit within sight of each pilot. 3.15.2.6 GPWS Aler t Discrete (Lamp Format Type 1 definition) GPWS Alert discrete (J1-77) will activate during Mode 5 Glideslope cautions only.
Honeywell MK VI MK VIII EGPWS Installation Design Guide TCAS/TAS Connector Vendor Model Honeywell CAS-81, TCAS II, TPA-81A Collins TTR-920, TCAS II CAS 66, 67 Function TA Only Inhibit Audio TA Only Inhibit Audio Standby Inhibit Audio PIN # RBP-5C RBP-5D RBP-5C RBP-5D P1A-17 P1A-18 Inhibit Audio P1-34 P1-32 P1-9 Goodrich* Skywatch HP (SKY899) Skywatch (SKY497) TCAS I (TCAS791/A) * Interface with the Goodrich Skywatch TAS requires a +28V pullup resistor in the aircraft wiring as shown in Figure 3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.15.2.12 Terrain Pop up Discrete Terrain Pop Up discrete (J1-51) will activate when a Terrain/Obstacle Caution or Warning alert event has occurred. This feature activates the pop up in an integrated display or will switch a relay to pop up Terrain display over selected weather radar display.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.15.3 Instruction s Using Appendix E Tables 5.2, 5.3.13 and 5.3.13-x as described above, select the Input/Output Discrete Type number that matches the aircraft configuration, feature preferences and version (part number) being installed. Record the ID number for the Input/Output Discrete Select number from Appendix E Table 5.3.13 under the Ident No. heading for Step (Category) 13 in Appendix E Table 5.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide H L J1-70 J1-71 High level audio H L J1-75 J1-74 Low level audio 8 ohm 600 ohm Audio Panel FIGURE 3.16-1 Audio Interface 3.17 Category 1 5 - 17 – Undefined Input Selects Category 15-17 are undefined input selects at this time. Appendix E Table 5.3.15, 5.3.16, and 5.3.17 define the Select options and identifies the first MK VI/VIII EGPWS version in which the option was available (see the Effectivity entry). 3.17.
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION IV CONFIGURATION MODULE PROGRAMMING AND TERRAIN DATABASE LOADING Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 115
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION IV – CONFIGURATION MODULE PROGRAMMING AND REGIONAL TERRAIN DATABASE LOADING SECTION IV – CONFIG MODULE PROGRAMMING AND REGIONAL TDB LOADING ................................. 117 4.1 INTRODUCTION............................................................................................................................................................ 117 4.2 HARNESS CHECKOUT AND POWER CHECK .......................................................
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION IV – Config Module Programming And Regional TDB Loading 4.1 Introduction The following procedures outline the steps necessary to accomplish a complete configuration of the MK VI/MK VIII EGPWS. This section must be accomplished in the order presented to minimize errors in configuring and operating the system(s).
Honeywell MK VI MK VIII EGPWS Installation Design Guide 4.4.2 EGPWC Fro nt Panel Test Connector The RS-232 interface with the EGPWC is accomplished via a test connector provided on the EGPWC front panel (J3). This provides access for a PC test monitor and portable data loading capabilities. The mating connector for the EGPWC test plug (P3) is a male, 15 pin, double density D-subminiature type (or equivalent).
Honeywell MK VI MK VIII EGPWS Installation Design Guide 4.4.3 WinVIEWS (Windows Virtual Interface to the Enhanced Warning System) WinVIEWS is a software tool developed by Honeywell to communicate with the EGPWS. WinVIEWS provides a detailed status of the software configuration and input signals, which enables quick identification of system configuration, and is utilized for programming the system Configuration Module.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 4. Using the Category ID’s as chosen from the Appendix E (refer to completed Table 5.2), create a command string with the following structure: CFG> CUW 0/15 # # # # # # # # # # # # # # #/ - CUW0 is the command and version number.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 4.5.1 CUW and C MR Commands An example CUW command/data string, its definition, and the corresponding CMR list is provided below.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 4.5.2 Configurati on Module Reprogramming Reprogramming the EGPWS Configuration Module is accomplished similar to the programming process above. Prior to reprogramming, the desired new configuration should be determined based on the MK VI/VIII Interface Description Document (Appendix E), document number 060-4314-401. For reprogramming the Configuration Module, the following procedure is used: 1.
Honeywell MK VI MK VIII EGPWS Installation Design Guide The MK VIII EGPWS (965-1210-0XX and 965-1220-0XX) have a Global Terrain Database. 4.6.2 Description This modification consists of loading the PCMCIA card into the EGPWS either In The Aircraft or On The Bench. An optional verification procedure is provided. 4.6.3 Approval This procedure contains no modification information that revises the approved configuration and therefore does not require FAA or other regulatory agency approval. 4.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 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.
Honeywell MK VI MK VIII EGPWS Installation Design Guide (7) When loading is complete the XFER COMP LED on the Smart Card turns ON. (8) Remove the PCMCIA card from the Smart Card slot. (9) After approximately 15 seconds the COMPUTER OK LED comes ON to indicate that the contents of the PCMCIA card were successfully transferred. (10)Remove the Smart Card connector from the EGPWC front panel J3 connector. (11)To perform the verification of the Terrain Database version, go to paragraph 4.6.6 below. 4.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide a) “SYSTEM CONFIGURATION” b) “PART NUMBER 965-11X0-XXX” c) “MOD STATUS XX” d) “SERIAL NUMBER XXXX” e) “APPLICATION SOFTWARE VERSION XXXXX” f) “TERRAIN DATABASE VERSION XXXX” The following example of Terrain Database Version annunciation: “419A” (for ATLANTIC), “419P” (for PACIFIC), or “419N” (for AMERICAS). Other versions will follow the same pattern (e.g. “421P”). (7) Other messages that follow the Terrain Database Version can be ignored.
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION V CERTIFICATION Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 127
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION V – CERTIFICATION 5.1 Introductio n This section outlines the procedures required to obtain FAA approval for the MK VI/MK VIII EGPWS installation. Recommended flight test procedures are also included. 5.2 Certificatio n Procedure 5.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide first of type installations, for these installations all sections of the Flight Test procedure shall be performed. Precedence has been established for testing only the Terrain Awareness functions when replacing an existing MK VI GPWS. Installers should contact their local FAA office for confirmation of this approach. For follow on installations of the same aircraft type and interface, the flight test is not required.
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION VI MK VI GPWS (classic) to EGPWS MK VI/VIII Pin to Pin Comparison Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 130
Honeywell MK VI MK VIII EGPWS Installation Design Guide SECTION VI - MK VI GPWS to MK VI/VIII EGPWS Signal Mapping Connector Pin-Out Sorted By Pin Number (USE FOR REFERENCE ONLY) shaded area indicates function change Signal Name –MK-VI GPWS (965-0686-001, -020) Roll Attitude Synchro (X) X=Indicates same function Signal Type Same Conn/Pin Synchro X Signal Type < IN Out > Signal Name -MK-VI/MK VIII EGPWS (Enhanced) J1-01 < AC Analog3W1 Roll Attitude Synchro (X) GND J1-02 < AC Analog3W3 Roll Att
Honeywell MK VI MK VIII EGPWS Installation Design Guide Signal Name –MK-VI GPWS (965-0686-001, -020) Signal Type Same Conn/Pin Signal Type < IN Out > Signal Name -MK-VI/MK VIII EGPWS (Enhanced) Audio Volume Control #1 Program Pin Progpin J1-26 < Analog (+) Spare 500’ Altitude Callout Program Pin Progpin J1-27 < Analog (-) Spare Spare Discrete (+28VDC) Discrete J1-28 < 28vDisc Magnetic Heading Validity Discrete (+28VDC) Radio Altimeter Validity (+28VDC) 28vDisc X J1-29 < 28vDisc DC
Honeywell MK VI MK VIII EGPWS Installation Design Guide Signal Name –MK-VI GPWS (965-0686-001, -020) Signal Type Same Conn/Pin Signal Type < IN Out > Signal Name -MK-VI/MK VIII EGPWS (Enhanced) Test Point #9 Test point J1-55 Monitor Out > (gnd) Test Point #10 Test point J1-56 453 Out (A) > Terrain Display Output Data #2 (A leg) Test Point #11 Test point J1-57 453 Out (B) > Terrain Display Output Data #2 (B leg) Test Point #12 Test point J1-58 453 Out (A) > Terrain Display Output Dat
Honeywell MK VI MK VIII EGPWS Installation Design Guide Signal Name –MK-VI GPWS (965-0686-001, -020) Signal Type Same Conn/Pin Signal Type < IN Out > Signal Name -MK-VI/MK VIII EGPWS (Enhanced) NEW CONNECTOR J2-01 < AC Analog3W1 Configurable Synchro #1 (X leg) J2-02 < AC Analog3W2 Configurable Synchro #1 (Y leg) J2-03 < AC Analog3W3 J2-04 < 429 IN (B) J2-05 < 429 IN (B) Configurable Synchro #2 (Z leg) Radio Altitude ARINC 429 Input (B leg) IOC #2 (Nav) ARINC 429 Input (B leg) ILS ARINC 42
Honeywell MK VI MK VIII EGPWS Installation Design Guide Signal Name –MK-VI GPWS (965-0686-001, -020) Signal Type Same Conn/Pin Signal Type < IN Out > Signal Name -MK-VI/MK VIII EGPWS (Enhanced) Spare RS-232 Input (Tx) Spare RS-422 Input (A leg) GPS/Spare RS-232 Common J2-27 < 232 IN (A) J2-28 < GND J2-29 < 232 IN (A) GPS RS-232 Input (Rcv) Spare RS-422 Input (A leg) J2-31 < GDisc Steep Approach #2 (GND) J2-32 Clock > Configuration Module Serial Clock J2-33 Data > Configuration Module S
Honeywell MK VI MK VIII EGPWS Installation Design Guide Signal Name –MK-VI GPWS (965-0686-001, -020) Signal Type Same Conn/Pin Signal Type < IN Out > Signal Name -MK-VI/MK VIII EGPWS (Enhanced) NEW CONNECTOR J3-01 PWR (L) > SmartCable Power Return (GND) J3-02 < Gdisc PCMCIA Card Present J3-03 < Data EGPWS Monitor Port RS-232 (RCV) J3-04 Data > EGPWS Monitor Port RS-232 (XMT) J3-05 J3-06 PWR (H) > SmartCable Power (+5VDC) J3-07 < Clock SmartCable Serial Clock J3-08 < Data SmartCabl
Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX A - Customer Worksheet Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 137
Honeywell MK VI MK VIII EGPWS Installation Design Guide Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 138
MK VI / MK VIII EGPWS ENHANCED GROUND PROXIMITY WARNING SYSTEM CUSTOMER INTERFACE WORK SHEET DATE: The purpose for this work sheet is to obtain the necessary aircraft data for determining the specific interface configuration for the MK VI or MK VIII Enhanced Ground Proximity Warning System (EGPWS). For defined MK VI and MK VIII EGPWS interface data, refer to Appendix E, Interface Description Document (IDD) for the Mark VI and VIII Enhanced Ground Proximity Warning System (MKVI/VIII EGPWS).
