Honeywell KMH 880 User manual

SYSTEM INSTALLATION
MANUAL
KMH 880/KTA 870
MULTI-HAZARD AWARENESS
TRAFFIC ADVISORY SYSTEM
MANUAL NUMBER 006-10609-0003
REVISION 3 AUGUST, 2002

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SYSTEM INSTALLATION
MANUAL
KMH 880/KTA 870
MULTI-HAZARD AWARENESS
TRAFFIC ADVISORY SYSTEM

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COPYRIGHT NOTICE
©2001/2002 Honeywell International Inc.
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BKMH880/KTA 870
Rev 3, August/2002 10609I03.CDL Page R- 1
REVISION HISTORY AND INSTRUCTIONS
MANUAL KMH 880/KTA 870 System Install Manual
REVISION 3, August, 2002
PART NUMBER 006-10609-0003
Add, delete or replace pages as indicated below and retain all tabs and dividers. Insert
this page immediately behind the title page as a record of revisions. This revision level of
this manual consists of the following individual publications:
PAGE ACTION
Rev 0 Initial Release Insert Entire Manual
Rev 1 B1, B2 Remove and Replace
Appendix F Insert New Appendix
Rev 2 Pages 2-17, and 18 Remove and Replace
Pages 3-3, 15, 29,
35, 93 and 97 Remove and Replace
Page 3-23 Figure 3-21 Add
Section IV Remove and Replace
Page D-11, 12 Remove and Replace
Rev. 3 Pages 1-2, 1-3, 1-8, 1-12, Addition of JTSO ref.
1-1
Section 3, all drawings Replace Figures 3-1 thru 3-21.
Revision of Configuration Insert new section IV
Category 8.
Addition of Configuration
Categories 10 & 11 and
Tables 4-11 & 4-12.
Addition of KTA Fault Codes Insert at the end of Appendix D.

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THIS PAGE IS RESERVED

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SECTION I
GENERAL INFORMATION
1.0 INTRODUCTION .................................................................................... 1-1
1.1 PURPOSE .............................................................................................. 1-1
1.2 APPLICABILITY OF THE SYSTEM MANUAL ....................................... 1-1
1.2.1 Equipment Applicability .......................................................................... 1-1
1.3 SYSTEM DESCRIPTION ....................................................................... 1-2
1.3.1 Basic EGPWS System ........................................................................... 1-2
1.3.2 Basic TAS System ................................................................................. 1-3
1.3.3 System Components .............................................................................. 1-3
1.3.4 System Operation .................................................................................. 1-6
1.4 TECHNICAL CHARACTERISTICS ........................................................ 1-9
1.5 UNIT AND ACCESSORIES SUPPLIED ................................................ 1-12
1.5.1 TAS Processor Unit ................................................................................ 1-12
1.5.2 Configuration Module ............................................................................. 1-13
1.5.3 Antennas ................................................................................................ 1-13
1.6 INSTALLATION ACCESSORIES SUPPLIED ........................................ 1-14
1.6.1 KMH 820/KTA 810 Installation Kit .......................................................... 1-14
1.6.2 Antenna Installation Kits.......................................................................... 1-15
1.6.3 Databases............................................................................................... 1-16
1.7 ACCESSORIES REQUIRED BUT NOT SUPPLIED .............................. 1-16
1.7.1 Temperature Probe ................................................................................ 1-16
1.7.2 GPS Antenna Splitter.............................................................................. 1-16
1.7.3 Miscellaneous ........................................................................................ 1-17
1.7.4 Cable And Wire ...................................................................................... 1-17
1.8 LICENSE REQUIREMENTS .................................................................. 1-17
1.9 INSTRUCTIONS FOR CONTINUED AIRWORTHINESS ...................... 1-18
1.9.1 KMH 820/KTA 810 Unit........................................................................... 1-18
1.9.2 Annunciators/Relays ............................................................................... 1-18
1.9.3 GPS Antenna .......................................................................................... 1-18
1.9.4 GPS Antenna Splitter.............................................................................. 1-18
1.9.5 Temperature Probe................................................................................. 1-19
1.9.6 Wire and Coax Cables ............................................................................ 1-19
1.9.7 Terrain Data Base Updates..................................................................... 1-19

