Installation Manual

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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV:C SHEET 1 OF 254

Airlines & Cvionics Products

Honeywell International, Inc.

15001 N.E. 36 th Street

Redmond, WA 98052

MK XXII

Enhanced Ground Proximity

Warning System

for

Rotorwing

Aircraft

Installation Manual

060-4314-225 Rev C

Part Numbers:

965-1590-006

965-1590-008

965-1590-010

965-1590-011

Release Date: 12/14/00

Summary of content (254 pages)

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Airlines & Cvionics Products Honeywell International, Inc. 15001 N.E.
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Honeywell MK XXII EGPWS Installation Manual This document is an unpublished work. Copyright 2000 Honeywell, International, 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.
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Honeywell MK XXII EGPWS Installation Manual Typed names constitute approval signatures. Actual signatures are on file at Honeywell in Redmond, WA. DRAWN Dennis Martin 12/8/00 CHECK Sara Stark 12/8/00 ENGR Dennis Martin 12/8/00 Dennis Martin 12/8/00 MFG QA APVD APVD REVISIONS SH REV ALL A DESCRIPTION DATE APPROVED 8/9/01 S. Wright 8/9/01 D. Martin 3/22/02 D. Martin 3/22/02 R Gilliland 6/07/02 D Martin 6/7/02 T Curtis Added Software –008 Revisions.
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 4
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Honeywell MK VI MK VIII EGPWS Installation Design Guide TABLE OF CONTENTS SECTION I – GENERAL INFORMATION............................................................................................ 16 1.1 INTRODUCTION .................................................................................................................................... 16 1.2 APPLICABILITY .................................................................................................................................... 16 1.
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Honeywell MK VI MK VIII EGPWS Installation Design Guide 1.11.3 Insertion/Removal Tool - P1, P2, P3 .................................................................................... .... 28 1.11.4 Spare Contacts - P1, P2, P3 ...................................................................................................... 28 1.12 LICENSE REQUIREMENTS ................................................................................................................... 28 SECTION II - INSTALLATION ........
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Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.3.2 Category 2 – Air Data Input Select....................................................................................... ....................................61 3.3.2.1 Instructions ........................................................................................................... ................................. 61 3.3.2.2 Examples ..........................................................................................................
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Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.3.9.3 Analog Glideslope Interface (cat. 9 ID 0,1,5) ................................................................................... 87 3.3.9.4 Digital Glideslope/Localizer Interface .............................................................................................. 88 3.3.9.5 Dual Glideslope Receiver.................................................................................................................. 88 3.3.
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Honeywell MK VI MK VIII EGPWS Installation Design Guide 3.3.14.1 Instructions .......................................................................................................... .............................. 104 3.3.15 Category 15, Autorotation Threshold ..................................................................................... ..............................105 3.3.15.1 Instruction...........................................................................................................
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Honeywell MK VI MK VIII EGPWS Installation Design Guide APPENDIX C..................................................................................................................... ....................................................143 WINVIEWS OPERATION INSTRUCTIONS ................................................................................................ ...................143 APPENDIX D..............................................................................................................
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Honeywell MK VI MK VIII EGPWS Installation Design Guide E 4.2.17.1 ARINC 429 Output Bus................................................................................................. ...........................177 E 4.2.17.2 ARINC 453 Output Bus................................................................................................. ...........................178 E 4.2.18 FRONT PANEL TEST INTERFACE................................................................................................
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Honeywell MK XXII EGPWS Installation Manual SECTION I GENERAL INFORMATION CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 12
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 13
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Honeywell MK XXII EGPWS Installation Manual SECTION I – GENERAL INFORMATION SECTION I – GENERAL INFORMATION............................................................................................ 16 1.1 INTRODUCTION .................................................................................................................................... 16 1.2 APPLICABILITY ....................................................................................................................................
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Honeywell MK XXII EGPWS Installation Manual 1.12 LICENSE REQUIREMENTS ...................................................................................................................
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Honeywell MK XXII EGPWS Installation Manual SECTION I – GENERAL INFORMATION 1.1 Introduction The Honeywell MK XXII Enhanced Ground Proximity Warning System (MK XXII EGPWS) provides alerts and warnings to prevent controlled flight into terrain (CFIT). This Installation Manual must be used in conjunction with the Interface Description Document (Appendix E) for the MK XXII Enhanced Ground Proximity Warning System (MK XXII EGPWS) to select features and design the installation for this system.
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Honeywell MK XXII EGPWS Installation Manual 1.
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Honeywell MK XXII EGPWS Installation Manual 1.5 Description of Equipm ent The MK XXII EGPWS is a rack mount ground proximity warning (GPWS) and terrain display (TAWS) computer.
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Honeywell MK XXII EGPWS Installation Manual 1.5.1 MK XXII EGPWS Comp uter The MK XXII EGPWS computer is available under P/N 965-1590-0XX with internal GPS. The MK XXII EGPWS computer is intended for Helicopters and provides a mixture of analog and digital interfaces. The type of supported displays is limited and includes some EFIS displays.
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Honeywell MK XXII EGPWS Installation Manual 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 computing Geometric Altitude. If Outside Air Temperature is not available, Geometric Altitude is computed using pressure altitude with a corresponding reduction in accuracy.
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Honeywell MK XXII EGPWS Installation Manual FIGURE 1-1 MK XXII EGPWS SMART CABLE 1.6 Technical Characteris tics MK XXII EGPWS TSO Compliance: TSO-C92c, TSO-C151a, class A Physical size (HxWxD): 6.20” x 3.04” x 10.30” Weight: 3.
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Honeywell MK XXII EGPWS Installation Manual Physical size: 2.68” x 1.51” x 0.32” (fits Positronic connector backshell) Weight: <1 pound with connector and backshell Mounting: Mounts to Positronic connector backshell Temperature (operational): same as MK XXII EGPWS Altitude range: same as MK XXII EGPWS Cooling: No cooling necessary Shock: No shock mounting required Power Consumption (5 VDC): from MK XXII EGPWS GPS Antenna Sensor See Manufacturer’s specifications Appendix D.
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 23
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Honeywell MK XXII EGPWS Installation Manual 1.8 Installation and Acces sories Kits NOTE: Not all installation kits are immediately available, contact Honeywell Order Administration (425-885-8719) for availability. 1.8.1 MK XXII EGPWS Insta llation Kits (A) New EGPWS installation with OAT and Internal GPS The MK XXII EGPWS Installation Kit #1, P/N 755-7013-001, contains the following parts: Vendor Name Vendor P/N Description QTY UM Honeywell P/N Positronic Ind.
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Honeywell MK XXII EGPWS Installation Manual 1.8.
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Honeywell MK XXII EGPWS Installation Manual Vendor Name Vendor P/N Description QTY UM Emteq D 07002-100 ARINC 453 Cable A/R EA M17/176-00002 Military Specification A/R EA Honeywell P/N 1.9.
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Honeywell MK XXII EGPWS Installation Manual 1.9.4.2 GPWS Caution (amber) G/S CANCLD switch/annunciator assembly. The ‘GPWS caution annunciator provides visual indication of an EGPWS alert. The EGPWS caution (amber) annunciator also has a switch that is used to manually inhibit EGPWS Mode 5 glideslope alerts. The bottom half of the annunciator provides visual indication that the mode 5 glideslope alerts have been canceled. 1.9.4.
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Honeywell MK XXII EGPWS Installation Manual 1.11 Tools Required 1.11.1 Crimping Tool - P1, P 2, P3 Description UM QTY Vendor Name & Part Number Hand Crimping Tool EA 1 Positronic Ind. 9507 Hand Crimping Tool EA 1 Daniels AFM8 Hand Crimping Tool EA 1 Military M22520/2-1 1.11.2 Contact Positioner - P 1, P2, P3 Description UM QTY Vendor Name & Part Number Contact Positioner, Socket P1 EA 1 Positronic Ind.