Honeywell MK VI MK VIII EGPWS Installation Design Guide AIRCRAFT SYSTEMS INFORMATION: (Use “N/A” if Not Applicable) Please provide the manufacturer, model number, part number, software part number, quantity per aircraft, and output data information for: OUTPUT DATA FORMAT – NOTES SYSTEM MFGR. MODEL NO. PART NO. S/W PART NO. QTY (ARINC 429, 547, 552, 575, DC, synchro, potentiometer, discrete, etc.
Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX B - Sample Wiring Diagrams Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 141
GLIDESLOPE AND/OR LOCALIZER RADIO ALTITUDE DISPLAY CONFIGURATION AUDIO Honeywell MK VI MK VIII EGPWS Installation Design Guide Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 142
ATTITUDE/MAGNETIC HEADING POSITION AIR DATA INPUT/OUTPUT DISCRETE FUNCTIONS Honeywell MK VI MK VIII EGPWS Installation Design Guide Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 143
AUTOPILOT ENGAGED FLAP SWITCH GEAR SWITCH CONFIG MODULE CONFIGURATION MODULE PROGRAMING Honeywell MK VI MK VIII EGPWS Installation Design Guide Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 144
Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX C WinVIEWS OPERATION INSTRUCTIONS Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 145
Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX C – WinVIEWS Operation Instructions RS-232 COMMUNICATION WITH THE EGPWS The EGPWS contains software that allows monitoring of its internal parameters, for testing purposes, without altering its operation. The monitoring of these parameter values enables the operator to quickly determine if the correct signal and scaling is being used by the EGPWS computer.
Honeywell MK VI MK VIII EGPWS Installation Design Guide WinVIEWS OPERATION: Windows Virtual Interface to the Enhanced Warning System WinVIEWS software is a tool developed by Honeywell to monitor or view values within the EGPWS. The WinVIEWS software provides a monitor function that does not alter the operation of the EGPWS. The monitoring of values assists in the installation testing of the EGPWS by allowing the operator to quickly determine if the correct signal and scaling is being used by the EGPWS.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Command File: MK68_GTP.CMD The format for the WinVIEWS command file is: 1. ASCII Text Only; no spaces 2. A CVT Item as specified in the test procedure 3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX D VENDOR CONTACT INFORMATION CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 149
Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX D - Vendor Contact Information Vendor Contact Information The vendor contact information provided below is current at the time of publication of this document. AMP 2800 Fulling Mill Road MS 038-035 Middletown, PA 17507 800 806-0480 http://www.amp.com Amphenol 20 Melford Drive Scarborough, Ontario, Canada M1B 2X6 Ph: 416-291-4401 Fax: 416-292-0647 http://www.amphenol.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Electronic Cable Specialists and Electrical Conservation Systems, Inc. 5300 W Franklin Drive Franklin, WI 53132-8642 414 421-5300 http://www.ecsdirect.com Electrical & Mechanical Technologies (EMTEQ) S84 W18693 Enterprise Drive Muskego, WI 53150 PH: 262 679-6170 Fax: 262 679-6175 888 679-6170 Email: Sales@emteq.com http://www.emteq.com Hollingsead International Sante Fe Springs, CA 213 921-3436 http://www.hollingsead.
Honeywell MK VI MK VIII EGPWS Installation Design Guide West Coast Specialties CAGE CODE: 97896 P.O.
Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX E Interface Description Document Proprietary notice on title page applies CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-150 REV: SHEET 153
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table of Contents APPENDIX E - INTERFACE DESCRIPTION DOCUMENT 159 1 INTRODUCTION 1.1 PART NUMBER 1.2 PURPOSE 1.3 SYSTEM OVERVIEW 1.4 DOCUMENT OVERVIEW 159 159 159 159 159 2 REFERENCES 159 3 MECHANICAL INTERFACE 3.1 WEIGHT 3.2 SYSTEM INTERFACE COMPONENTS 3.2.1 EGPWC Mounting 3.2.2 EGPWC Connectors 3.2.3 Configuration Module 3.3 OUTLINE 160 160 160 160 160 161 162 4 ELECTRICAL INTERFACE 4.1 INTRODUCTION 4.2 SIGNAL INTERFACES 4.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 4.3 FRONT PANEL TEST INTERFACE 4.3.1 RS-232 Maintenance Port (serial port 4) 4.3.2 PCMCIA / SmartCable Port 4.3.3 GSE Present Discrete Input 4.4 FRONT PANEL STATUS INDICATORS 172 173 173 173 173 5 AIRCRAFT APPLICATION DATA 5.1 CONFIGURATION TYPES 5.2 CONFIGURATION SELECTION 5.3 CONFIGURATION SELECTION TABLES 5.3.1 Category 1, Aircraft / Mode Type Select 5.3.2 Category 2, Air Data Input Select 5.3.3 Category 3, Position Input Select 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.2.10 6.2.11 6.2.12 6.2.13 6.2.14 6.2.15 6.2.16 6.2.17 6.2.18 6.2.19 6.2.20 6.2.20.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.3.3 Barometric Altitude Rate (212) 6.3.4 Computed Airspeed (206) 6.4 DIGITAL DATA, RS-232 6.4.1 Xpress GPS Packets ID 15: Lat/Lon/Estimated Horizontal Position Error 6.4.2 Xpress GPS Packets ID 16: Altitude/Estimated Vertical Position Error 6.4.3 Xpress GPS Packets ID 17: Ground Speed/Track Angle 6.4.4 Xpress GPS Packets ID 18: East/North/Up Velocity 6.4.5 Xpress GPS Packets ID 1C: GPS State 6.5 DIGITAL DATA, RS-422 6.5.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.1.2.7 7.1.2.8 7.1.2.9 7.1.2.10 7.1.2.11 7.1.2.12 7.1.2.13 7.1.2.14 7.1.2.15 7.1.3 7.1.3.1 7.1.3.2 7.1.3.3 7.1.3.4 7.1.3.5 7.1.3.6 7.1.4 7.1.4.1 7.1.5 7.1.5.1 7.1.5.2 7.1.5.3 7.1.6 7.1.6.1 7.1.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX E - Interface Description Document 1 INTRODUCTION 1.1 Part Number This document is the Interface Description Document for the MK VI and MK VIII Enhanced Ground Proximity Warning System (EGPWS).