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LIST OF ILLUSTRATIONS
Figure 1-1 KMH 880/KTA 870 System ......................................................... 1-6
LIST OF TABLES
Table 1-1 KMH 880/KTA 870 Applicable Versions ...................................... 1-2
Table 1-2 KMH 880 LRUs ........................................................................... 1-4
Table 1-3 KTA 870 LRUs ............................................................................ 1-4
Table 1-4 KMH 820 w/o GPS Multi-Hazard Unit Technical Specifications .. 1-9
Table 1-5 KMH 820 w/ GPS Multi-Hazard Unit Technical Specifications..... 1-10
Table 1-6 KTA 810 Traffic Advisory Unit Technical Specifications .............. 1-10
Table 1-7 KCM 805 Configuration Module Technical Specifications ........... 1-11
Table 1-8 KA 815 Traffic Antenna Technical Specifications ........................ 1-11
Table 1-9 KA 92 GPS Antenna Technical Specifications ............................ 1-12
Table 1-10 KMH 820/KTA 810 Processor Units ............................................ 1-12
Table 1-11 KCM 805 Configuration Module .................................................. 1-13
Table 1-12 KA 815/KA 92 Antennas .............................................................. 1-13
Table 1-13 GPS Cable Run Lengths ............................................................. 1-14
Table 1-14 KMH 820/KTA 810 Installation Kit .............................................. 1-15
Table 1-15 KA 815 Installation Kit................................................................ 1-15
Table 1-16 KA 92 Installation Kit .................................................................. 1-15
Table 1-17 Data Bases................................................................................... 1-16
Table 1-18 Temperature Probe ..................................................................... 1-16
Table 1-19 GPS Antenna Splitter ................................................................... 1-17
Table 1-20 Miscellaneous Accessories ......................................................... 1-17
Table 1-21 Cable and Wire ............................................................................ 1-17
SECTION II
INSTALLATION
2.0 INTRODUCTION .................................................................................... 2-1
2.1 UNPACKING AND INSPECTING EQUIPMENT.................................... 2-1
2.2 EQUIPMENT INSTALLATION ............................................................... 2-1
2.2.1 General ................................................................................................ 2-1
2.2.2 Avionics Cooling Requirements ........................................................... 2-2
2.2.3 Processor Installation ........................................................................... 2-3
2.2.3.1 Cooling Considerations ..................................................................... 2-3
2.2.3.2 Installation Considerations ................................................................ 2-3
2.2.3.3 Installation Procedure ....................................................................... 2-5
2.2.4 Configuration Module Installation.......................................................... 2-11
2.2.4.1 Cooling Considerations ..................................................................... 2-11

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2.2.4.2 Installation Considerations ................................................................ 2-11
2.2.4.3 Installation Procedure ....................................................................... 2-11
2.2.5 Directional Antenna Installation ............................................................ 2-15
2.2.5.1 KA 815 Antenna Installation Considerations ..................................... 2-15
2.2.6 GPS Antenna Installation ..................................................................... 2-19
2.2.6.1 KA 92 antenna Installation Considerations (KMH 820 EGPWS only) .2-19
2.2.6.2 Installation Procedure ....................................................................... 2-19
2.2.7 TAS Coaxial Cable Fabrication............................................................. 2-28
2.2.8 GPS Coaxial Cable Fabrication ............................................................ 2-29
LIST OF ILLUSTRATIONS
Figure 2-1 KMH 820/KTA 810 Installation Drawing....................................... 2-7
Figure 2-2 Configuration Module Installation Drawing................................... 2-13
Figure 2-3 KA 815 Antenna Outline and Mounting Drawing ......................... 2-17
Figure 2-4 KA 815 Antenna Installation Drawing........................................... 2-21
Figure 2-5 KA 815 Doubler Plate Drawing..................................................... 2-23
Figure 2-6 KA 92 Outline and Mounting Drawing ......................................... 2-25
Figure 2-7 GPS Antenna Splitter ................................................................... 2-27
Figure 2-8 Coax Cable Treatment ................................................................. 2-30
Figure 2-9 Standard Coax Cable................................................................... 2-30
Figure 2-10 Bulkhead/In-Line Connection Coax Cable ................................... 2-30
Figure 2-11 TNC Antenna Coax/Connector Assembly.................................... 2-31
Figure 2-12 TNC Antenna Coax/Connector Assembly.................................... 2-32
LIST OF TABLES
Table 2-1 Signal Losses.............................................................................. 2-29
SECTION III
SYSTEM PLANNING
3.0 INTRODUCTION ................................................................................... 3-1
3.0.1 Applicable Part Numbers Subsection Description ................................ 3-1
3.0.2 Function Subsection Description .......................................................... 3-1
3.0.3 Requirements and Limitations Subsection Description........................ 3-1
3.0.4 Electrical Characteristics Subsection Description. ............................... 3-1
3.0.5 Interface Subsection Description ......................................................... 3-2
3.1 GENERAL INTERCONNECT INFORMATION ...................................... 3-5
3.1.1 Power Inputs ..................................................................................... 3-5
3.1.2 On Discrete........................................................................................ 3-5
3.1.3 Air/Ground Discrete Input ................................................................. 3-6
3.1.4 Landing Gear Discrete Input ............................................................. 3-6