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 29
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Honeywell MK XXII EGPWS Installation Manual SECTION II INSTALLATION CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 30
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 31
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Honeywell MK XXII EGPWS Installation Manual SECTION II – INSTALLATION SECTION II - INSTALLATION .............................................................................................................................. 33 2.1 INTRODUCTION .................................................................................................................................................... 33 2.2 UNPACKING AND INSPECTING THE EQUIPMENT .........................................................................
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Honeywell MK XXII EGPWS Installation Manual SECTION II - INSTALLATION 2.1 Introduction 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.
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Honeywell MK XXII EGPWS Installation Manual 2.3.2 MK XXII Computer Loc ation Care should be exercised to avoid mounting components near equipment operating with high pulse current or high power outputs such as radar and satellite communications equipment. In general, the equipment should be installed in a location convenient for operation, inspection, and maintenance, and in an area free from excessive vibration, heat, and noise generating sources.
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Honeywell MK XXII EGPWS Installation Manual E. Slide the EGPWS unit in the mounting tray, and secure it using the Hold Down latch. F. (After Continuity and Power check) Attach the cable harness to the front panel connectors and lock connectors using the slide lock of the P1 & P2 connectors. The EGPWS should be wired according to the interconnect diagrams in Section III, of this manual. 2.3.
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Honeywell MK XXII EGPWS Installation Manual 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.
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Honeywell MK XXII EGPWS Installation Manual INSTALLATION ASSEMBLY SEQUENCE STEP 1 Install all MK XXII system aircraft wiring to this connector using items 1.2 (Crimp Contacts) and item 1.1 (Connector). See figure 2-1.1 below. FIGURE 2-1.
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Honeywell MK XXII EGPWS Installation Manual 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 2-1.
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Honeywell MK XXII EGPWS Installation Manual STEP 3 Position item 1.7 (Slide lock) onto wired connector as shown in figure 2-1.3 below: FIGURE 2-1.
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Honeywell MK XXII EGPWS Installation Manual 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 2-1.
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Honeywell MK XXII EGPWS Installation Manual STEP 5 Install item 1.6 (Spring Clip) as shown figure 2-1.5 below: FIGURE 2-1.
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Honeywell MK XXII EGPWS Installation Manual 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 2-1.
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Honeywell MK XXII EGPWS Installation Manual 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 2-1.
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Honeywell MK XXII EGPWS Installation Manual 2.3.6 GPS Antenna location The antenna must be mounted on top of the fuselage. Avoid mounting the antenna near any projections such as the rotor mast, or engine exhaust, where shadows could occur or high heat could damage the antenna. It is recommended that there be a separation of at least 3 feet between the GPS antenna and any VHF Comm antenna on the aircraft.
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Honeywell MK XXII EGPWS Installation Manual 2.3.10.1 Description EGPWS warning GPWS P/TEST This assembly is illuminated with Red background and black or white letters. For dark cockpits black background and Red letters. The EGPWS warning annunciator is not normally dimmable. For Lamp Format 1 (I/O Discrete Type 128) the lamp is activated during any Mode 1 through Mode 4, and Terrain /Obstacle Awareness alerts and warnings.
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Honeywell MK XXII EGPWS Installation Manual 2.3.10.2 Location Cockpit layout, size and operator’s preference will determine if only one set of lights is used (i.e., mounted in the center), or if dual sets of lights are used (one set on each side), or a combination thereof is desired. For a typical example of cockpit light locations refer to Figure 2-7. For panel cutouts and assembly options see the manufacturer’s specifications in Appendix D.
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Honeywell MK XXII EGPWS Installation Manual FIGURE 2-1.
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Honeywell MK XXII EGPWS Installation Manual 2.3.10.3 Inhibit Switch Functio ns and Selection The Terrain Inhibit and Audio Inhibit functions are optional but it is recommended that one be used to inhibit the system during certain operations. The operator should evaluate the two options together with the Low Altitude Mode function and select the one that best fits his operational requirements. The Low Altitude Mode is also described below for reference. 2.3.10.3.
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Honeywell MK XXII EGPWS Installation Manual FIGURE 2-2 MK XXII EGPWS OUTLINE CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 49
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Honeywell MK XXII EGPWS Installation Manual FIGURE 2-3 MK XXII EGPWS MOUNTING TRAY Honeywell P/N 405-0383-001 CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 50
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 51
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Honeywell MK XXII EGPWS Installation Manual SECTION III SYSTEM PLANNING CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 52
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 53
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Honeywell MK XXII EGPWS Installation Manual SECTION III – SYSTEM PLANNING SECTION III – SYSTEM PLANNING..................................................................57 3.1 INTRODUCTION .................................................................................................................................... 57 3.2 SYSTEM WIRING/ ELECTRICAL INTERFACES........................................................................................ 57 3.2.1 Primary Power Input ............................
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Honeywell MK XXII EGPWS Installation Manual 3.3.6.3 Terrain Display Configuration Group.................................................................................................... 73 3.3.6.4 Display Input Control Group ................................................................................................................. 75 3.3.6.5 Output 429 Bus Group........................................................................................................................... 75 3.3.6.
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Honeywell MK XXII EGPWS Installation Manual 3.3.13.5 Weight ON Wheels (WOW) Discrete ............................................................................................. 97 3.3.13.6 Glideslope Cancel Discrete ............................................................................................................. 98 3.3.13.7 Mode 6 Low Volume Discrete ........................................................................................................ 98 3.3.13.8 Autopilot Engaged Discrete .
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Honeywell MK XXII EGPWS Installation Manual SECTION III – SYSTEM PLANNING 3.1 Introduction This section provides information for selecting features and wiring the electrical interfaces of the MK XXII EGPWS. Sample wiring diagrams for the most commonly used MK XXII EGPWS configurations are provided in Appendix B. Appendix E Section E 3 groups features (functions) into sets called Categories. This document follows the Category structure of the Appendix E .
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Honeywell MK XXII EGPWS Installation Manual 3.2.3 GPS Antenna A GPS antenna connector is available on the front of the MK XXII EGPWS 965-1590-0XX. 3.2.4 Analog and Digital Inp uts The analog and digital inputs to the MK XXII EGPWS are defined as the Categories are selected. Instructions for documenting these interfaces are provided with the Category selection instructions. Section 3.3 contains detailed category configuration information. 3.2.
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Honeywell MK XXII EGPWS Installation Manual 3.2.7 Audio Output 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 Outputs The MK XXII EGPWS provides for up to twelve 0.
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Honeywell MK XXII EGPWS Installation Manual 3.3 Configurable Interface s The following subsections define configurable interfaces for the EGPWS. Typical interface connection information and diagrams are provided. Use this in conjunction with Appendix E which has detailed interface configuration information. 3.3.1 Category 1 - Aircraft / Mode Type Select Category 1 specifies the general aircraft type, warning mode definitions, , fixed or retractable gear, and engine torque interface.
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Honeywell MK XXII EGPWS Installation Manual not detect autorotation and thus do not provide the autorotation altitude callouts or advanced gear warnings. Mode 1 is inhibited in these types. The generic types are segregated into retractable and fixed gear configurations and tail strike warning profiles. Contact the Honeywell GPWS hot line 1 800 813-2099 for help in selecting the correct generic type.
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Honeywell MK XXII EGPWS Installation Manual 3.3.2.2 Examples 3.3.2.3 Analog altitude and 500 ohm OAT EGPWS MK XXII Uncorrected Barometric Altitude J1 Analog Air Data Computer (+) 62 Altitude Out (-) 43 Signal Common Baro Altitude Valid +28V BIT Out 9 +5V Excitation 25 (+) 63 500 ohm Temperature Probe Temp. Input (-) 44 Chassis Ground 53 Analog-ADC.