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3 MECHANICAL INTERFACE 3.1 Weight The maximum weight for all MK VI and MK VIII EGPWC part numbers is 3.9 pounds. 3.2 System Interface Components Refer to section 3.3 for outline drawings. 3.2.1 EGPWC Mounting The mounting rack for the EGPWC is identified as follows: TRAY Honeywell P/N Source/Vendor 405-0383-001 Bendix/King Vendor Part Number 071-04003-0002 3.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.2.3 Configuration Module The EGPWS aircraft configuration is programmed into a configuration module installed in the aircraft wiring. This configuration module is identified as follows: Vendor/Supplier Supplier P/N Honeywell 700-1710-001 Honeywell 700-1710-020 * The configuration module is installed as part of the P2 mating connector backshell and contains reprogrammable memory for configuration storage.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.3 Outline Dimensions of the MK VI and MK VIII EGPWC hardware and their associated mounting rack are given in this section. The mounting rack is identical to that of the MK VI GPWC. FIGURE 3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide FIGURE 3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 4 ELECTRICAL INTERFACE 4.1 Introduction The MK VI and MK VIII EGPWS provide electrical interfaces for aircraft systems and to support maintenance functions. The interfaces are made via the front panel aircraft interface connectors, front panel maintenance/test port and front panel LED’s. A TNC coaxial connector is located on the front panel for internal GPS receivers in the 965-1190-0XX MK VI EGPWC, and 965-1220-0XX MK VIII EGPWC only.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 4.2.3 DC Analog Inputs Unless otherwise specified, Input Signal accuracy is 1% linearity +0.1% full scale offset. 4.2.3.1 Radio Altitude Quantity Input Impedance, each leg Maximum Reverse Fault Current Signal Range Input Voltage Range (VRA) Conversion Range (VC) Input Filter Broken Wire Detect Pin Assignment (Signal Mnemonic): Signal (+) Return (-) 1 > 83 KΩ < 200 µA 0 to 2500 feet 37.7V ≥ VRA ≥ -2.5V 29.7V ≥ VC ≥ -0.4V 0.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 4.2.3.4 Barometric Altitude Quantity Input Impedance, each leg Reverse Fault Current Input Voltage Range Input Filter Input Type Broken Wire Detect Pin Assignment (Signal Mnemonic): Signal (+) Return (-) 1 > 83 KΩ < 200 µA -0.18 VDC to +15 VDC 0.1 Second Low Pass, ± 10% Differential Input will be biased less than -3000 feet J1-62 J1-43 (ALT_H) (ALT_L) 4.2.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 4.2.4.2 Synchro Magnetic Heading Quantity Synchro Angle Range Reference Voltages Pin Assignment (Signal Mnemonic): X leg Y leg Z leg 1 ±180 deg ±26 VACRMS ± 20% (see 4.2.4.4) J1-22 J1-23 J1-3 (SYN_2X) (SYN_2Y) (SYN_2Z) 4.2.4.3 Synchro Pitch Attitude Quantity Synchro Angle Range Reference Voltages Pin Assignment (Signal Mnemonic): X leg Y leg Z leg 1 ±80 deg Not Required J1-5 J1-7 J1-6 (SYN_3X) (SYN_3Y) (SYN_3Z) 4.2.4.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 4.2.5 ARINC 429/575 Digital Serial Bus Inputs Quantity Format Low Speed Data Rate High Speed Data Rate Direction of Information Flow Word/Frame Structure Data definition Channel Receive #1 A leg Receive #1 B leg 8 DITS, ARINC 429/575 Low or high speed 1 12.0 KBPS to 14.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 4.2.6.1 GPS RS-232 Digital Serial Bus (serial port 3) One port is provided for use with external or internal RS-232 GPS interfaces. This port is common with the GPS RS-422 port described in Section 4.2.6.2 and can only function as a RS-232 interface or a RS-422 interface but not both.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 4.2.7 Discrete Inputs Discrete signals are intended for remote switching through the aircraft, and are therefore subject to being connected to other signals, and are also subject to transient voltage conditions. For these reasons, the following rules apply to each input, unless otherwise stated. Each input is capable of withstanding voltage transients of ± 600VDC for 10 µs and ± 50VDC continuously, without damage.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Connector Type Low Level DC on RF Output Pin Assignment (Signal Mnemonic): TNC +5 VDC ±5%, 50 mAmps maximum, Shield Ground. GPS ANT (COAX) 4.2.10 OAT Voltage Reference Output This output is an accurate voltage source for 500 Ω resistive temperature sensors. Quantity 1 Output Voltage 5.000 VDC ±10 mVDC (no load) Nominal Load 500 Ω Pin Assignment (Signal Mnemonic): J1-25 (OAT_REF) NOTE: This output has a source impedance of 4.42 KΩ, 0.1%. 4.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Quantity Maximum Power Output Nominal Output Impedance Load Impedance Number of Available Power Output Levels Pin Assignment (Signal Mnemonic): Signal (+) Return (-) 1 4 Watts Nominal 8Ω 8Ω or greater 5 selectable levels excluding the Mode 6 Audio Reduction function J1-70 J1-71 (AUD_HL_H) (AUD_HL_L) 4.2.12.2 Low Level (Interphone) Audio Output The 600-ohm output is capable of driving one 600-ohm load at the specified level (or at a reduced level).
Honeywell MK VI MK VIII EGPWS Installation Design Guide 4.3.1 RS-232 Maintenance Port (serial port 4) One port is provided which meets the characteristics specified in RS232C. This bus can be used to read internal data from the MK VI or MK VIII EGPWS for both bench, and aircraft testing or transmitting configuration data for selected EGPWS interfaces and options.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5 AIRCRAFT APPLICATION DATA This section describes the MK VI and MK VIII EGPWS interfaces for aircraft applications. Section 5.1 is a listing of the selection categories defining the various aircraft sensor interfaces and EGPWS functional options. Section 5.2 describes how the Category ID’s are selected and programmed for the interface to aircraft sensors and EGPWS functional options. Section 5.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.2: Category ID Selection Procedure Step (Category) Signal Selection Selects: 1 2 3 a) Aircraft Type b) Mode Type Selects: a) Air Data Source Selects: a) Position Source Selects: 4 a) Altitude Callouts Menu Selects: 5 a) Audio Menu Selects: 6 a) Terrain Display Config. Instruction Ident No. Using Table 5.3.1, and any sub-tables contained within, locate the Aircraft / Mode Type. Record the Ident (ID No.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Step (Category) Signal Selection Instruction Ident No. Selects: 13 14 15 16 17 a) Input Discrete Functions b) Output Discrete Functions Selects: a) Audio Output Level Using Table 5.3.13, and any sub-tables contained within, locate the desired I / O Discrete type. Record the Ident (ID No.) on the space available on Ident column of this table. _______ Using Table 5.3.14, and any sub-tables contained within, locate the desired Volume type.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5.3 Configuration Selection Tables Configuration selection is defined by category (or group of functions or inputs). The Category number identifies the subsection where the details are defined. For example Air Data, Category 2, is defined in Section 5.3.2, and Position Input Source, Category 3, is defined in Section 5.3.3. 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide The following table provides identification of the basic Aircraft/Mode Types and associated parameters. For purposes of selecting an ID, use the “Description” provided in Table 5.3.1 appropriate to the desired variables as given above. Table 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5.3.2 Category 2, Air Data Input Select The following table provides identification of the Air Data source type. The entry in the Air Data Type corresponds to a table that provides detailed information on the configuration. For example, the details for Air Data Type #2 are found in Table 5.3.2-2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 5.3.2-0: AIR DATA INPUT SELECT #0 (+) = J1-62 (–) = J1-43 Outside Air Temp Total Air Temperature REFERENCE 6.1.3 6.1.4 4.2.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 5.3.2-2: AIR DATA INPUT SELECT #2 CHANNEL 429RX_2 A = J2-39 B = J2-38 CONNECT TO: ADC #1 Format: ARINC 575 (Low Speed) Fault Designation: AIR DATA BUS Bus Type: Basic Data Uncorrected Baro. Alt Computed Airspeed Barometric Rate Static Air Temperature Label 203 206 212 213 Reference 6.3.2 6.3.4 6.3.3 6.3.1 Sig. Bits 17 13 11 10 Range ±131,072 FT ±1024 KTS ±20480 FPM ±512 Degrees Signal Type Basic Basic Basic Basic Resolution 1.0 0.
Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 5.3.2-4: AIR DATA INPUT SELECT #4 (+) = J1-62 (–) = J1-43 Outside Air Temp Total Air Temperature REFERENCE 6.1.13 6.1.4 4.2.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 5.3.2-6: AIR DATA INPUT SELECT #6 CHANNEL 429RX_2 CONNECT TO: ADC #1 Format: ARINC 429 (Low Speed) Fault Designation: AIR DATA BUS Bus Type: Basic A = J2-39 B = J2-38 Data Uncorrected Baro. Alt Computed Airspeed Static Air Temperature Label 203 206 213 Reference 6.2.1 6.2.39 6.2.2 Configuration Data Derive Baro Altitude Rate Sig. Bits 17 14 11 Range ±131,072 FT ±1024 KTS ±512 Degrees Type Signal Type Basic Basic Basic Resolution 1.
Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 5.3.2-11: AIR DATA INPUT SELECT #11 (+) = J1-62 (–) = J1-43 Outside Air Temp Total Air Temperature REFERENCE 6.1.16 6.1.4 4.2.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 5.3.2-12: AIR DATA INPUT SELECT #12 SIGNAL CONNECTION REFERENCE SUMMARY DATA Uncorrected Barometric Altitude (+) = J1-62 (–) = J1-43 6.1.
Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 5.3.2-255: AIR DATA INPUT SELECT #255 CHANNEL 429/422RX_1 A = J2-37 B = J2-36 CHANNEL 429RX_3 A = J2-41 B = J2-40 CONNECT TO: IOC #1 Format: ARINC 429 (High Speed) Fault Designation: IOC BUS 1 Bus Type: Basic Data Uncorrected Baro. Alt Corrected Baro. Alt Computed Airspeed True Airspeed Barometric Rate Static Air Temperature Label 203 204 206 210 212 213 Reference 6.2.1 6.2.38 6.2.39 6.2.40 6.2.3 6.2.2 Sig.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5.3.3 Category 3, Position Input Select The following table provides identification of the Position source signal. Each entry in the Position Input Type column has a corresponding table that provides detailed information on the configuration. For example, the details for Position Input Type #0 are found in Table 5.3.3-0.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.3-0: Position Input Type 0 (Low Speed ARINC 743A GPS) CHANNEL 429RX_4 A = J2-25 B = J2-8 CONNECT TO: GPS (ARINC 743A) Format: ARINC 429 (Low Speed) Data Latitude - Normal Longitude - Normal GPS Hor. Int. Limit Altitude VFOM HFOM Ground Speed True Track Angle North/South Velocity East/West Velocity Vertical Velocity Sensor Status **UTC **Date Reference 6.2.7 6.2.8 6.2.5 6.2.4 6.2.13 6.2.10 6.2.6 6.2.9 6.2.53 6.2.54 6.2.58 6.2.16 6.2.17 6.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.3-3: Position Input Type 3 (RS232 GPS, PXpress format) CHANNEL GPS_RXA GPS_TXA J2-28 (cm) J2-29 (Rx) CONNECT TO: GPS (PXpress format) Format: RS232 (9600 baud) Data Latitude Longitude HP Error Altitude VP Error Ground Speed True Track Angle East Velocity North Velocity Vertical Velocity GPS State Integrity State Error Status Reference 6.4.1 6.4.1 6.4.1 6.4.2 6.4.2 6.4.3 6.4.3 6.4.4 6.4.4 6.4.4 6.4.5 6.4.5 6.4.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.3-10: Position Input Type 10 (Low Speed ARINC 743A GPS, no N/S-E/W Velocities) CHANNEL 429RX_4 A = J2-25 B = J2-8 CONNECT TO: GPS (ARINC 743A) Format: ARINC 429 (Low Speed) Data Latitude – Normal Longitude – Normal GPS Hor. Int. Limit Altitude VFOM HFOM Ground Speed True Track Angle Sensor Status **UTC **Date Reference 6.2.7 6.2.8 6.2.5 6.2.4 6.2.13 6.2.10 6.2.6 6.2.9 6.2.16 6.2.17 6.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.3-13: Position Input Type 13 (High Speed ARINC 743 GPS, no N/S-E/W Velocities) CHANNEL 429RX_4 A = J2-25 B = J2-8 Fault Designation: GPS BUS Bus Type: Basic CONNECT TO: GPS (ARINC 743) Format: ARINC 429 (High Speed) Data Latitude – Normal Longitude – Normal GPS Hor. Int. Limit Altitude VFOM HFOM Ground Speed True Track Angle Sensor Status **UTC **Date Reference 6.2.7 6.2.8 6.2.5 6.2.4 6.2.14 6.2.11 6.2.6 6.2.9 6.2.16 6.2.17 6.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.3-255: Position Input Type 255 (Dual High Speed ARINC 743A GPS) CHANNEL 429RX_4 A = J2-25 B = J2-8 CHANNEL 429RX_7 CONNECT TO: GPS #1 (ARINC 743A) Format: ARINC 429 (High Speed) Fault Designation: GPS BUS 1 Bus Type: Basic Data Reference Latitude - Normal 6.2.7 Longitude - Normal 6.2.8 GPS Hor. Int. Limit 6.2.5 Altitude 6.2.4 VFOM 6.2.13 HFOM 6.2.10 Ground Speed 6.2.6 True Track Angle 6.2.9 Sensor Status 6.2.16 **UTC 6.2.17 **Date 6.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5.3.4 Category 4, Altitude Callouts The following table provides identification of the Altitude Callouts Menu. Each entry in the ID column corresponds to a particular menu selection. The Altitude Callouts menu ID’s 0 through 12 consist of standard callouts. Selecting ID 0 – 12 will result in the callouts listed being enunciated.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5.3.5 Category 5, Audio Menu Select The Audio Menu Select option consists of sets of voices that are mapped to specific warning mode outputs. The Audio Menu tables list the alert/warning conditions in order of priority. The following table provides identification of the Audio Menu Type. Each entry in the Audio Menu Type column has a corresponding table that provides detailed information on the configuration.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5.3.6 Category 6, Terrain Display Select The following table (5.3.6) has an identification number (ID) associated with each Terrain Display configuration. Each of the ID rows has a group number for the Display Configuration, the Input Control. The TA&D Pop Up Disable function is defined by a Boolean. The ID groups will completely identify a particular Terrain Display Interface. Table 5.3.6: Terrain Display Select ID Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide ID Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.1-1 No Display, TAD and TCF enabled No Table Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide • • • • • • If all the conditions indicated for the amber “TERR” above are FALSE. If the display is in normal MFD mode (not HSI backup, or SG backup) AND if label051 bit 11 transitions from 0 to 1 (rising edge), AND Checklist is not selected on the MFD, AND TCAS Auto Pop Up is not occurring. The display will change to Map mode. The display will energize the Terrain selection relays. The display will annunciate “TERR”.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.1-246 Honeywell/Bendix EFIS 10, EFS 86 Radar system MK VIII Only Display Configuration Group 246 Function Display Type Sweep Type Auto Pop Up Value Bendix EFIS 10 (Non-Integrated) Normal, Sweep range +/- 90 degrees Category 7, Options Select Group #1 TA&D Alternate Pop Up: False TA&D Alternate Pop Up: True Pop Up on Caution or Warning.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 8. If bits 15-18 right range output from the EGPWS does not match right MFD range (via label 171), then display white “RANGE MISMATCH” on the right PFD and MFD. Label 051 If bit 17 = 1 then display white “TERRAIN OFF” message on PFD and MFD. Labels 052-055 EGPWS ASCII characters are not used. Green “TERRAIN” on PFD and MFD by EFIS. Label 274 If bit 13 or 22 = 1 then display red “PULL UP” on left and right PFD.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Label 051 Labels 052-055 Label 274 If bits 15-18 right range output from EGPWS does not match right MFD range (via label 171), then display white “RANGE MISMATCH” on right PFD and MFD. If Bit 17 = 1 then display white “TERRAIN OFF” message on PFD and MFD and Terrain window will be cleared by EPIC. EGPWS ASCII characters are not used. Green TERRAIN on PFD and MFD by EFIS. If Bit 13 or 22 =1 then display red “PULL UP” on left and right PFD.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide The display will be blanked when the amber “TERR” is present. The display will Pop Up to Terrain mode as follows: • If all the conditions indicated for the amber “TERR” above are FALSE. • If the display is in normal MFD mode (not HSI backup, or SG backup) AND if label 051 bit 11 transitions from 0 to 1 (rising edge), AND Checklist is not selected on the MFD, AND TCAS Auto Pop Up is not occurring. • The display will change to Map mode.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.6.1-255 Honeywell SPZ8000 older style MK VIII Only Display Configuration Group 255 Function Display Type Sweep Type Auto Pop Up Peaks Mode (Elevations via overlay) Manual select Manual deselect Auto Range Moving Marker Overlay Page Display bus type DISPLAY BUS #1 453TX_1 A = J1-58 B = J1-59 DISPLAY BUS #2 453TX_2 A = J1-56 B = J1-57 Value Honeywell (5x6) SPZ8000 older style; does not blank every fourth weather radar display line.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5.3.7 Category 7, Options Select Group #1 The following table provides identification of the Options Select Group #1. Each entry in the ID column corresponds to a particular combination of TA&D Alternate Pop Up, Obstacle Awareness Enabled, Peaks Mode Enabled, Bank Angle Enable, Steep Approach Enabled, Flap Reversal and GPS Altitude Reference selection. Refer to section 7.5 for configuration messages that will be present for each option selected.