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3.1.5 Above/Below/Normal Input............................................................... 3-7
3.1.6 Baro Altitude (ARINC 429) Input ....................................................... 3-7
3.1.7 Advisory Inhibit Input ........................................................................ 3-7
3.1.8 TAS Valid Output .............................................................................. 3-8
3.1.9 Visual Annunciate Traffic (Lamp Output) .......................................... 3-8
3.1.10 Synthesized Voice Output ................................................................ 3-8
3.1.11 Air Temperature Input ....................................................................... 3-9
3.1.12 GPS Input ......................................................................................... 3-9
3.1.13 Factory Test Input ............................................................................. 3-10
3.1.13.1 TAS ATE Enable Input ................................................................... 3-10
3.1.13.2 TAS Built In Test Equipment (BITE) .............................................. 3-10
3.1.13.3 EGPWS Self Test Input ................................................................. 3-11
3.1.13.4 Display Select Input ....................................................................... 3-12
3.1.13.5 Terrain Awareness Inhibit Discrete ................................................ 3-12
3.1.14 Terrain Warning ................................................................................ 3-12
3.1.15 Terrain Caution.................................................................................. 3-12
3.1.16 Weather Select Output ..................................................................... 3-12
3.1.17 EGPWS Audio On Discrete .............................................................. 3-13
3.1.18 EGPWS Terrain Inop and Terrain Not Available Output.................... 3-13
LIST OF ILLUSTRATIONS
Figure 3-1 KMH 880/KTA 870 Interconnect Family...................................... 3-3
Figure 3-2 KMH 820/KTA 810 Pinout Diagram ............................................. 3-15
Figure 3-3 KMH 820/KTA 810 System Interconnect Block Diagram ............. 3-29
Figure 3-4 KMH 820/KTA 810 Power Interface ............................................ 3-33
Figure 3-5 KMH 820/KTA 810 Discrete Interface ......................................... 3-35
Figure 3-6 KMH 820/KTA 810 Configuration Module Interconnect ............... 3-37
Figure 3-7 KMH 820/KTA 810 Attitude/Heading Interface............................. 3-39
Figure 3-8 KMH 820/KTA 810 Radar/Barometric Altitude Interface ............. 3-41
Figure 3-9 KMH 820/KTA 810 Antenna/Suppression Interface.................... 3-49
Figure 3-10 KMH 820/KTA 810 EFS 40/50 Interface .................................... 3-51
Figure 3-11 KMH 820/KTA 810 GC 362A Interface ....................................... 3-53
Figure 3-12 KMH 820/KTA 810 Honeywell GC 362A Interface....................... 3-59
Figure 3-13 KMH 820/KTA 810 Collins GC 362A Interface............................. 3-65
Figure 3-14 KMH 820/KTA 810 Honeywell Primus 1000 Interface.................. 3-69
Figure 3-15 KMH 820/KTA 810 Honeywell SPZ-805 Interface........................ 3-73
Figure 3-16 KMH 820/KTA 810 Diagnostic/Data Recorder Interface ............. 3-77
Figure 3-17 KMH 820/KTA 810 TAS ATE Interface....................................... 3-79
Figure 3-18 KMH 820/KTA 810 CP 66B Interface........................................... 3-81
Figure 3-19 KMH 820/KTA 810 KFS 578A Interface....................................... 3-83
Figure 3-20 KMH 820/KTA 810 Display Interface............................................ 3-87
Figure 3-21 KMH 820/KTA 810 External GPS Interface.................................. 3-97
Figure 3-22 KMH 820/KTA 810 Processor Front Connector .......................... 3-99
Figure 3-23 KMH 820/KTA 810 Front Connector Cable.................................. 3-100
Figure 3-24 KMH 820/KTA 810 Rear Connector Cable................................... 3-101