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Honeywell MK XXII EGPWS Installation Manual 3.3.2.4 Digital – ARINC 429 (Cat. 2 ID 5, 1, 6) Air Data Type 1 (AZ-800 or equivalent) is a low speed, digital ARINC 429 signal having the air data labels 203, 206, 212, and 213. Air Data Type 5 (AZ-800 or equivalent) is a low speed, digital ARINC 429 signal having the air data labels 203, 204, 206, 212, and 213. Air Data Type 6 (AZ-800 or equivalent) is a low speed, digital ARINC 429 signal having the air data labels 203, 206, and 213.
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Honeywell MK XXII EGPWS Installation Manual 3.3.2.5 Digital –ARINC 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. J2 EGPWS MK XXII ARINC 575 Air Data Bus ARINC 575 Air Data A 39 A ARINC 575 Bus - Hi B 38 B ARINC 575 Bus - Lo ARINC575-ADC.
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Honeywell MK XXII EGPWS Installation Manual 3.3.2.6 Shadin 2000 (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) 500ohm probe using +5 volt excitation from the MK XXII EGPWC.
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Honeywell MK XXII EGPWS Installation Manual 3.3.2.7 Digital – ARINC 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. EGPWS MK VI / MK VIII ARINC 429 High Speed ARINC 429 High Speed J2 IOC Buses A 39 A B 38 B A 41 A B 40 B IOC Bus 1 IOC Bus 2 ARINC429-IOC.
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Honeywell MK XXII EGPWS Installation Manual 3.3.3 Category 3 – Position Input Select Category 3 defines the Global Position System bus type and interface. GPS Input selection is available in the following formats: ARINC 429 low speed and ARINC 429 high speed in either ARINC 743 or 743A format, RS-232, and Internal GPS card. CAUTION Not all GPS receivers calculate Horizontal Figure of Merit (HFOM) and Vertical Figure of Merit (VFOM) correctly and thus are unacceptable sources of position.
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Honeywell MK XXII EGPWS Installation Manual 3.3.3.Examples 3.3.3.1 ARINC 429 BUS (Cat. 3 ID 0,1,4,5) EGPWS MK XXII J2 ARINC 429 GPS Bus ARINC 429 GPS A 25 A ARINC 429 Bus - Hi B B ARINC 429 Bus - Lo 8 ARINC429-GPS.vsd Vendor Model GNS-XLS (17960-0203-) 429 GPS Alt ARINC Speed Ref.
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Honeywell MK XXII EGPWS Installation Manual 3.3.3.3 Dual ARINC 429 BUS (Cat. 3 ID 255) NOTE: If GPS #2 is not installed in the aircraft, then GPS bus #1 must be connected in parallel to both EGPWS GPS input ports. J2 EGPWS MK XXII ARINC 429 GPS Bus ARINC 429 GPS Bus ARINC 429 GPS A 25 A Hi B 8 B Lo A 23 A Hi B B ARINC 429 Bus 1 ARINC 429 Bus 2 6 Lo ARINC429-DualGPS.vsd 429 GPS Alt ARINC Speed Ref.
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Honeywell MK XXII EGPWS Installation Manual 3.3.4 Category 4 – Altitude Callouts Category 4 defines the Altitude Callout menu choices and Smart ‘500’ Callout selection along with Autorotation callout enablement. Appendix E Table E 3.1.4 defines the Altitude Callout Menu options and identifies the first MK XXII EGPWS version in which the option was available (see the Effectivity entry).
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Honeywell MK XXII EGPWS Installation Manual 3.3.5 Category 5 – Audio Menu Select Category 5 defines one Audio Menu options for Helicopters (ID 128). 3.3.5.1 Instructions 1. Using Appendix E Tables E 3, Under Step/category 5 select Audio Menu. Using table E 3.1.5, select ID number for your audio menu and record that number on Table E 3 under Ident No. This number will be used for programming the configuration module. 2.
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Honeywell MK XXII EGPWS Installation Manual 3.3.6 Category 6 – Terrain Display Select Category 6 defines the Terrain Display options available. Appendix E Table E 3.1.6 defines the Terrain Display Select options (Display Configuration Group Tables, Display Input Control Group Tables and Output 429 Bus Group Tables) and identifies the first MK XXII EGPWS version in which the option was available (see the Effectivity entry). Note: TA&D mode enabling/disabling is controlled by Category 6.
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Honeywell MK XXII EGPWS Installation Manual 3.3.6.3 Terrain Display 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.
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CAGE CODE: 97896 SCALE: NONE SIZE: A J1-32 J1-31 J1-54 DSD #2 Gnd Gnd J1-56 J1-57 A 453 #2 B DSD #1 Gnd J1-58 J1-59 A 453 #1 B J1-51 J2-41 J2-40 A B Range #2 Gnd J2-37 J2-36 A B Range #1 DWG NO: 060-4314-225 Momentary ON BRT/ DIM/ TEST 453 OUT DISPLAY RELAY ARINC 429 RANGE BUS FIGURE 3.3.
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Honeywell MK XXII EGPWS Installation Manual 3.3.6.4 Display Input Control Group This input bus is connected to the display (or display controller) and transmits Range settings, Display Mode, and Display status to the MK XXII EGPWC. 3.3.6.5 Output 429 Bus Group This output bus is commonly connected to EFIS and/or EICAS displays and Flight Recorders and transmits MK XXII EGPWC alert, fault, and mode status to other systems. 3.3.6.
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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 Lamp Test 28V Lamp Dimming Bus 3 B 57 REV: C MK XXII 965-1590-006 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 A 1 A 56 SHEET 76 80-5145-X-2 TRA45.
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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 Lamp Test 28V Lamp Dimming Bus N6 B B 36 Q6 B A 41 REV: C SHEET 77 Q6 B B 57 MK XXII 965-1590-006 or later. Terrain INOP (out) 55 Note: GNS-XLS will not perform auto pop-up during Alert. For interface and operation of the GNS-XLS see Honeywell GNS-XLS System Installation Manual 006-10528-0000 GNS-XLS.
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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 Lamp Test 28V Lamp Dimming Bus REV: C SHEET 78 MK XXII 965-1590-006 or later. Terrain INOP (out) 55 Note: For interface and operation of the Avidyne FSD see Avidyne FSD Installation Manual P/N 600-0067 D98-00001-5X Avidyne.
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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C B 57 A 56 B 59 A 58 Terrain INOP (out) 55 Terrain Inhibit (in) 12 Terrain Display Select (out) 54 MK XXII 965-1590-006 or later.
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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 open TERR momentary A B 57 A 56 REV: C MK XXII 965-1590-006 or later.
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Honeywell MK XXII EGPWS Installation Manual 3.3.7 Category 7 – Options Select Group #1 Category 7 enables/disables the following Options: Steep Approach (not available in MkXXII), TA&D Alternate Pop Up, Peaks Mode, Obstacle Awareness, Bank Angle, WOW Reversal, and GPS Altitude Reference. Appendix E Table E 3.1.7 defines the Options Select group and identifies the first MK XXII EGPWS version in which the option was available (see the Effectivity entry).
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Honeywell MK XXII EGPWS Installation Manual For Helicopters TA&D Alternate Pop Up should always be set to False. 3.3.7.4 Peaks Mode Peaks mode is an alternate means of displaying terrain data. The standard terrain display mode displays terrain relative to the aircraft altitude that is within the aircraft envelope (the terrain is above or not more than 2000 feet below the aircraft). The terrain display is typically blank during the cruise portion of a flight.
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Honeywell MK XXII EGPWS Installation Manual 3.3.7.8 WOW Reversal The WOW discrete input is defined in Category 13. The Category 7 control is used to reverse the defined logic to match aircraft wiring, if necessary.
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Honeywell MK XXII EGPWS Installation Manual 3.3.8 Category 8 – Radio Altitude Input Select Category 8 defines the Radio Altitude and Decision Height interface. 3.3.8.1 Instructions 1. Using Appendix E Tables E 3, under Step/category 8 select Radio Altitude Type. Using table E 3.1.8 and E 3.1.8-x select ID number for your Radio Altimeter and record that number on Table E 3 under Ident No. for step 8. This number will be used during programming of the configuration module. 2. Appendix E Tables E 3.1.
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Honeywell MK XXII EGPWS Installation Manual 3.3.8.
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Honeywell MK XXII EGPWS Installation Manual 3.3.9 Category 9 – Navigation Inputs Select Category 9 selects the Glideslope and Localizer Deviation interfaces and Glideslope Validity and ILS Tuned discretes. Appendix E Table E 3.1.9 defines the Category 9 Navigation Inputs Select options (called Navigation Inputs Select Types) and identifies the first MK XXII EGPWS version in which the option was available (see the Effectivity entry). 3.3.9.1 Instructions 1. Using Appendix E Tables E 3, E 3.1.9 and E 3.1.
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Honeywell MK XXII EGPWS Installation Manual 3.3.9.2 Example 3.3.9.3 Analog Glideslope Interface (cat.
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Honeywell MK XXII EGPWS Installation Manual 3.3.9.
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Honeywell MK XXII EGPWS Installation Manual 3.3.10 Category 10 – Attitude Input Select Category 10 defines the Roll and Pitch Attitude interface. 3.3.10.1 Attitude Signals Roll Angle is used for Bank Angle callout, Pseudo Altitude Algorithm and Terrain Awareness display. Pitch Angle is used for the Tail Strike alert. NOTE: For MD900 series aircraft where no Tail Strike alert is applicable, Pitch is not required, so a roll only configuration may be selected. Appendix E Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual 3.3.10.3 Example 3.3.10.
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Honeywell MK XXII EGPWS Installation Manual 3.3.10.5 Digital ARINC 429 High Speed Attitude Input ID 128 (Litef LCR 92S or equivalent) is a high speed, digital ARINC 429 signal having roll pitch angle, and roll pitch rate labels 325, 324, 327, and 326.