Honeywell MK VI MK VIII EGPWS Installation Design Guide ID 36 37 38 39 40 41 42 43 44 45 46 47 48 49 50 51 52 53 54 55 56 57 58 59 60 61 62 63 64 65 66 67 68 69 70 71 72 73 74 75 76 77 78 79 80 81 82 83 84 85 Steep Approach Enabled 1 False False False False False False False False False False False False False False False False False False False False False False False False False False False False True True True True True True True True True True True True True True True True True True True True True True
Honeywell MK VI MK VIII EGPWS Installation Design Guide ID 86 87 88 89 90 91 92 93 94 95 96 97 98 99 100 101 102 103 104 105 106 107 108 109 110 111 112 113 114 115 116 117 118 119 120 121 122 123 124 125 126 127 Steep Approach Enabled 1 True True True True True True True True True True True True True True True True True True True True True True True True True True True True True True True True True True True True True True True True True True TA&D Alternate Pop Up False False False False False False Fals
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5.3.8 Category 8, Radio Altitude Input Select The following table provides identification of the Radio Altitude type. The entry in the Radio Altitude Type corresponds to a table that provides detailed information on the configuration. For example, the details for Radio Altitude Type #1 are found in Table 5.3.8-1. ARINC 552, ALT 55 and digital ARINC 429 compatible Radio Altimeters are supported.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.8-1: Radio Altitude Input Select Type 1 (ALT 55) SIGNAL Radio Altimeter #1 PIN FUNCTION CONNECTION REFERENCE (+) = J1-64 (-) = J1-45 6.1.2 4.2.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.8-251: Radio Altitude Input Select Type 251 (ARINC 429 via dual IOC buses with DH/MDA) Fault Designation: IOC BUS 1 Bus Type: Basic CHANNEL 429RX_1 CONNECT TO: IOC #1 Format: ARINC 429 (High Speed) A = J2-37 B = J2-36 CHANNEL 429RX_3 Data Reference Radio Altitude 6.2.29 Decision Height/MDA 6.2.62 CONNECT TO: IOC #2 Format: ARINC 429 (High Speed) Data Radio Altitude Decision Height/MDA A = J2-41 B = J2-40 Reference 6.2.29 6.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.8-254: Radio Altitude Input Select Type 254 (ARINC 429 via dual IOC buses) CHANNEL 429RX_1 A = J2-37 B = J2-36 CHANNEL 429RX_3 A = J2-41 B = J2-40 Fault Designation: IOC BUS 1 Bus Type: Basic CONNECT TO: IOC #1 Format: ARINC 429 (High Speed) Data Reference Radio Altitude 6.2.29 Decision Height (format 3) 6.2.41 MDA (format 3) 6.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5.3.9 Category 9, Navigation Input Select The following table provides identification of the Navigation type. The entry in the Navigation Type corresponds to a table that provides detailed information on the configuration. For example, the details for Navigation Type #1 are found in Table 5.3.9-1. In this category, only the following signals are defined: • • • • Glideslope source selection. Localizer source selection.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.9-0: Navigation Inputs Select 0 SIGNAL CONNECTION (+) = J1-65 (-) = J1-46 Glideslope Deviation PIN FUNCTION Glideslope Validity Discrete #1 +28V ILS Tuned Discrete #1 GND ILS Tuned Discrete #1 REFERENCE 6.1.6 4.2.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.9-5: Navigation Inputs Select 5 SIGNAL CONNECTION REFERENCE Glideslope Deviation (+) = J1-65 (-) = J1-46 6.1.6 4.2.3.2 Localizer Deviation (+) = J1-30 (-) = J1-10 6.1.17 4.2.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.9-252: Navigation Inputs Select 252 CHANNEL 429/422RX_1 A = J2-39 B = J2-38 CHANNEL 429RX_3 A = J2-21 B = J2-04 CONNECT TO: IOC #1 Format: ARINC 429 (High Speed) Fault Designation: IOC BUS 1 Bus Type: Basic Data Reference Glideslope 6.2.30 Localizer 6.2.33 CONNECT TO: IOC #2 Format: ARINC 429 (High Speed) Label 174 173 Data Glideslope Localizer Reference 6.2.30 6.2.33 Sig. Bits 12 12 Range ±0.8 DDM ±0.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5.3.10 Category 10, Attitude Input Select The following table provides identification of the Attitude Roll Angle type. The entry in the Attitude Input Select corresponds to a table that provides detailed information on the configuration. For example, the details for Attitude Input Select #2 are found in 5.3.10-2. In this category, only the following signals are defined: • • • • • • • • Roll Attitude.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.10-2: Attitude Input Select Type 2 SIGNAL CONNECTION REFERENCE Roll Attitude (X) = J1-1 (Y) = J1-21 (Z) = J1-2 6.1.15 Pitch Attitude (X) = J1-5 (Y) = J1-7 (Z) = J1-6 6.1.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.10-253: Attitude Input Select Type 253 CHANNEL 429RX_7 A = J2-37 B = J2-36 Data Roll Angle Pitch Angle Body Roll Rate Body Pitch Rate Inertial Vertical Speed Inertial Altitude CHANNEL 429RX_7 A = J2-41 B = J2-40 Fault Designation: IOC BUS 1 Bus Type: Basic CONNECT TO: IOC #1 Format: ARINC 429 (High Speed) Reference 6.2.31 6.2.34 6.2.50 6.2.49 6.2.56 6.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5.3.11 Category 11, Heading Input Select The following table provides identification of the Heading type. The entry in the Heading Input Select corresponds to a table that provides detailed information on the configuration. For example, the details for Magnetic Heading Input Select #0 are found in Table 5.3.11-0. In this category, only the following signals are defined: • • Magnetic Heading True Heading Table 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.11-3: Heading Input Select Type 3 CHANNEL 429RX_7 A = J2-23 B = J2-6 Fault Designation: AHRS BUS Bus Type: Basic CONNECT TO: AHRS Format: ARINC 429 (High Speed) Data Magnetic Heading True Heading Reference 6.2.32 6.2.37 Label 320 314 Sig. Bits 15 15 Range ±180 degrees ±180 degrees Signal Type Basic Basic Resolution 0.0054931640625 0.0054931640625 Rate (ms) 10-20 25-50 Table 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5.3.12 Category 12, Windshear Input Select The following table provides identification of the Windshear Input Type. The entry in the Windshear Input Type corresponds to a table that provides detailed information on the configuration. For example, the details for Windshear Input Type #255 are found in 5.3.12-255.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5.3.13 Category 13, Input / Output Discrete Type Select The following table provides identification of the Input/Output Discrete Type. Each entry in the Input/Output Discrete Type column has a corresponding table that provides detailed information on the configuration. For example, the details for Input/Output Discrete Type #0 are found in Table 5.3.13-0. Table 5.3.13: Input/Output Discrete Type Select ID Input/Output Discrete Type (Table 5.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.13-0: Input/Output Discrete Type 0 CONN PIN # CHANNEL DESIGNATION REFERENCE PIN TYPE J1-38 28V_DISC_02 Input +28V Glideslope Inhibit Discrete 6.6.12 J1-19 GND_DISC_02 Input GND Glideslope Inhibit Discrete 6.6.11 J1-37 28V_DISC_03 Input +28V Landing Flaps Discrete 6.6.5 J1-18 GND_DISC_03 Input GND Landing Flaps Discrete 6.6.4 J1-36 28V_DISC_04 Input +28V Audio Inhibit Discrete 6.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.13-1: Input/Output Discrete Type 1 CONN PIN # CHANNEL DESIGNATION REFERENCE PIN TYPE J1-38 28V_DISC_02 Input +28V Glideslope Inhibit Discrete 6.6.12 J1-19 GND_DISC_02 Input GND Glideslope Inhibit Discrete 6.6.11 J1-37 28V_DISC_03 Input +28V Landing Flaps Discrete 6.6.5 J1-18 GND_DISC_03 Input GND Landing Flaps Discrete 6.6.4 J1-36 28V_DISC_04 Input +28V Audio Inhibit Discrete 6.