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LIST OF TABLES
Table 3-1 KMH 820/KTA 810 Connector Pin Assignment ........................... 3-102
SECTION IV
POST INSTALLATION CONFIGURATION AND CHECK OUT
4.0 INTRODUCTION .................................................................................... 4-1
4.1 LINE SELECT KEYS .............................................................................. 4-1
4.2 CONFIGURATION PROCEDURE ......................................................... 4-1
4.2.1 Power On ............................................................................................. 4-1
4.2.2 Aircraft Configuration ........................................................................... 4-1
4.2.3 EGPWS Configuration Instructions....................................................... 4-2
4.2.3.1 Equipment needed................................................................................ 4-2
4.2.3.2 Configuration Module Programming ..................................................... 4-2
4.2.3.3 Configuration String Format.................................................................. 4-3
4.2.3.4 RS-232 Maintenance Port (Port SMC1)................................................ 4-4
4.2.3.5 Configuration Sequence of Events ....................................................... 4-4
4.2.3.6 Configuration Types.............................................................................. 4-5
4.2.3.7 Configuration Identification Selection.................................................... 4-5
4.2.3.8 Configuration Tables............................................................................. 4-7
4.2.3.8.1 Category 1, Aircraft/Mode Type Select............................................. 4-7
4.2.3.8.2 Category 2, Air Data Input Select ..................................................... 4-7
4.2.3.8.3 Category 3, Position Input Select ..................................................... 4-9
4.2.3.8.4 Category 4, Terrain Display Select................................................... 4-10
4.2.3.8.5 Category 5, Input/Output Discrete Type Select ................................ 4-11
4.2.3.8.6 Category 6, Audio Menu Select........................................................ 4-11
4.2.3.8.7 Category 7, Audio Output Level........................................................ 4-11
4.2.3.8.8 Category 8, Altitude Monitor Options................................................ 4-12
4.2.3.8.9 Category 9, Terrain Display Alternate Pop Up Option...................... 4-12
4.2.3.8.10 Category 10, Attitude and Heading Select........................................ 4-13
4.2.3.8.11 Category 11, Display Option Select.................................................. 4-14
4.2.4 TAS Configuration Options .................................................................. 4-15
4.2.4.1 TAS RS-232 Maintenance Port............................................................ 4-18
4.2.4.2 TAS RS-422 Data Recorder ................................................................ 4-18
4.3 GROUND TEST PROCEDURES ........................................................... 4-19
4.3.1 Required Test Equipment ...................................................................... 4-19
4.3.2 EGPWS Ground Test Procedures ......................................................... 4-19
4.3.3 TAS Ground Test Procedures................................................................ 4-22

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LIST OF ILLUSTRATIONS
Figure 4-1 TAS Bearing Measurements ............................................................ 4-37
LIST OF TABLES
Table 4-1 Configuration Identification........................................................... 4-5
Table 4-2 Aircraft/Mode Type Select............................................................ 4-7
Table 4-3 Air Data Input Select .................................................................... 4-9
Table 4-4 Position Input Select..................................................................... 4-9
Table 4-5 Terrain Display Select .................................................................. 4-10
Table 4-6 Input/Output DiscreteType Select ................................................ 4-11
Table 4-7 Audio Menu Select ....................................................................... 4-11
Table 4-8 Audio Output Level....................................................................... 4-12
Table 4-9 Altitude Monitor Option................................................................. 4-12
Table 4-10 Terrain Display Alternate Pop Up Option ..................................... 4-13
Table 4-11 Attitude and Heading Type........................................................... 4-13
Table 4-12 Display Option Type..................................................................... 4-15
SECTION V
CERTIFICATION
5.0 INTRODUCTION .................................................................................... 5-1
5.1 CERTIFICATION PROCEDURE ............................................................ 5-1
5.1.1 Equipment Compatibility ........................................................................ 5-1
5.1.2 Equipment Location ............................................................................... 5-1
5.1.3 Federal Communication Commission Rules .......................................... 5-2
5.1.4 TSO Category ........................................................................................ 5-2
5.1.5 FAA Requirements ................................................................................. 5-2
5.1.6 FAA Form 337 ........................................................................................ 5-2
5.1.7 Flight Manual Revision ........................................................................... 5-3
5.1.8 Pilot Briefing ........................................................................................... 5-3
SECTION VI
OPERATION
6.0 INTRODUCTION..................................................................................... 6-1