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Honeywell MK XXII EGPWS Installation Manual 3.3.11 Category 11 – Heading Input Select Category 11 defines the Magnetic Heading interface. Appendix E Table E 3.1.11 defines the Heading Input Select types and identifies the first MK XXII EGPWS version in which the option was available (see the Effectivity entry). 3.3.11.1 Instructions 1. Using Appendix E Tables E 3, E 3.1.11 and E 3.1.
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Honeywell MK XXII EGPWS Installation Manual 3.3.11.3 Example 3.3.11.3.1 Analog Heading (Synchro) (CAT.
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Honeywell MK XXII EGPWS Installation Manual 3.3.11.3.2 Digital ARINC 429 High Speed Heading Input ID (Litef LCR 92S or equivalent) is a high speed, digital ARINC 429 signal having roll angle, pitch angle, roll rate, pitch rate, and heading labels 320, 325, 324, 327, and 326.
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Honeywell MK XXII EGPWS Installation Manual 3.3.12 Category 12 – Windshear Input Select Category 12 defines the Windshear interface. Windshear is not applicable to MK XXII. 3.3.12.1 Instruction Select ID 0 for all helicopter configurations.
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Honeywell MK XXII EGPWS Installation Manual 3.3.13 Category 13 – 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 E 3.1.13 defines the Input/Output discretes options and identifies the first MK XXII EGPWS version in which the option was available (see the Effectivity entry). 3.3.13.1 Instruction 1. Using Appendix E Tables E 3, E 3.1.13, and E 3.1.
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Honeywell MK XXII EGPWS Installation Manual 3.3.13.3 Audio Inhibit Discrete The Audio Inhibit discrete is an optional input to maintain audio and visual prioritization. When activated, this discrete inhibits all audio (Ground Proximity and Terrain Awareness). Activation of the Audio Inhibit input for more than 60 seconds will result in the “All Modes Inhibit” fault.
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Honeywell MK XXII EGPWS Installation Manual NOTE: The logic sense of the WOW discrete can be reversed by selecting the WOW eversal option in Category 7, see section 3.3.7. 3.3.13.6 Glideslope Cancel Discrete The Glideslope Cancel discrete provides the crew with the capability to manually cancel Mode 5 for an approach. This is automatically reset when the aircraft descends below 30 feet or ascends above 2000 feet or by selecting a non-ILS frequency.
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Honeywell MK XXII EGPWS Installation Manual 3.3.13.9 Terrain Awareness Inhibit The Terrain Awareness inhibit discrete, inhibits the Terrain Awareness modes in the MK XXII EGPWS. This discrete is typically connected to an “alternate action switch” in the cockpit. The recommended label for this switch is “Terrain Override” although labeling for this switch should be consistent with existing cockpit nomenclature.
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Honeywell MK XXII EGPWS Installation Manual 3.3.13.12 Timed Audio Inhibit Discrete The Timed Audio Inhibit will cause the inhibiting of all audio messages for a period of 5 minutes or until reset. The discrete input is connected to a momentary lighted switch. When pressed the condition is latched in memory and will be reset after 5 minutes have elapsed or pressing the switch again or when landing. The switch lighting, indicating the Audio is Inhibited is driven by a discrete output described below.
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Honeywell MK XXII EGPWS Installation Manual For Lamp Format Type 1, the amber “Below G/S” lamp is driven by the GPWS Alert (Glideslope only) discrete and the red “GPWS” lamp is driven by the remaining alerts and warnings. For Lamp Format Type 2, the red “EGPWS” lamp is driven by the GPWS Warning (Pull Up, Warning Terrain, and Warning Obstacle only) discrete and the amber “EGPWS” lamp is driven by the remaining alerts and warnings. 3.3.13.
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Honeywell MK XXII EGPWS Installation Manual 3.3.13.22 Terrain Display Select #1 & #2 Discrete Terrain Display Select #1 & #2 discrete (J1-54 & J1-49) will activate after the related pilot has initiated manual selection of the Terrain Display Select (momentary) discrete #1 or #2 (J1-32 & J1-31, Category 6). This feature activates a ‘TERR” white lamp located in the cockpit within sight of each pilot. The lamp serves to remind the flight crew that this function is active.
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Honeywell MK XXII EGPWS Installation Manual Table 0-1 MKXXII EGPWS – Example Cockpit Lights CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 103
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Honeywell MK XXII EGPWS Installation Manual 3.3.14 Category 14 – Audio Output Level Category 14 controls the Audio Output level for alert menu callouts (cautions and warnings). Refer to Category 13 for information on the Mode 6 Low Volume discrete. Appendix E Table E 3.1.14 defines the Audio Output Level options and identifies the first MK VI/VIII EGPWS version in which the option was available (see the Effectivity entry). 3.3.14.1 Instructions 1. Using Appendix E Tables E 3 and E 3.1.
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Honeywell MK XXII EGPWS Installation Manual 3.3.15 Category 15, Autorotation Threshold Category 15 controls the Autorotation Threshold level used for Autorotation detection. Actual thresholds are determined during first of type flight. The thresholds are found in Table 3.1.15-1-1 below. Appendix E Table E 3.1.15 defines the Autorotation threshold options. 3.3.15.1 Instruction 1. Using Table 3.1.15-1-1 below and Appendix E Tables E 3 and E 3.1.
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Honeywell MK XXII EGPWS Installation Manual AUTOROTATION THRESHOLD Aircraft Type ID Aircraft Model Threshold % Threshold ID 128 S-76 B/C+ 7.5 15 129 S-76C/A++ 7.5 15 130 S-76A/A+ 7.5 15 131 Bell 212 6 12 131 Bell 412 6 12 132 EC-155B 7.5 15 133 MD900 7.5 15 133 MD902 7.5 15 AS 365N3 7.5 15 6 12 134 135 136 137 138 139 140 141 Bell 412, DC Torque 142 143 144 145 Table 3.1.
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Honeywell MK XXII EGPWS Installation Manual SECTION IV CONFIGURATION MODULE PROGRAMMING AND REGIONAL TERRAIN DATABASE LOADING CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C 107 SHEET
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Honeywell MK XXII EGPWS Installation Manual SECTION IV – CONFIGURATION MODULE PROGRAMMING AND REGIONAL TERRAIN DATABASE LOADING SECTION IV – CONFIGURATION MODULE PROGRAMMING AND REGIONAL TERRAIN DATABASE LOADING .................................................................................................................109 4.1 INTRODUCTION .................................................................................................................................. 109 4.
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Honeywell MK XXII EGPWS Installation Manual SECTION IV – CONFIGURATION MODULE PROGRAMMING AND REGIONAL TERRAIN DATABASE LOADING 4.1 Introduction The following procedures outline the steps necessary to accomplish a complete configuration of the MK XXII EGPWS. This section must be accomplished in the order presented to minimize errors in configuring and operating the system(s).
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Honeywell MK XXII EGPWS Installation Manual parameters, for testing purposes, without altering its operation. The monitoring of these parameter values enables the operator to quickly determine if the EGPWC is using the correct signal and scaling. The communication link utilizes the RS-232 communication protocol configured as follows: 19200 Baud, No Parity, 8 Bits, and 1 Stop Bit 4.4.
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Honeywell MK XXII EGPWS Installation Manual To obtain a copy of the WinVIEWS software, contact: Honeywell or Aerospace Electronic Systems Honeywell Aerospace Electronic Systems PO Box 97001 PO Box 97001 Redmond, WA 98073-9701 USA Redmond, WA 98073-9701 USA Attn: Order Administration M/S 33 Attn: EGPWS Applications Engineering Phone: (425) 885-8719 Phone: (425) 885-3711 FAX: FAX: (425) 885-8988 (425) 885-2994 GPWS Hotline: (800) 813-2099 WinVIEWS can be sent via e-mail when an e-mail address
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Honeywell MK XXII EGPWS Installation Manual - CUW0 is the command and version number. CUW writes the category ID’s defined by version 0 definition (0 is the only version currently available) to the Configuration Module via the EGPWC without a CRC (checksum) value attached (this is generated by the EGPWC when the data is transmitted). - /15 indicates the beginning of the data string (/) with 15 being the number of categories to follow.
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Honeywell MK XXII EGPWS Installation Manual Configuration Module and listed on the PC screen. Alternately, when not in the Configuration sub-mode, the command “PS” (Present Status) will display EGPWC and configuration data. 7. Configuration Module programming is complete. If the “CFG >” prompt is still present type “Exit” to exit the Configuration sub-mode. 4.5.1 CUW and CMR Comm ands An example CUW command/data string, its definition, and the corresponding CWR list is provided below.
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Honeywell MK XXII EGPWS Installation Manual Category 7 ID: Category 8 ID: Category 9 ID: Category 10 ID: Category 11 ID: Category 12 ID: Category 13 ID: Category 14 ID: Category 15 ID: CRC: 29 1 0 2 0 0 129 0 15 527518533 4.5.2 Configuration Module Reprogramming Reprogramming the EGPWS Configuration Module is accomplished similar to the programming process above.
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Honeywell MK XXII EGPWS Installation Manual associated ID is read from the Configuration Module and listed on the PC display. Alternately, when not in the Configuration sub-mode, the command “PS” (Present Status) will display the EGPWC and Configuration Module data. 7. Configuration Module reprogramming is complete. 4.6 Regional Terrain Data base Loading 4.6.1 Effectivity The MK XXII EGPWS (965-1590-0XX) are shipped from the factory with the North American Regional Terrain Database installed.
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Honeywell MK XXII EGPWS Installation Manual 4.6.4 Material – Cost and Av ailability The Regional Terrain Database PCMCIA card is available at no charge to Operators that will be operating outside of the North America region.