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.13-2: Input/Output Discrete Type 2 CONN PIN # CHANNEL DESIGNATION REFERENCE PIN TYPE J1-38 28V_DISC_02 Input +28V Glideslope Inhibit Discrete 6.6.12 J1-19 GND_DISC_02 Input GND Glideslope Inhibit Discrete 6.6.11 J1-37 28V_DISC_03 Input +28V Landing Flaps Discrete 6.6.5 J1-18 GND_DISC_03 Input GND Landing Flaps Discrete 6.6.4 J1-36 28V_DISC_04 Input +28V Audio Inhibit Discrete 6.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.13-3: Input/Output Discrete Type 3 CONN PIN # CHANNEL DESIGNATION REFERENCE PIN TYPE PIN FUNCTION Ref J1-38 28V_DISC_02 Input +28V Glideslope Inhibit Discrete 6.6.12 J1-19 GND_DISC_02 Input GND Glideslope Inhibit Discrete 6.6.11 J1-37 28V_DISC_03 Input +28V Landing Flaps Discrete 6.6.5 J1-18 GND_DISC_03 Input GND Landing Flaps Discrete 6.6.4 J1-36 28V_DISC_04 Input +28V Audio Inhibit Discrete 6.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.13-4: Input/Output Discrete Type 4 CONN PIN # CHANNEL DESIGNATION REFERENCE PIN TYPE J1-38 28V_DISC_02 Input +28V Glideslope Inhibit Discrete 6.6.12 J1-19 GND_DISC_02 Input GND Glideslope Inhibit Discrete 6.6.11 J1-37 28V_DISC_03 Input +28V Landing Flaps Discrete 6.6.5 J1-18 GND_DISC_03 Input GND Landing Flaps Discrete 6.6.4 J1-36 28V_DISC_04 Input +28V Audio Inhibit Discrete 6.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.13-5: Input/Output Discrete Type 5 CONN PIN # CHANNEL DESIGNATION REFERENCE PIN TYPE J1-38 28V_DISC_02 Input +28V Glideslope Inhibit Discrete 6.6.12 J1-19 GND_DISC_02 Input GND Glideslope Inhibit Discrete 6.6.11 J1-37 28V_DISC_03 Input +28V Landing Flaps Discrete 6.6.5 J1-18 GND_DISC_03 Input GND Landing Flaps Discrete 6.6.4 J1-36 28V_DISC_04 Input +28V Audio Inhibit Discrete 6.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.13-6: Input/Output Discrete Type 6 CONN PIN # CHANNEL DESIGNATION REFERENCE PIN TYPE J1-38 28V_DISC_02 Input +28V Glideslope Inhibit Discrete 6.6.12 J1-19 GND_DISC_02 Input GND Glideslope Inhibit Discrete 6.6.11 J1-37 28V_DISC_03 Input +28V Landing Flaps Discrete 6.6.5 J1-18 GND_DISC_03 Input GND Landing Flaps Discrete 6.6.4 J1-36 28V_DISC_04 Input +28V Audio Inhibit Discrete 6.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.13-7: Input/Output Discrete Type 7 CONN PIN # CHANNEL DESIGNATION REFERENCE PIN TYPE J1-38 28V_DISC_02 Input +28V Glideslope Inhibit Discrete 6.6.12 J1-19 GND_DISC_02 Input GND Glideslope Inhibit Discrete 6.6.11 J1-37 28V_DISC_03 Input +28V Landing Flaps Discrete 6.6.5 J1-18 GND_DISC_03 Input GND Landing Flaps Discrete 6.6.4 J1-36 28V_DISC_04 Input +28V Audio Inhibit Discrete 6.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.13-254: Input/Output Discrete Type 254 CONN PIN # CHANNEL DESIGNATION REFERENCE PIN TYPE J1-38 28V_DISC_02 Input J1-19 GND_DISC_02 Input PIN FUNCTION Ref +28V Glideslope Inhibit Discrete 6.6.12 GND Glideslope Inhibit Discrete 6.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Table 5.3.13-255: Input/Output Discrete Type 255 CONN PIN # CHANNEL DESIGNATION REFERENCE PIN TYPE J1-38 28V_DISC_02 Input J1-19 GND_DISC_02 Input PIN FUNCTION Ref +28V Glideslope Inhibit Discrete 6.6.12 GND Glideslope Inhibit Discrete 6.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 5.3.14 Category 14, Audio Output Level The following table provides identification of the Audio Output Level Select. Each entry in the ID column corresponds to a particular nominal alert output level selection (Max, -6 dB, -12 dB, -18dB and –24dB). The nominal “Max” output is 4 W(rms) for the 8-ohm output and 100 mW(rms) for the 600-ohm output.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6 CONFIGURABLE INPUT DATA DEFINITION This section defines the EGPWS input signal characteristics or data word formats for input signals commonly used in MK VI and VIII EGPWS applications. See Section 5 for specific information on signal usage. 6.1 Analog Input Data 6.1.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.1.
Honeywell MK VI MK VIII EGPWS Installation Design Guide External Validity Flag Connection: AIC LSB: AIC Status Mask: External Validity Type: None 0.03125 °C 00000000 None 6.1.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Signal Open Wire Threshold Reference Dynamic Range: Reference Reasonable Range: Scale: Input Signal Connection: Input Reference Connection: AIC Name: External Validity Flag Connection: AIC FIFO LSB: AIC Status Mask: External Validity Type: None None None Roll Angle (deg) = 1 deg/deg (X) = J1-1, (Y) = J1-21, (Z) = J1-2 None S1 (Synchro #1) None 0.00549316° 0000010F None 6.1.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Signal Dynamic Range: Signal Reasonable Range: Signal Open Wire Threshold Reference Dynamic Range: Reference Reasonable Range: Scale: Input Signal Connection: Input Reference Connection: AIC Name: External Validity Flag Connection: AIC LSB: AIC Status Mask: External Validity Type: –100 to +3200 Feet –30 to +2800 Feet –50 Feet None None RALT (ft) = 250 ft/VDC * Voltsin (+) = J1-64, (–) = J1-45 None D1 (DC1) J1-29 0.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.1.14 ARINC 547/578-4 Low Level Glideslope Deviation Validity Data Item Signal Name: AIC Algorithm: Signal Dynamic Range: Signal Reasonable Range: Signal Open Wire Threshold Reference Dynamic Range: Reference Reasonable Range: Scale: Input Signal Connection: Input Reference Connection: AIC Name: External Validity Flag Connection: AIC LSB: AIC Status Mask: External Validity Type: Value Low Level Glideslope Validity, DC Signal DC Absolute –1.1 to +1.
Honeywell MK VI MK VIII EGPWS Installation Design Guide AIC LSB: AIC Status Mask: External Validity Type: 2 Feet 0000200F Discrete Validity, 28V 6.1.
Honeywell MK VI MK VIII EGPWS Installation Design Guide BIT 31 0 0 1 1 BINARY (BNR) DATA DEFINITION Failure Warning No Computed Data (NCD) Functional Test Normal Operation BIT 30 0 1 0 1 BIT 29 DEFINITION Plus, North, East, Right, To, Above Minus, South, West, Left, From, Below 0 1 BINARY CODED DECIMAL (BCD) DATA BIT 30 DEFINITION 0 Plus, North, East, Right, To, Above 1 No Computed Data (NCD) 0 Functional Test 1 Minus, South, West, Left, From, Below BIT 31 0 0 1 1 Unless identified as using the Hon
Honeywell MK VI MK VIII EGPWS Installation Design Guide B4 1 1 B3 0 1 B2 1 0 B1 1 0 0 0 0 0 0 1 1 1 1 1 0 1 1 0 DEGREE SYMBOL BOX ↓ 1 1 1 1 0 1 0 + , 0 1 1 ; < 1 0 0 K L 1 0 1 [ \ . = > M N ] ↑ / ? O ← → 1 1 0 1 1 1 SER4 SER5 SER6 TRIANGLE DIAMOND 6.2.1 Uncorrected Barometric Altitude (203) Source: ARINC 706 DADC or IOC UNCORRECTED BAROMETRIC ALTITUDE LABEL (Octal) 203 Units: Feet Approx. LSB: 1 Foot Max.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.2.7 Latitude (110) - GPS Source: ARINC 743(A) GPSSU LATITUDE – GPS LABEL (Octal) 110 Units: Degrees Approx. LSB: 0.000172 Deg Max. Range: ± 180 Degrees Data Bits: 9 to 28 = 20 + = North Sign Bit: 29 Pad Bits: None Transmit Interval (mSec): 1000 Maximum Data Type: 2’s Complement Binary SDI Bits: 9, 10 6.2.8 Longitude (111) - GPS Source: ARINC 743(A) GPSSU LONGITUDE – GPS LABEL (Octal) 111 Units: Degrees Approx. LSB: 0.000172 Deg Max.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.2.16 Sensor Status (273) - GPS Source: ARINC 743(A) GPSSU SENSOR STATUS – GPS LABEL (Octal) 273 Units: N/A Max. Range: N/A Approx.