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LIST OF APPENDICES
APPENDIX A Mode C..................................................................................... A-1
APPENDIX B STC .......................................................................................... B-1
APPENDIX C Certification .............................................................................. C-1
APPENDIX D TASDiag................................................................................... D-1
APPENDIX E TSO.......................................................................................... E-1
APPENDIX F Airplane Flight Manual Supplement ......................................... F-1

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SECTION 1
GENERAL INFORMATION
1.0 INTRODUCTION
This manual contains information relative to the physical, mechanical and electri-
cal characteristics of the KMH 880/KTA 870 Multi-Hazard Awareness System. It
includes the basic guidelines, considerations and recommendations for the instal-
lation and ground checkout of KMH 880/KTA 870 Multi-Hazard Awareness System
and associated components. It is intended to provide the detail required to assist
the installer in preparation for installation and appropriate work instructions to
ensure a proper installation and checkout.
This manual assumes a familiarity with avionics installation practices, with sys-
tems on board the aircraft and access to manuals and regulations commensurate
with the installation of such equipment.
The information contained herein, together with the general procedures outlined in
FAA AC 43.13-1B and AC 43.13-2A should be followed carefully to ensure a safe
and electrically sound system installation.
The contents of this manual are for information and reference use only and must
not be construed as a formal FAA approved work authorization.
It is highly recommended that prior to beginning the installation of the KMH 880/
KTA 870 system that this manual is carefully reviewed. Upon review the neces-
sary configuration items and system requirements will be identified allowing a
speedy installation.
Operational information is contained in the KMH 880/KTA 870 Operators Manual
supplied with each unit.
1.1 PURPOSE
This manual will describe the detailed system requirements for the Bendix/King KMH 880
Multi-Hazard Awareness System and KTA 870 Traffic Advisory System . The KMH 880
combines TAS (Traffic Advisory System) with EGPWS (Enhanced Ground Proximity
Warning System). The KTA 870 has TAS only.
1.2 APPLICABILITY OF THE SYSTEM MANUAL
1.2.1 Equipment Applicability
This manual is applicable only to KMH 880 Multi-Hazard Awareness/KTA 870 Traf-
fic Awareness System part numbers displayed in the table below:

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1.3 SYSTEM DESCRIPTION
1.3.1 Basic EGPWS System
The KMH 880 EGPWS is a revolutionary new step in Controlled Flight Into Terrain
(CFIT) protection. It is capable of producing advanced alerting for prevention of
CFIT accidents. In addition to the alerting protection the system will also produce
a terrain display. This display depicts relative terrain in reference to the lateral and
vertical positions of the aircraft.
The EGPWS is intended for Light Turbine and Piston Aircraft Operations. It has
effective operational performance in providing timely alerts and operational terrain
display to enhance situational awareness. This performance, coupled to the sys-
tem's simplicity, practicality, small size and weight, with a minimum number of
required aircraft sensors, provides a formidable safety value.
NOTE
The EGPWS portion of the KMH 820 is not suitable for helicopter operation.
No Radio Altimeter, Landing Gear or Flap Discretes, or Glideslope Receiver are
necessary. This significantly lowers the installation costs.
The KMH 880 is a system designed to minimize the system requirements down to
a level economical to the private pilot. It is the central component in the system
providing timely alerts and optional display of impending terrain incursions.
The KMH 820 is a TSO C151a Class B compliant unit.
UNIT NOMENCLATURE PART NUMBER
KTA 810 Traffic Advisory Unit 066-01152-0101
KMH 820 w/o GPS Multi-hazard Awareness Unit 066-01175-0101
KMH 820 w/GPS Multi-hazard Awareness Unit 066-01175-2101
Table 1-1 KMH 880/KTA 870 Applicable Versions