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Honeywell MK XXII EGPWS Installation Manual 4.6.5 Accomplishment Instr uctions Load the PCMCIA card data as described in paragraphs 4.6.5 A. or 4.6.5 B. below. Loading time will be approximately 70 minutes. A. Loading the PCMCIA Card Data with the Computer mounted in the Aircraft. (1) Connect the Smart Cable (Honeywell PN 951-0386-001) to the EGPWC J3 connector. (2) Ensure that the 28 VDC circuit breaker to the EGPWC is ON and that the COMPUTER OK LED on the EGPWC front panel is on.
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Honeywell MK XXII EGPWS Installation Manual (3) Connect the Smart Cable (Honeywell PN 951-0386-001) to the EGPWC J3 connector. (4) Turn the Power Supply ON and verify the COMPUTER OK LED on front of the EGPWC panel is on. (5) Insert the PCMCIA card into the Smart Cable PCMCIA card slot. NOTE: Precautionary notes on the PCMCIA card, regarding insertion and/or removal while power is applied, should be ignored since the EGPWC automatically handles the application and removal of PCMCIA card power.
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Honeywell MK XXII EGPWS Installation Manual to continue from level-to-level, the ST button must also be ‘pressed and held’ for more than 0.5 seconds, but less than 2 seconds, which is identical to the Short Cancel function. Therefore, for simplicity, the phrase “Press ST Button” in the verification procedure means to press and hold the ST button for more than 0.5 seconds, but less than 2 seconds.
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C 120 SHEET
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Honeywell MK XXII EGPWS Installation Manual SECTION V CERTIFICATION CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 121
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 122
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Honeywell MK XXII EGPWS Installation Manual SECTION V – CERTIFICATION 124 5.1 INTRODUCTION ................................................................................................................................. 124 5.2 CERTIFICATION PROCEDURE ............................................................................................................. 124 5.2.2 Equipment Location ..................................................................................................................
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Honeywell MK XXII EGPWS Installation Manual SECTION V – CERTIFICATION 5.1 Introduction This section outlines the procedures required to obtain FAA approval for the MK XXII EGPWS installation. 5.2 Certification Procedur e 5.2.1.1 Equipment Compatibi lity Careful consideration must be paid to the electrical characteristics of existing equipment or possible additions that will be interfaced to the MK XXII EGPWS, in order to ensure system compatibility.
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Honeywell MK XXII EGPWS Installation Manual 5.2.6 Flight Test Honeywell has developed a generic Flight Test procedure for the MK XXII EGPWS, drawing number 060-4314-006. The Flight Test procedure was developed for first of type installations, for these installations all sections of the Flight Test procedure shall be performed. For follow on installations of the same aircraft type and interface, the flight test is not required.
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 126
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Honeywell MK XXII EGPWS Installation Manual APPENDIX A CUSTOMER WORKSHEET CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 127
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 127
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Phone: N# Engine Type (model number): Installer: Contact: Notes: Other (specify) Weather Radar Controller Weather Radar R/T Weather Radar Indicator QTY SCALE: NONE MANUFACTURER CAGE CODE: 97896 Multifunction Display (MFD) EFIS Display Control Panel EFIS Display EFIS Symbol Generator SYSTEM SIZE: A DWG NO: 060-4314-225 MODEL NO. REV: C PART NO.
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MFGR. CAGE CODE: 97896 MSL MODEL NO. * GPS Altitude Reference: WGS-84 Engine Torque DG Radio Altimeters ILS Receivers AHRS / IRU / INU VG GPS * Air Data Computers SYSTEM output data information for: SCALE: NONE PART NO. SIZE: A QTY OUTPUT DATA FORMAT – NOTES REV: C SHEET 129 (ARINC 429, 547, 552, 575, DC, synchro, potentiometer, discrete, etc. Identify available ARINC 429 labels) Use “N/A” if Not Applicable DWG NO: 060-4314-225 S/W PART NO.
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GND > ° < ° OPEN +28 VDC > ° < ° barometric altitude, corrected baro altitude, baro rate, computed airspeed, static air temperature or total air ADC Range Display CAGE CODE: 97896 Torque Engine 1 and 2 or FADEC SCALE: NONE SIZE: A DWG NO: 060-4314-225 SHEET 130 altitude, latitude, longitude, ground speed, true track, true heading, mag variation, Nav mode, horizontal figure of FMS / GPS REV: C glideslope deviation / flag , localizer deviation / flag ILS / NAV receiver merit, horizontal int
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CAGE CODE: 97896 Main Rotor RPM Rotational Frequencies: SCALE: NONE SIZE: A Distance from tail rotor blade (lowest point) to ground Distance from lowest point of tail or tail-skid to ground Distance from CG to center of Tail Rotor Distance from CG to Tail (Lowest point of tail or skid) Height of Nominal CG above ground Aircraft Tail Geometry: (be specific) Model: Manufacturer: GENERIC MODEL INFORMATION ENHANCED GROUND PROXIMITY WARNING SYSTEM MK XXII EGPWS DWG NO: 060-4314-225 No.
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Torque Engine SYSTEM SCALE: NONE SIZE: A DWG NO: 060-4314-225 In % Torque (ARINC 429, RS 422, RS 232, synchro, DC, AC Signal Scale Factor DATA FORMAT CAGE CODE: 97896 Number of Engines ENHANCED GROUND PROXIMITY WARNING SYSTEM MK XXII EGPWS REV: C SHEET 132 NOTES
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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 133
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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 134
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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 135
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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 136
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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 137
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Honeywell MK XXII EGPWS Installation Manual APPENDIX B SAMPLE WIRING DIAGRAMS CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 139
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV:C SHEET 140
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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV:C SHEET 141 Honeywell MK XXII EGPWS Installation Manual
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CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV:C SHEET 142 Honeywell MK XXII EGPWS Installation Manual
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Honeywell MK XXII EGPWS Installation Manual APPENDIX C WinViews OPERATION INSTRUCTIONS CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 143
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 144
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Honeywell MK XXII Installation Manual 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.
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Honeywell MK XXII Installation Manual 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.
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Honeywell MK XXII Installation Manual Command File: MK XXII_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.
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Honeywell MK XXII Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 148
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Honeywell MK XXII EGPWS Installation Manual APPENDIX D VENDOR DRAWINGS CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 149
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 150
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Honeywell MK XXII EGPWS Installation Manual D 1-0 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 Barry Controls Burbank, CA 818 843-1000 United Kingdom: Surrey, England 44 (0932) 22-4122 Brighton, MA 616 787-1555 Germany: Raunheim, Germany 49 (6142) 43077/8/9 EDMO 5505 E. Rutter Ave. Spokane, WA 99212 www.edmo.
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Honeywell MK XXII EGPWS Installation Manual Korry Electronics 901 Dexter Avenue North Seattle, WA Attention: Airline Sales 206 281-1300 800 257- 8921 For orders and AOG requirements, contact: Sonya Cordova 206 281-3567 email: scordova@korry.com fax: 206 281-3576 SITA: SEAKEXD For engineering inquiries, contact: Tom Howard Bob Jacques Airline Business Manager Airline Business Manager 206 281-1458 206 281-3584 email: thoward@korry.com email: bjacques@korry.
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Honeywell MK XXII EGPWS Installation Manual D1-1 EDMO EDMO Distributors (800)235-3300 – “One Stop Shopping” for the following EGPWS and TAWS support products: * MD41-12XX/13XX TAWS ACU’s from Mid-Continent Instruments * 90-44802-1 PMA’d TAWS ACU from West Coast Specialties * Eaton and StacoSwitch EGPWS split switch & annunciator kits * Shadin XYZ compass to RS-232/422 Converters * Shadin low cost Airdata computers * Solid State Altitude Encoders (most models) * GAE-1575 GPS Repeater for hangar testing *
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Honeywell MK XXII EGPWS Installation Manual D1-2 EMTEQ EMTEQ, Inc. supports all EGPWS/TAWS systems manufactured by Honeywell, Inc. by offering products to help complete your installation. The installation provisions are fully compliant with ARINC specifications and standards. We have a full understanding of the system requirements for coaxial components, wire harnesses, Switchpanels and mounting accessories.
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Honeywell MK XXII EGPWS Installation Manual TABLE 1 Table 1.A. (Teflon ® Jacketed RF Coax) (High Temp) Cable Type O.D. Bend Radius Per 100 ft (inches) Minimum TFLX130-100 21.60 dB 0.130 “ ½” TFLX165-100 17.00 dB 0.161” 1 ¾” TFLX205-100 13.90 dB 0.195 “ 1 ¾” TFLX295-100 7.60 dB 0.205 “ 3.0 “ TFLX480-100 4.75 dB 0.480 “ 2.40 “ P/N Loss @ 1600 Mhz Table 1.B. (PE – Polyethylene Jacketed RF Coax) (85 C temp) Cable Type O.D.