Honeywell MK VI MK VIII EGPWS Installation Design Guide BIT 23 (1) = TENS of the MONTH (0 or 1) BITS 24 to 27 (4) = UNITS of the DAY (0 to 9) BITS 28 to 29 (2) = TENS of the DAY (0 to 3) 6.2.19 Control Word (154) - MFD CONTROL WORD – MFD LABEL (Octal) 154 Units: N/A Data Bits: Discrete word, see below Transmit Interval (mSec): 50 ms Bit No. 11 – 13 14 15 – 29 Source: MFD Max. Range: N/A + = N/A Data Type: Discrete Approx.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Bit No. 11–22 23 24 – 29 CONTROL WORD 2 BIT ASSIGNMENTS DEFINITION Spares Display Range Divide by 20 Display Range as specified in the table below BITS 24 to 29 = Display Range (5 to 320NM, format as follows) Bit 29 Bit 28 Bit 27 Bit 26 Bit 25 Bit 24 RANGE 0 0 0 0 0 0 320 NM 0 0 0 0 0 1 5 NM 0 0 0 0 1 0 10 NM 0 0 0 1 0 0 20 NM 0 0 1 0 0 0 40 NM 0 1 0 0 0 0 80 NM 1 0 0 0 0 0 160 NM Note: The range bits are additive; e.g.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 16 17 18 19 20 21 22 23 24 25 26 27 28 29 Range (Start), 0.25 NM, Not Used by EGPWC Range (Start), 0.5 NM, Not Used by EGPWC Range (Start), 1 NM, Not Used by EGPWC Range (Start), 2 NM, Not Used by EGPWC Range (Start), 4 NM, Not Used by EGPWC Range (End), 0.0625 NM, Not Used by EGPWC Range (End), 0.125 NM, Not Used by EGPWC Range (End), 0.25 NM, Not Used by EGPWC Range (End), 0.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Label 011 communicates the response to the KCPB Query / Setup Label (KCPB Label 027) or on a continuous basis. For a detailed description of the Query / Continuous Response Label 011 definition see the EGPWS Interface Methodology, 060-4303-000. 6.2.25 Key Press Data (012) – KCPB KEY PRESS DATA LABEL (Octal) 012 Units: N/A Data Bits: Discrete word Transmit Interval (mSec): 180 Source: Honeywell TDU/FMS Max.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Bits 14 to 16 = Mode, format as follows Bit 16 Bit 15 0 0 0 0 0 1 0 1 1 0 1 0 1 1 1 1 Bit 14 0 1 0 1 0 1 0 1 MODE Standby Weather Only Map Only Windshear Hazard Factor Test Windshear and Turbulence Weather and Turbulence Windshear Icon 6.2.27 Discrete Word (273) – Bendix Weather Radar Vertical Profile Mode Source: EFIS/Weather Radar Discrete Word LABEL (Octal) 273 Units: N/A Max. Range: N/A Approx.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.2.31 Roll Angle (325) Source: ARINC 704 INU / IRS/ AHRS / FMS or IOC ROLL ANGLE LABEL (Octal) 325 Units: Degrees/180 Approx. LSB: 0.01099 Deg Max. Range: ± 180 Degrees Data Bits: 15 to 28 = 14 + = Right Wing Down Sign Bit: 29 Pad Bits: 11 to 14 Transmit Interval (mSec): 10 to 36 Data Type: 2’s Complement Binary SDI Bits: 9, 10 6.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 23-19 24 25 26 27 28 29 Unused (always 0) Program Pin A Status Program Pin B Status Program Pin C Status Program Pin D Status Program Pin E Status Unused (always 0) 6.2.37 True Heading (314) Source: IRS/AHRS/IOC TRUE HEADING LABEL (Octal) 314 Units: Degrees/180 Max. Range: +/- 180 Degrees Approx. LSB: 0.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.2.43 Longitudinal Acceleration (331) Source: IOC LONGITUDINAL ACCELERATION LABEL (Octal) 331 Units: g’s Max. Range: +/-4.0 g’s Approx. LSB: 0.000977 g’s Data Bits: 17 to 28 = 12 + = Forward Sign Bit: 29 Pad Bits: 11 to 16 Transmit Interval (mSec): 10 to 20 Data Type: 2’s Complement Binary SDI Bits: 9, 10 6.2.44 Left Body Angle of Attack (224) Source: IOC Body Angle of Attack LABEL (Octal) 224 Units: degrees Max. Range: +/-180 degrees Approx.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 25 – 28 Navigation data source currently displayed on the Primary Flight Display (PFD).
Honeywell MK VI MK VIII EGPWS Installation Design Guide 22 23 24 25-28 29 Timed Audio Inhibit (momentary) Reserved for EGPWS Test command Bit Steep Approach activated (alternate action) Terrain Display Range (as specified in the table below) Not Used BITS 25 to 28 = Terrain Display Range (0.5 to 2000 NM) format as follows: DISPLAY RANGE BIT ASSIGNMENTS Bits 28-25 DEFINITION Bits 28-25 DEFINITION 0000 0.5 NM 1000 150 NM 0001 1.0 NM 1001 200 NM 0010 2.5 NM 1010 300 NM 0011 5.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.2.53 North/South Velocity (166) - GPS Source: ARINC 743(A) GPSSU NORTH/SOUTH VELOCITY – GPS LABEL (Octal) 166 Units: Knots Approx. LSB: 0.125 Knots Max. Range: ± 4,096 Knots Data Bits: 14 to 28 = 15 + = North Sign Bit: 29 Pad Bits: 11 to 13 Transmit Interval (mSec): 1000 Maximum Data Type: 2’s Complement Binary SDI Bits: 9, 10 6.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.2.59 Latitude Fine (120) - GPS Source: ARINC 743(A) GPSSU Latitude Fine - GPS LABEL (Octal) 120 Units: Degrees Max. Range: +/-0.000172 Deg Approx. LSB: 8.38E-8 Deg Data Bits: 18 to 28 = 11 + = N/A Sign Bit: 29 Pad Bits: 11 to 17 Transmit Interval (mSec): 1000 Maximum Data Type: 2’s Complement Binary SDI Bits: 9, 10 6.2.60 Longitude Fine (121) - GPS Source: ARINC 743(A) GPSSU Longitude Fine - GPS LABEL (Octal) 121 Units: Degrees Max. Range: +/-0.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.3.2 Uncorrected Barometric Altitude (203) Source: ARINC 575 ADC UNCORRECTED BAROMETRIC ALTITUDE LABEL (Octal) 203 Units: Feet Approx. LSB: 1 Foot Max. Range: ± 131,072 Feet Data Bits: 13 to 29 = 17 + = Above Sea Level (ASL) Sign Bit: Part of SSM Pad Bits: 9 to 17 Transmit Interval (mSec): 62.5 Maximum Data Type: 2’s Complement Binary SDI Bits: N/A 6.3.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.4.4 Xpress GPS Packets ID 18: East/North/Up Velocity Byte 0 1-4 5-8 9-12 Data Valid Flag East Velocity North Velocity Up Velocity Type Byte Real Real Real Units Valid = 1, Invalid = 0 Meters/Second Meters/Second Meters/Second 6.4.5 Xpress GPS Packets ID 1C: GPS State This packet contains information concerning the current state of the receiver subsystem.
Honeywell MK VI MK VIII EGPWS Installation Design Guide (*****) NAV Mode (binary) 0 en route 1 terminal 2 approach 3 oceanic (******) Error Status (true if set; false otherwise) 0 not used 1 ROM failure 2 RAM failure 3 Nonvolatile RAM lost 4 RF failure 5 not used 6 not used 7 BaseBand ASIC failure 8 BaseBand ASIC timeout 9 not used 10 RS-232 channel 1 receiver timeout 11 EEPROM failure 12 RS-232 channel 2 fail 13 1 millisecond underflow 14 not used 15 1 millisecond overflow 6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide DISPLAY RANGE BIT ASSIGNMENTS Bits 4 - 7 Range Bits 4 - 7 Range 0100 0.5 NM 0110 150 NM 0010 1.0 NM 1100 200 NM 1111 2.5 NM 1010 300 NM 1011 5.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.6 Discrete Inputs This section contains a brief description of each input discrete is used in the EGPWS. There are 28 possible discrete inputs each have one of the following input characteristics 1) 15 Open/Ground two state discretes 2) 13 Open/28VDC two state discretes The EGPWS supports the following inputs in discrete form.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.6.4 GND Landing Flap Discrete Type: Supplied by Flap or Flap selector handle switch. Signal Status: Landing Flaps or Not Landing Flaps Fault monitoring: Indication of landing flaps selected for more than 60 seconds at airspeeds above 250 (180 for GA Slow) knots will result in a flap switch fault which will cause a GPW INOP indication.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.6.9 +28V ILS Tuned Discrete #1 Type: Supplied by ILS/VOR Mode Selector. Signal Status: ILS tuned or VOR tuned +28 V ILS Tuned Discrete #1 Level 6 Audio readout ILS Tuned => “28 Volts ILS 1 Tuned” ILS Not Tuned => “28 Volts ILS 1 Not Tuned” 6.6.10 Glideslope Validity Discrete #1 A Glideslope Validity Discrete may be used by EGPWS, for the ARINC 547 Glideslope Receiver input. Type: Validity from ARINC 547 Glideslope receiver.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.6.14 Decision Height Discrete Type: Decision Height Bug switch Signal Status: Less than Decision Height or Greater than Decision Height Level 6 Audio readout Less Than DH => “Below DH” Greater Than DH => “Above DH” DH Discrete 6.6.15 Mode 6 Low Volume Discrete Type: Mode 6 low volume select switch Signal Status: Low Volume Select or Normal Volume “Low Volume” in this case refers to the -6db volume level used during Self-Test.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.6.19 Display Select Discrete #2 Type: Supplied by momentarily actuated cockpit manual switch. Signal Status: Terrain Awareness Display (TAD) activated if not active or TAD canceled if currently active. Level 6 Audio readout True => “Display Discrete 2 True” False => “Display Discrete 2 False” Display Select Discrete #2 6.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 6.6.25 Steep Approach Discrete #2 Activates steep approach biasing if Steep Approach Enabled is true (see Category 7, Section 5.3.7). Alt. Action Type: Supplied by an alternate action (latching) and self indicating cockpit switch . Momentary Type: Supplied by a momentary (non-latching) switch with switch lamp driven by EGPWS Steep Approach Discrete output.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7 OUTPUT DATA DEFINITION 7.1 ARINC 429 Output Data The MK VI and VIII EGPWC provides one or two ARINC 429 low or high-speed output channels per section 5.3.6.3. The output consist of internal parameters that can be used for display selection, test purposes, and discrete outputs that can be used for discrete outputs, test and recording. During LRU Self-Test the SSM of each output label is set to the Functional Test status code.
Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE 7.1-1: ARINC 429 DITS OUTPUTS 270 271 272 273 274 300 7.1.1.1 7.1.1.2 7.1.1.3 7.1.1.4 7.1.1.5 7.1.1.6 135 164 261 067 310 311 223 224 242 331 332 362 364 375 376 7.1.2.1 7.1.2.2 7.1.2.3 7.1.2.4 7.1.2.5 7.1.2.6 7.1.2.7 7.1.2.8 7.1.2.9 7.1.2.10 7.1.2.11 7.1.2.12 7.1.2.13 7.1.2.14 7.1.2.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.1.1 Discrete Output Words The discrete output words transmit the status of all MK VI, and VIII EGPWC discrete and audio outputs. Label 274 is typically used to drive EFIS and/or EICAS displays. The other discrete labels are typically only used for flight recording and test purposes. 7.1.1.1 EGPWS Alert Discrete #1 (270) Data: Discrete Label: 270 Octal Significant Bits: (see table below) Sign Bit: N/A Transmit Interval: 100 msec ± 10% Bit No.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.1.1.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.1.1.5 EGPWS Alert Discrete #2 (274) Data: Discrete Label: 274 Octal Significant Bits: (see table below) Sign Bit: N/A Transmit Interval: 50 to 100 msec Bit No.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.1.2 Internal Data Outputs Internal data outputs are only used for test purposes. Tables 7.1.2.1 through 7.1.2.6 are available for both MKVI and MKVIII EGPWS. Tables 7.1.2.7 through 7.1.2.15 are are only output when the Honeywell Windshear Algorithm is enabled (available only on the MKVIII EGPWS) and are only used for test purposes. 7.1.2.1 Geometric Altitude VFOM (135) LABEL (Octal) 135 Units: Feet Max. Range: 32,768 Ft Approx. LSB: 0.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.1.2.8 Body Angle of Attack—Left (224) – MKVIII EGPWS w/ Windshear only Units: Degrees/180 Approx. LSB: 0.00549 Degree LABEL (Octal) 224 Max. Range: ± 180 Degrees Data Bits: 14 to 28 = 15 + = Nose Up Sign Bit: 29 Pad Bits: 11 to 13 Data Type: 2’s Compliment Binary SDI Bits: 9, 10 Transmit Interval (mSec): 100 ± 20% 7.1.2.9 Corrected Airspeed (242) – MKVIII EGPWS w/ Windshear only Units: Feet/Second LABEL (Octal) 242 Max. Range: 2048 Ft/Sec Approx.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.1.3 Terrain Display Outputs The following ARINC 429 outputs support the Terrain Display function. 7.1.3.1 Displayed Range (050) Data: Discrete BIT NO 11 – 14 15 – 18 19 - 29 Label (Octal): 050 Transmit Interval: 200 msec ± 10% DEFINITION TERRAIN DISPLAY RANGE #1 (0.5 to 2000 NM format) TERRAIN DISPLAY RANGE #2 (0.5 to 2000 NM format) UNDEFINED NOTE: Bits contain left and right side Terrain Display Ranges (0.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.1.3.3 Message Word #1 (052) This label contains the color to be displayed on the 6-character terrain display window.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.1.3.5 Message Word #3 (054) This label contains the second 2 characters to be displayed on the 6 character terrain display window.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.1.4 Equipment Identification Provides equipment identification for maintenance reporting. 7.1.4.1 Equipment Identification Word (377) Data: Discrete Label (Octal): 377 BIT NO DEFINITION 11 - 22 ID Code 23 - 29 Spare (set to zero) Transmit Interval: 500 msec ± 10% Equipment ID code = 023 Hex for EGPWC. 7.1.5 Fault Summary Words (for Proline 4/21) Provides fault diagnosis information. 7.1.5.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.1.5.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.1.6.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.4.2 Audio On Discrete The Audio On discrete goes true whenever any voice message is being enunciated. It will stay true until the voice is completed. This output can be used to inhibit other audio systems (e.g., TCAS) during EGPWS audio or used to drive the audio key line input provided on some aircraft audio systems. 7.4.3 Monitor Discretes (GPWS INOP & Terrain INOP or Terrain Not Available) The EGPWC produces two discrete monitor outputs.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.4.11 Windshear Caution The MK VIII EGPWC Windshear Cautions can be configured to activate any of the discrete outputs. Depending on configuration, the Caution discrete will typically drive its own output lamp or provide a discrete output to other aircraft systems. 7.4.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 7.5.1 System Status Messages System Status Messages provide additional information beyond Internal and External Current Faults in order to help isolate the reason for certain EGPWC INOP situations. These messages will be read out during Present Status on the RS-232 interface or voice output during Self-Test Level 2. The table below defines the System Status Messages. TABLE 7.5.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 8 CONNECTOR INTERFACE 8.1 Pinout for Front Connectors sorted by pin number Table 8.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Connector Pin J1-49 J1-50 J1-51 J1-52 Channel Designation Reference DISC_OUT_9 MON_OUT_3 DISC_OUT_8 DISC_OUT_7 J1-53 J1-54 J1-55 J1-56 J1-57 J1-58 J1-59 J1-60 J1-61 J1-62 J1-63 J1-64 J1-65 J1-66 J1-67 J1-68 J1-69 J1-70 J1-71 J1-72 J1-73 GND DISC_OUT_6 MON_OUT_2 453TX_2A 453TX_2B 453TX_1A 453TX_1B PWR_H PWR_L ALT_H OAT_H RALT_H GSDEV_H J1-74 J1-75 J1-76 J1-77 J1-78 AUD_LL_L AUD_LL_H DISC_OUT_3 DISC_OUT_2 DISC_OUT_1 J2-01 J2-02 J2-03 J2-04 J2-05 J2
Honeywell MK VI MK VIII EGPWS Installation Design Guide Connector Pin Channel Designation Reference J2-23 429RX_7A J2-24 J2-25 J2-26 J2-27 429RX_8A 429RX_4A 429TX_2A ADC_TXA J2-28 J2-29 GND GPS_RXA J2-30 J2-31 J2-32 J2-33 J2-34 J2-35 J2-36 429TX_GPS_A GND_DISC_15 SPICLK SPIMISO 26REF_2H 26REF_2L 429/422RX_1B J2-37 429/422RX_1A J2-38 J2-39 J2-40 429RX_2B 429RX_2A Signal Usage Summary AHRS ARINC 429 Input A leg GPS #2 ARINC 429 Input A leg Spare ARINC 429 Input (A leg) GPS ARINC 429 Input (A leg
Honeywell MK VI MK VIII EGPWS Installation Design Guide Figure 8.1-1, Front Panel Connector Orientation - J1, J2, J3, GPS ANT Note: The GPS ANT connector only applies to the 965-1190-0xx and the 965-1220-0xx. MK VI EGPWS shown.
Honeywell MK VI MK VIII EGPWS Installation Design Guide Figure 8.
Honeywell MK VI MK VIII EGPWS Installation Design Guide 9 DEFINITIONS The following acronyms are provided for use with this document: Acronym Interpretation AAAS ADC ADS AGC AGL AHRS AIC AIMS ASA AOA ASL ATP BCD BIST BIT BITE BNR C/O CAA CAIMS CFDS CFIT CFM CISRD CMC COTS CP CRS CW DAA DADC DAU DC DDM DEVN DH DITS DME DO DSP DSU DSWC EEPROM EFCP EFIS EGPWC EGPWD EGPWS EICAS EMI ENB EPROM F/T F/W Alternate Audio Alert Select Air Data Computer Air Data System Automatic Gain Control Above Ground Level A
Honeywell MK VI MK VIII EGPWS Installation Design Guide Acronym Interpretation FAA FCC FDR FIAS FMC FMS FPM FSEU FWC G/S GMT GPS GPW GPWS GT H/W HDG HDOP HFOM HSID I/O IAC ICD ILS INOP IOC IRS ISO IVS KT KTS LED LRRA LRU LSB LT MCP MDA MFD MKII MKV MKVI MKVII MKVIII MLS MMU MSB MSL N/A NCD ND NVM OMS P/N PAR PC PCMCIA PFD Federal Aviation Administration Flight Control Computer Flight Data Recorder Flight Inspection Aircraft System Flight Management Computer Flight Management System Feet per Minute Flaps
Honeywell MK VI MK VIII EGPWS Installation Design Guide Acronym Interpretation PMAT PP PVM PWS QFE QNH RA RAM RDOP ROM RTCA RTS RWY S/T S/W SDI SDRD SIG SPC SRD SSM ST SWC TA&D TACAN TAD TBD TCAS TCF TERPS TK TLB TSO TTL UART USM UTC UUT VDC VDOP VFOM VHF VLSI VOR W/S WC WGS-84 WX Portable Maintanence Access Terminal Program Pin Processor/Voice/Memory Predictive Windshear System Corrected Baro Alt relative to field elevation Corrected Baro Alt relative to sea level Radio Altitude Random Access Memory Ra