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1.3.2 Basic TAS System
The Airborne TAS system is capable of surveillance of aircraft equipped with tran-
sponders (i.e., Mode S and ATCRBS) able to reply to ATCRBS Mode C interroga-
tions in their operational environments. This is a step toward determining
potential collisions and displaying traffic advisory information to the pilot. The TAS
system will interoperate with the U.S. National Standard Air Traffic Control Radar
Beacon System (ATCRBS) and perform reliably out to a range of ten nautical
miles for densities up to 0.08 aircraft per square nautical mile while complying with
all ATCRBS signals-in-space requirements. The TAS equipment will not degrade
either the electromagnetic or the air traffic environment.
When all features are implemented the equipment has the capabilities of the Traf-
fic Advisory System (TAS) defined by TSO-C147 Class A.
The TAS system will provide:
(1) An alert to the pilot using an audible and visual advisory of the proximity of
an intruder aircraft.
(2) The range to ± 0.1 nautical mile, altitude (if reported by surveilled aircraft),
and relative bearing of intruder aircraft with maximum installed accuracy of
±30° with high reliability. If the intruder aircraft is transponder equipped,
within ten nautical miles, ± 10,000 feet relative altitude, and TAS is not in
interference limiting, it will be reliably detected and reported.
(3)Timely data that does not lag more than 2 seconds behind the actual rela-
tive position as seen by the pilot during normal flight operations.
(4) Probability of displaying false targets will be less than 2%. If they are dis-
played, they will not persist for more than a few seconds.
(5) No increase of traffic on the Secondary Surveillance Radar radio frequen-
cies in a manner that degrades the ATC system.
(6) Display of indications that do not encourage the pilot to maneuver without
first visually acquiring the other aircraft and determining that a maneuver is
required.
1.3.3 System Components
The KMH 880 Multi-Hazard Awareness System shall be composed of the KMH
820 (TAS/EGPWS Processor), a top mounted directional antenna (KA 815), a bot-
tom mounted antenna (a KA-815 directional antenna which shall provide esti-
mated bearing of target aircraft, or an omni-directional monopole antenna which
will not provide bearing information), a top mounted GPS antenna (KA 92), and a
Configuration Module (KCM 805).

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A Multifunctional Display Unit, KMD 540, shall provide control and display of traffic
(via the KAC 504 Traffic Card) and control and display of EGPWS data (via the
KAC 502 Adapter Card). Other displays that are compatible with ARINC 735A
may be used for traffic with this system. See Figure 1-1.
The KTA 870 Traffic Advisory System is similar to the KMH 880 except the KTA
810 Traffic Advisory Unit has only TAS and not EGPWS. The KTA 870 system
does not use a KA 92 GPS antenna. See Table 1-2 and Table 1-3 for a complete
description and part number listing for both systems.
KMH 880 SYSTEM PRIMARY LRUs
System Component LRU Manufacturer/
Model Designator
LRU Description LRU Part Number
TAS/GA EGPWS
Processor
Bendix/King KMH 820 Multi-Hazard Awareness
Processor
066-01175-0101
066-01175-2101
Directional Antenna Bendix/King KA 815 TAS Directional Antenna 071-01599-0100
GPS Antenna Bendix/King KA 92 GPS Antenna 071-01553-0200
Configuration Module Bendix/King KCM 805 Configuration Module 071-00112-0100
Control Panel/Display Bendix/King KMD 540 Multi-function Display 066-04035-0X01
Bendix/King KAC 502 EGPWS Card 071-00158-0211
Bendix/King KAC 504 Traffic Card 071-00166-0411
Table 1-2 KMH 880 LRUs
KTA 870 SYSTEM PRIMARY LRUs
System Component LRU Manufacturer/
Model Designator
LRU Description LRU Part Number
TAS Processor Bendix/King KTA 810 TAS Processor 066-01152-0101
Directional Antenna Bendix/King KA 815 TAS Directional Antenna 071-01599-0100
Configuration Module Bendix/King KCM 805 Configuration Module 071-00112-0100
Control Panel/Display Bendix/King KMD 540 Multi-function Display 066-04035-0X01
Bendix/King KAC 504 Traffic Card 071-00166-0411
Table 1-3 KTA 870 LRUs

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In addition to the equipment listed in Tables 1-2and 1-3, the KMH 820/KTA 810
was qualified with the following displays:
AlliedSignal IVA 81A/C/D TCAS Display 066-50001-XXXX TSO C119a
066-05053-XXXX TSO C8c
066-01171-XXXX
Bendix/King IN 182A EGPWS Display 066-03084-003X TSO C63b
Other displays that are compatible with ARINC 735A may be used to display traffic
with this system. The EGPWS data may also be displayed on Bendix/King and
AlliedSignal weather radar display units. To put traffic on these weather radar dis-
plays, the following adapter unit is required:
Bendix/King GC 362A Graphics computer 071-01505-0X03 TSO C105
(To allow traffic on radar displays)

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Figure 1-1 KMH 880/KTA 870 System
1.3.4 System Operation
A. EGPWS System
1. EGPWS Modes of Operation
a. Optional Alerting and Warning Parameters
The EGPWS may also be installed in aircraft that do not require FAA
approved TAWS Systems, and may be utilized with an optional set of alert-
ing and warning parameters that are designed especially for smaller piston
aircraft and their normal flight characteristics.