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Honeywell MK XXII EGPWS Installation Manual TABLE 2 Table 2.A.
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Honeywell MK XXII EGPWS Installation Manual TABLE 2 (continued) Table 2.B.
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Honeywell MK XXII EGPWS Installation Manual Tool Frame and Die Part Numbers Mil-Spec P/N Daniels Cable Type for Hex Die P/N for Hex Die Tool Frame Die Hex PFLX195 M22520/5-19 Y142 M22520/5-01 (HX4) B Hex PFLX200 M22520/5-19 Y142 M22520/5-01 (HX4) B Hex PFLX240 M22520/5-43 Y141 M22520/5-01 (HX4) A Hex PFLX340 M22520/5-35 Y137 M22520/5-01 (HX4) A Hex PFLX500 M22520/5-21 Y149 M22520/5-01 (HX4) A Hex TFLX130 M22520/5-43 Y141 M22520/5-01 (HX4) A (ARINC) / B Hex TFLX165 M225
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Honeywell MK XXII EGPWS Installation Manual Installation Considerations: Meeting the specifications when faced with a long cable run could be challenging at some times. Solutions typically are found when combining a Low Loss Cable (large OD) for the majority of the run with a “pig tail” at the box or antenna sides. The “pig tail” cable will have a small OD, and will be very flexible to make the installation in difficult areas easier. Please use the Tables above for additional information.
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Honeywell MK XXII EGPWS Installation Manual D1-3 Aerospace Optics Aerospace Optics Inc. Aerospace Optics Inc. is pleased to support the Honeywell EGPWS/TAWS team with our line of Vivisun LED lighted switches and indicators. We would welcome the opportunity to assist with your installation and address your Honeywell EGPWS/TAWS lighting requirements. LED Lighting The Honeywell EGPWS/TAWS systems offer state-of-the-art performance.
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Honeywell MK XXII EGPWS Installation Manual Please feel free to contact the Aerospace Optics Technical Sales Team for assistance in addressing the use of LED lighted switches and indicators. Aerospace Optics Inc. 3201 Sandy Lane Fort Worth TX, 76016 1-(888)VIVISUN- (848-4786) Toll Free Fax (817) 654-3405 www.vivisun.com e-mail : switches@vivisun.
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Honeywell MK XXII EGPWS Installation Manual D1-4 StacoSwitch StacoSwitch As a supplier of high reliability switches and indicators for avionics since 1958, StacoSwitch is proud to be integrated with many Honeywell products and divisions. Through our relationship with EDMO Distributors in Spokane, WA, we supply AV17 kits that include all the switches, annunciators, and crimp pins needed to complete the installation of your Honeywell EGPWS (TAWS) system.
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Honeywell MK XXII EGPWS Installation Manual APPENDIX E INTERFACE DESCRIPTION DOCUMENT CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 163
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Honeywell MK XXII EGPWS Installation Manual CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 164
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Honeywell MK XXII EGPWS Installation Manual INTRODUCTION ...................................................................................................................................................................166 E1 Part Number .............................................................................................................................................................166 E2 Purpose.....................................................................................................
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Honeywell MK XXII EGPWS Installation Manual INTRODUCTION E1 PART NUMBER This document is the Interface Description for the MKXXII Helicopter Enhanced Ground Proximity Warning System (EGPWS) part number 965-1590-0XX.
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Honeywell MK XXII EGPWS Installation Manual E4 ELECTRICAL INTERFACE E 4.1 INTRODUCTION The MK XXII EGPWS provides 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 965-1590-0XX MK XXII EGPWC.
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Honeywell MK XXII EGPWS Installation Manual 3 Note that this is not a floating input. +28 VDC must be applied to both PWR_H and +28 VDC Return to both PWR_L inputs. E 4.2.3 DC ANALOG INPUTS Unless otherwise specified, Input Signal accuracy is1% linearity +0.1% full scale offset. E 4.2.3.
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Honeywell MK XXII EGPWS Installation Manual When used as a validity input: Active Voltage Range (Logic True) Inactive Voltage Range (Logic False) Broken Wire Detect +160 to +840 mVDC 0 to 50 mVDC Input will be biased less than –1 VDC When used as a localizer input: Signal Range Input Voltage Range Broken Wire Detect ±12 Dots ±0.9VDC Input will be biased less than -15 dots E 4.2.
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Honeywell MK XXII EGPWS Installation Manual E 4.2.7 AC ANALOG INPUTS Unless otherwise specified, Input Signal accuracy is1% linearity +0.1% full scale offset E 4.2.7.1 SYNCHRO ROLL ATTITUDE Quantity Input Impedance: X leg Input Impedance: Y leg Input Impedance: Z leg Maximum Reverse Fault Current Input Voltage Range Synchro Angle Range Reference Voltages Accuracy Pin Assignment (Signal Mnemonic): X leg Y leg Z leg E 4.2.7.2 1 > 140 KΩ > 140 KΩ > 140 KΩ < 200 µamps ±11.
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Honeywell MK XXII EGPWS Installation Manual E 4.2.7.3 CONFIGURATION DEFINED SYNCHRO INPUTS Quantity Input Impedance: X leg Input Impedance: Y leg Input Impedance: Z leg Maximum Reverse Fault Current Input Voltage Range Reference Voltages Accuracy Pin Assignment (Signal Mnemonic): #1 X leg #1 Y leg #1 Z leg #2 X leg #2 Y leg #2 Z leg #3 X leg #3 Y leg #3 Z leg E 4.2.8 3 > 140 KΩ > 140 KΩ > 140 KΩ < 200 µamps ±11.8 VACRMS ± 20% (leg to leg) ±26 VACRMS ± 20% 2.5% linearity + 0.
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Honeywell MK XXII EGPWS Installation Manual E 4.2.9 ARINC 429/575 DIGITAL SERIAL BUS INPUTS Quantity Format Low Speed Data Rate High Speed Data Rate Direction of Information Flow Word/Frame Structure 8 DITS, ARINC 429/575 Low or high speed 1 12.0 KBPS to 14.
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Honeywell MK XXII EGPWS Installation Manual E 4.2.9.1 RS-232 / RS-422 DIGITAL SERIAL BUS INPUTS Two full duplex RS-232 / RS-422 buses and a third RS-422 receiver are provided at the aircraft interface connectors. The RS-422 transceivers are electrically multiplexed with the RS-232 transceivers, and are selected through the configuration process. The third RS-422 receiver is electrically multiplexed with the ARINC 429 channel 1 receiver. The maintenance RS-232 bus is described in section 0.
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Honeywell MK XXII EGPWS Installation Manual E 4.2.9.4 AIR DATA RS-232 DIGITAL SERIAL BUS (SERIAL PORT 2) One port is provided for use with Air Data computer or Static Pressure Sensor interfaces. This port is common with the Air Data RS-422 port described in Section 0 and can only function as a RS-232 interface or a RS-422 interface but not both. Pin Assignment (Signal Mnemonic): Transmit Receive Common E 4.2.9.
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Honeywell MK XXII EGPWS Installation Manual The Ground discretes are internally biased via a pull up resistor, and are externally pulled down to ground when active. The characteristics of each Ground discrete input are as follows: Ground Discrete Characteristics Quantity Active Voltage Range (Logic True) Inactive Voltage Range (Logic False) Diode Isolation Input Impedance Maximum Fault Current Pin Assignment (Signal Mnemonic): E 4.2.11 15 < +3 VDC > 100 KΩ (to ground) or > +3.
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Honeywell MK XXII EGPWS Installation Manual E 4.2.13 OAT VOLTAGE REFERENCE OUTPUT This output is an accurate voltage source for 500 Ω resistive temperature sensors. Quantity Output Voltage Nominal Load Pin Assignment (Signal Mnemonic): 1 5.000 VDC ±10 mVDC (no load) 500 Ω J1-25 (OAT_REF) NOTE: This output has a source impedance of 4.42 KΩ, 0.1%. E 4.2.
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Honeywell MK XXII EGPWS Installation Manual • If a ‘soft’ Glideslope alert is being issued (given 6 dB below nominal alert volume level). • If a Self Test is in progress, alerts are given 6 dB below nominal alert volume level. • Selection of Mode 6 Low Volume Discrete (lowers callout volume by 6 dB - See Section 5.3.13). E 4.2.16.1 HIGH LEVEL (SPEAKER) AUDIO OUTPUT The 8-ohm output is capable of driving a speaker directly but can also be used to drive other devices with equal or higher impedance.
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Honeywell MK XXII EGPWS Installation Manual E 4.2.17.2 ARINC 453 OUTPUT BUS Quantity Format Data Rate Word/Frame Structure Data definition 2 1600 bit Manchester BI-phase per ARINC 708A 1 Mb per second Refer to Section 7.2 Refer to Section 7.2 Pin Assignment (Signal Mnemonic): Bus #1 (A leg) Bus #1 (B leg) Bus #2 (A leg) Bus #2 (B leg) J1-58 J1-59 J1-56 J1-57 E 4.2.
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Honeywell MK XXII EGPWS Installation Manual E 4.2.18.2 PCMCIA / SMARTCABLE PORT One port is provided which meets the Motorola SPI characteristics. The PCMCIA / SmartCable interface allows for both the uploading, and downloading of internal MK IV, VI, VIII and XXII EGPWS information. Using this interface system, software and databases can be updated.
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Honeywell MK XXII EGPWS Installation Manual E5 AIRCRAFT APPLICATION DATA This section describes the MK XXII EGPWS interfaces for aircraft applications. Section E 5.1 is a listing of the selection categories defining the various aircraft sensor interfaces and EGPWS functional options. Section E 5.2 describes how the Category ID’s are selected and programmed for the interface to aircraft sensors and EGPWS functional options. Section E 5.
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Honeywell MK XXII EGPWS Installation Manual TABLE E 3 CATEGORY ID SELECTION PROCEDURE Signal Selection Step (Category) Selects: 1 a) Aircraft Type b) Mode Type Selects: 2 a) Air Data Source Selects: 3 a) Position Source Selects: 4 a) Altitude Callouts Menu Selects: 5 a) Audio Menu Selects: 6 a) Display Config.
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Honeywell MK XXII EGPWS Installation Manual Signal Selection Step (Category) Selects: 9 a) Glideslope and/or Localizer Source Selects: 10 a) Attitude Source Selects: 11 a) Magnetic Heading Source Selects: 12 Selects: a) 13 b) Input Discrete Functions a) Audio Output Level Selects: 15 a) Using Table 5.3.9, and any sub-tables contained within, locate the desired Navigation signal type. Ident No. Record the Ident (ID No.) on the space available on Ident column of this table.
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Honeywell MK XXII EGPWS Installation Manual E 5.3.1 CATEGORY 1, AIRCRAFT / MODE TYPE SELECT Category 1 defines the Aircraft Type. This determines the warning modes algorthm configuration, gear type and Torque Interface characteristics. The following table provides ID values for each of the basic helicopter type descriptions. For purposes of selecting an ID, use the “Description” provided in Table E 3.1.1 appropriate to the desired variables as given above. Refer to the identified Table E .3.1.
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Honeywell MK XXII EGPWS Installation Manual TABLE E 3.1.1: HELICOPTER TYPE ID AND TORQUE INPUTS FOR EGPWS MK XXII ID 128 129 130 131 132 133 134 135 136 137 138 139 Reserved 141 142 Reserved Reserved 145 Torque Type Table (E 3.1.1-x) 0 1 2 3 4 5 6 7 8 9 10 5 DESCRIPTION Effectivity App. Cfg.
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Honeywell MK XXII EGPWS Installation Manual E 5.3.1.2 ENGINE TORQUE DATA SELECTION WHEN A SINGLE ENGINE HELICOPTER IS ADDED TO THIS SECTION, IT NEEDS TO BE TREATED AS IF THERE WERE TWO ENGINES VIA AIRCRAFT WIRING. THE SRD REQURIEMENTS ARE ALL WRITTEN FOR TWO ENGINES, BUT SINGLE ENGINES WERE ACCOUNTED FOR AS LONG AS THIS METHOD IS USED. TABLE E 3.1.
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Honeywell MK XXII EGPWS Installation Manual TABLE E 3.1.1-4 TORQUE DATA SELECT 4 (EC-155B, AS-365N3) CHANNEL RX429-8 CONNECT TO: Eng #1 (high speed) Fault Designation: ENGINE 1 BUS Bus Type: Basic A = J2-24 B = J2-07 CHANNEL RX429-5 (Note 1) A = J2-21 B = J2-04 Data Torque CONNECT TO: Eng #2 (high speed) Label 053 Data Torque Label 053 Sig. Bits 15 Range 0 to 180% Signal Type Basic Resolution 0. 0078125 Rate (ms) 20 Resolution 0. 0078125 Rate (ms) 20 Resolution 0.
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Honeywell MK XXII EGPWS Installation Manual TABLE E 3.1.1-8 TORQUE DATA SELECT 8 (AS365 DAUPHIN N3) CHANNEL RX429-8 CONNECT TO: Eng #1 (low speed) Fault Designation: ENGINE 1 BUS Bus Type: Basic A = J2-24 B = J2-07 CHANNEL RX429-5 (Note 1) A = J2-21 B = J2-04 Data Torque CONNECT TO: Eng #2 (low speed) Label 211 Data Torque Label 211 Sig. Bits 15 Range 799% Signal Type Basic Resolution 0.1 Rate (ms) 100 Resolution 0.1 Rate (ms) 100 Resolution 0.1 Rate (ms) 100 Resolution 0.
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Honeywell MK XXII EGPWS Installation Manual SIGNAL Engine Torque #1 CONNECTION (+) = J1-26 (-) = J1-27 Engine Torque #2 (+) = J1-66 (-) = J1-47 TABLE E 3.1.1-12 TORQUE DATA SELECT 14 (COAST GUARD HH-65) SUMMARY DATA Format: DC Input Type: Basic Fault Designation: ENGINE TORQUE 1 Validity: none Format: DC Input Type: Basic Fault Designation: ENGINE TORQUE 2 Validity: none SIGNAL Engine Torque #1 Engine Torque #2 TABLE E3.1.
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Honeywell MK XXII EGPWS Installation Manual E 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 E 3.1.2.
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Honeywell MK XXII EGPWS Installation Manual TABLE E 3.1.
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Honeywell MK XXII EGPWS Installation Manual TABLE E 3.1.2-3: AIR DATA INPUT SELECT #3 CONNECTION SUMMARY DATA (+) = J1-62 (-) = J1-43 Format: DC with Validity Flag Input Type: Basic Fault Designation: BAROMETRIC ALTITUDE FAULT Validity: Barometric Alt Valid (+28V) Format: DC Input Type: Basic Fault Designation: STATIC AIR TEMPERATURE FAULT Outside Air Temp Total Air Temperature 5 V = J1-25 Temp Input (probe element): (+) = J1-63 (-) = J1-44 Ground GND = J1-53 J1 25 (5 V Ref) 4.
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Honeywell MK XXII EGPWS Installation Manual TABLE E 3.1.
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Honeywell MK XXII EGPWS Installation Manual TABLE E 3.1.2-6: AIR DATA INPUT SELECT #6 CHANNEL 429RX_2 A = J2-39 B = J2-38 CONNECT TO: ADC #1 (Low Speed) Format: ARINC 429 Data Uncorrected. Baro. Alt Computed Airspeed Static Air Temperature Fault Designation: AIR DATA BUS Bus Type: Basic Label 203 206 213 Configuration Data Derive Baro Altitude Rate Sig. Bits 17 14 11 Range ±131,072 FT ±1024 KTS ±512 Degrees Signal Type Basic Basic Basic Type Resolution 1.0 0.0625 0.25 Rate (ms) 31.3-62.5 62.
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Honeywell MK XXII EGPWS Installation Manual TABLE E 3.1.2-11: AIR DATA INPUT SELECT #11 CONNECTION SUMMARY DATA (+) = J1-62 (-) = J1-43 Format: DC with Validity Flag Input Type: Basic Fault Designation: BAROMETRIC ALTITUDE FAULT Validity: Barometric Alt Valid (+28V) Format: DC Input Type: Basic Fault Designation: STATIC AIR TEMPERATURE FAULT Outside Air Temp Total Air Temperature 5 V = J1-25 Temp Input (probe element): (+) = J1-63 (-) = J1-44 Ground GND = J1-53 J1 25 (5 V Ref) 4.
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Honeywell MK XXII EGPWS Installation Manual TABLE E 3.1.2-12: AIR DATA INPUT SELECT #12 SIGNAL CONNECTION Uncorrected Barometric Altitude (+) = J1-62 (-) = J1-43 Outside Air Temp No Connection Computed Airspeed No Connection PIN FUNCTION Barometric Altitude Validity Discrete (+28V) CONNECTION J1-9 SUMMARY DATA Format: DC with Validity Flag Input Type: Basic Fault Designation: BAROMETRIC ALTITUDE FAULT Validity: Barometric Alt Valid (+28V) Format: Internal Constant 250C and Valid.
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Honeywell MK XXII EGPWS Installation Manual MSL type. The Universal GPS1000 based GPS sources are of WGS-84 type. If the internal GPS source (ID=2) is defined, the GPS altitude reference in Category 7 must be MSL. Note 2: Universal GPS 1000 does not calculate VFOM and HFOM correctly which makes it an unacceptble position source for helicopters. CHANNEL 429RX_4 A = J2-25 B = J2-8 TABLE E 3.1.
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Honeywell MK XXII EGPWS Installation Manual CHANNEL GPS_RXA GPS_TXA Internal TABLE E 3.1.3-2: POSITION INPUT TYPE 2 (INTERNAL RS-232 GPS) Internal GPS Fault Designation: INTERNAL GPS [XPGPS_Int] = 1 Bus Type: Basic (9600 baud) Data ID/byte Sig.
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Honeywell MK XXII EGPWS Installation Manual CHANNEL 429RX_4 A = J2-25 B = J2-8 TABLE E 3.1.3-5: POSITION INPUT TYPE 5 (HIGH SPEED ARINC 743 GPS) CONNECT TO: Fault Designation: GPS BUS GPS (High Speed) Bus Type: Basic per ARINC 743 Data Label Sig. Bits Range Signal Type Latitude - Normal 110 20 ±180 Degrees Basic Longitude - Normal 111 20 ±180 Degrees Basic GPS Hor. Int.
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Honeywell MK XXII EGPWS Installation Manual E 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 consists of standard callout options and Autorotation Mode reversion callout options. ID’s 0 through 127 consist of standard callouts while ID’s 128 through 255 include standard callouts and reversion to a set of Autorotation callouts.
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Honeywell MK XXII EGPWS Installation Manual Note: Selecting an Altitude Callout ID without a minimums callout can be accomplished by leaving the Decision Height input discrete open or connected to +28VDC.
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Honeywell MK XXII EGPWS Installation Manual E 5.3.5 CATEGORY 5, AUDIO MENU SELECT The following table provides identification of the Voice Menu type. Each entry in the Voice Menu column has a corresponding table that provides detailed information on the configuration. For example, the details for Voice Menu # are found in Table E 3.1.5-128. TABLE E 3.1.5: AUDIO MENU TYPE ID Audio Menu Type Description Effectivity App Cfg. . -006 -006 (Table E 3.1.5.-x) 128 128 Basic Helicopter Menu TABLE E 3.1.
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Honeywell MK XXII EGPWS Installation Manual E 5.3.6 CATEGORY 6, TERRAIN DISPLAY SELECT Section Overview 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.
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Honeywell MK XXII EGPWS Installation Manual for information describing the requirements to interface an EGPWS to the Collins Pro Line II system equipped with EFIS 84/85/86 Displays and WXR-350/840/700 or TWR-850 Weather Radar systems. Note 4: This interface only supports the SG-810 and SG-811 SPZ-8000. This display is defined for the –001 & -003 releases but can cause periodic resets of the EGPWS due to an internal SCI range problem. The –001 & -003 release should not be used for this display.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Table Table E 3.1.6-1 No Display – TAD and TCF Enabled OUTPUT 429 BUS GROUP 0 Channel 429TX_1 (Low Speed) 429TX_2 Pins A = J2-43 B = J2-42 A = J2-26 B = J2-9 Comments Transmits (Section 7) Label sets: 7.1.1.x, 7.1.2.x, 7.1.3.x and 7.1.4.x No Connection (No Data Output) Table Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Table Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Table Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual • When interfacing to a single display controller configuration the bus must be connected to both EGPWS input channels. This prevents the EGPWS from reporting an external bus fault on the second channel.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.6-13 Integrated Honeywell P880/660/440 (WXPD w/ SCI range) Display Configuration Group 11 (Honeywell Integrated P880/660/440).
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Output 429 Bus Group 0 Channel Pins Comments 429TX_1 (Low Speed) A = J2-43 B = J2-42 Transmits (Section 7) Label sets: 7.1.1.x, 7.1.2.x, 7.1.3.x, 7.1.4.x, and 7.1.6.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Display Input Control Group 2 CHANNEL 429_422RX_1 CONN PIN # J1-32 CONNECT TO: WX-IND 429 out (range) Bus 1 (Low Speed) Data Mode (Display Word 1) Range (Display Word 2) Discrete Word (VP) CONNECT TO: WX-IND 429 out (range) Bus 2 (Low Speed) Data Mode (Display Word 1) Range (Display Word 2) Discrete Word (VP) REFERENCE NAME GND_DISC_12 J1-31 GND_DISC_13 A = J2-37 B = J2-36 CHANNEL 429RX_3 A = J2-41 B = J2-40 * Fault Designation: DISPLAY BUS 1 Bus Type: Ba
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Output 429 Bus Group 0 Channel Pins Comments 429TX_1 (Low Speed) A = J2-43 B = J2-42 Transmits (Section 7) Label sets: 7.1.1.x, 7.1.2.x, 7.1.3.x, 7.1.4.x, and 7.1.6.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Table E3.1.
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Honeywell MK XXII EGPWS Installation Manual Output 429 Bus Group Channel Pins Comments 429TX_1 (Low Speed) A = J2-43 B = J2-42 Transmits (Section 7) Label sets: 7.1.1.x, 7.1.2.x, 7.1.3.x, 7.1.4.x, and 7.1.6.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual • • • • • • • 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. The display will energize the Terrain selection relays. The display will annunciate “TERR”. The display will change to the range indicated by the EGPWS ARINC 429 Label 050.
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Honeywell MK XXII EGPWS Installation Manual Table E 3.1.
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Honeywell MK XXII EGPWS Installation Manual E 5.3.7 CATEGORY 7, OPTIONS 1 SELECT 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 / WOW Reversal and GPS Altitude Reference selection. Refer to section 7.5 for configuration messages that will be present for each option selected.
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Honeywell MK XXII EGPWS Installation Manual ID 34 35 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 TA&D Alternate Pop Up 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 CAGE CODE: 97896 Peaks Mode Enabled5 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 T
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Honeywell MK XXII EGPWS Installation Manual E 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 0-1. ARINC 552, ALT 55 and digital ARINC 429 compatible Radio Altimeters are supported.
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Honeywell MK XXII EGPWS Installation Manual TABLE E 3.1.8-1: RADIO ALTITUDE INPUT SELECT TYPE 1 (ALT 55) CONNECTION SUMMARY DATA (+) = J1-64 Format: Alt 55 with Validity Flag (-) = J1-45 Input Type: Basic Fault Designation: RADIO ALTIMETER FAULT Validity: Radio Altitude Valid Discrete #1 (+28V) PIN FUNCTION CONNECTION PIN TYPE CHANNEL DESIGNATION Polarity/Configuration REFERENCE Radio Altitude Validity J1-29 Input 28V_DISC_07 >+17V = Valid Discrete #1 (+28V) <+4.
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Honeywell MK XXII EGPWS Installation Manual TABLE E 3.1.8-4: RADIO ALTITUDE INPUT SELECT TYPE 4 (KRA 405) CONNECTION SUMMARY DATA (+) = J1-64 Format: Alt 55 with Validity Flag (-) = J1-45 Input Type: Basic Fault Designation: RADIO ALTIMETER FAULT Validity: Radio Altitude Valid Discrete #1 (+28V) PIN FUNCTION CONNECTION PIN TYPE CHANNEL DESIGNATION Polarity/Configuration REFERENCE Radio Altitude Validity J1-29 Input 28V_DISC_07 >+17V = Valid Discrete #1 (+28V) <+4.
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Honeywell MK XXII EGPWS Installation Manual E 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 0-1. In this category, only the following signals are defined: • • Glideslope source selection. Localizer source selection. (optional for digital only) TABLE E 3.1.
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Honeywell MK XXII EGPWS Installation Manual SIGNAL TABLE E 3.1.9-1: NAVIGATION INPUTS SELECT 1 SUMMARY DATA Format: ARINC 547 with Low Level Validity & ILS Select (+) = J1-65 Input Type: Basic (-) = J1-46 Fault Designation: GLIDESLOPE FAULT Validity: Low Level Glideslope Deviation Validity Format: DC Input Type: Basic (+) = J1-30 Fault Designation: GLIDESLOPE LOW LEVEL VALIDITY FAULT (-) = J1-10 > 0.145V = Valid (typical active range is 0.16V to 0.84V) <= 0.
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Honeywell MK XXII EGPWS Installation Manual E 5.3.10 CATEGORY 10, ATTITUDE INPUT SELECT The following table provides identification of the Roll Attitude 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 #1 are found in 0-1. In this category, only the following signals are defined: • • • • Roll Attitude Pitch Attitude TABLE E 3.1.
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Honeywell MK XXII EGPWS Installation Manual SIGNAL Roll Attitude PIN FUNCTION Attitude Validity Discrete #1 TABLE E 3.1.10-4: ATTITUDE INPUT SELECT TYPE 4 SUMMARY DATA Format: 3 Wire Synchro with Validity Flag (X) = J1-1 Input Type: Basic (Y) = J1-21 Fault Designation: ROLL FAULT Validity: Attitude Validity Discrete #1 (Z) = J1-2 Reference: None CHANNEL DESIGNATION Polarity/Configuration CONNECTION PIN TYPE REFERENCE J1-68 Input 28V_DISC_12 >+17V = Valid <+4.4V = Invalid CONNECTION Summary Data 6.6.
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Honeywell MK XXII EGPWS Installation Manual E 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 #1 are found in 0-1. In this category, only the following signals are defined: • Magnetic Heading TABLE E 3.1.
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Honeywell MK XXII EGPWS Installation Manual E 5.3.12 CATEGORY 12, WINDSHEAR INPUT SELECT The Windshear warning is not applicable to Helicopters. The following table provides the definition of Windshear Input Select ID 0, which is used for helicopter installations. ID Description 0 No Windshear CAGE CODE: 97896 TABLE E 3.1.12: WINDSHEAR INPUT SELECT Windshear INOP Disable Windshear Caution Voice Disable SCALE: NONE TRUE SIZE: A TRUE DWG NO: 060-4314-225 Effectivity App. Cfg.
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Honeywell MK XXII EGPWS Installation Manual E 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 #128 are found in Table E 3.1.13-128. TABLE E 3.1.
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Honeywell MK XXII EGPWS Installation Manual CONN PIN # J1-38 CHANNEL DESIGNATION REFERENCE 28V_DISC_02 J1-19 GND_DISC_02 J1-37 28V_DISC_03 J1-18 GND_DISC_03 J1-36 28V_DISC_04 J1-17 GND_DISC_04 TABLE E 3.1.13-128: INPUT/OUTPUT DISCRETE TYPE 128 PIN TYPE PIN FUNCTION Input Input Input Input Input Polarity/Configuration +28V Glideslope Inhibit Discrete >+17V = Inhibit <+4.4V = Not Inhibit Gnd = Inhibit Gnd = Not Inhibit >+17V = WOW <+4.
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Honeywell MK XXII EGPWS Installation Manual CONN PIN # J1-38 CHANNEL DESIGNATION REFERENCE 28V_DISC_02 J1-19 GND_DISC_02 J1-37 28V_DISC_03 J1-18 GND_DISC_03 J1-36 28V_DISC_04 J1-17 GND_DISC_04 TABLE E 3.1.13-129: INPUT/OUTPUT DISCRETE TYPE 129 PIN TYPE PIN FUNCTION Input Input Input Input Input Polarity/Configuration +28V Glideslope Inhibit Discrete >+17V = Inhibit <+4.4V = Not Inhibit Gnd = Inhibit Gnd = Not Inhibit >+17V = WOW <+4.
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Honeywell MK XXII EGPWS Installation Manual E 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 output is 4 Wrms for the 8-ohm output and 100 mWrms for the 600-ohm output. The Audio Output Level can be additionally reduced by 6dB with the Mode 6 Low Volume discrete (see Category 13).
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Honeywell MK XXII EGPWS Installation Manual E 5.3.15 CATEGORY 15, AUTOROTATION THRESHOLD The following table provides identification of the Autorotation Threshold. Each entry in the ID column corresponds to an engine torque threshold for autorotation. Each helicopter type has a unique engine torque percentage during autorotation based on the aerodynamic qualities of the aircraft. This value is not typically published or well known, thus it has been included as a configuration item in Table 10.3.15.
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Honeywell MK XXII EGPWS Installation Manual E6 CONNECTOR INTERFACE E 6.
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Honeywell MK XXII EGPWS Installation Manual Connector Pin J1-52 Channel Designation Reference Signal Usage Summary* 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 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 TORQUE_2H GND_DISC_14 28V_DISC_12 J1-70 J1-71 J1-72 J1-73 J1-74 J1-75 J1-76 J1-77 J1-78 AUD_HL_H AUD_HL_L MON_OUT_1 DISC_OUT_4 AUD_LL_L AUD_LL_H DISC_OUT_3 DISC_OUT_2 DISC_OUT_1 Spare Out
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Honeywell MK XXII EGPWS Installation Manual Connector Pin Channel Designation Reference Signal Usage Summary* J2-26 J2-27 J2-28 J2-29 J2-30 J2-31 J2-32 J2-33 J2-34 J2-35 429TX_2A 422_232TX_2A GND GPS_RXA EGPWS ARINC 429 Output #2 (A leg) ADC RS-232 / 422 Output (A leg) GPS / ADC RS-232 / 422 Common GPS RS-232 / 422 Input (A leg) GND_DISC_15 SPICLK SPIMISO 26REF_2H 26REF_2L J2-36 429_422RX_1 J2-37 429_422RX_1 J2-38 J2-39 J2-40 J2-41 J2-42 J2-43 J2-44 J2-45 J2-46 J2-47 J2-48 J2-49 J2-50 429RX_2B 4
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Honeywell MK XXII EGPWS Installation Manual Figure E 4, Front Panel Connector Orientation - J1, J2, J3, GPS ANT CAGE CODE: 97896 SCALE: NONE SIZE: A DWG NO: 060-4314-225 REV: C SHEET 250
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Honeywell MK XXII EGPWS Installation Manual Figure E 4.
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Honeywell MK XXII EGPWS Installation Manual E7 DEFINITIONS The following acronyms are provided for use with this document: Acronym AAAS ADC ADS AGL AHRS AIC AIMS AOA ASA ASL ATP BCD BIST BIT BITE BNR BOSS 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 CAGE CODE: 97896 Interpretation Alternate Audio Alert Select Air Data Computer Air Data System Above Ground Level Attitude Heading Reference
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Honeywell MK XXII EGPWS Installation Manual Acronym Interpretation F/T Functional Test F/W F/W FAA FCC FDR FIAS FMC FMS FPM FSEU FWC G/S GMT GPS GPW GPWS GT H/W HDG HDOP 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 MKXXII MLS MMU MSB N/A NCD ND NVM OMS P/N PAR Fail/Warning Fail/Warning Federal Aviation Administration Flight Control Computer Flight Data Recorder Flight Inspection Aircraft System Flight Management Computer Flight Management
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Honeywell MK XXII EGPWS Installation Manual Acronym PC PCMCIA PFD 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 VHF VLSI VOR W/S WC WX CAGE CODE: 97896 Interpretation Personal Computer Personal Computer Memory Card Industry Association Primary Flight Display Portable Maintanence Access Terminal Program Pin Processor/Voice/Memory Predictive Windshear System Corrected Baro Alt relative