SYSTEM INSTALLATION MANUAL CAS 67A TCAS II SYSTEM

Transcription

1 SYSTEM INSTALLATION MANUAL CAS 67A TCAS II SYSTEM MANUAL NUMBER REVISION 7 SEPTEMBER, 2004

2 WARNING The enclosed technical data is eligible for export under License Designation NLR and is to be used solely by the individual/organization to whom it is addressed. Diversion contrary to U.S. law is prohibited. COPYRIGHT NOTICE , 2004 Honeywell International Inc. REPRODUCTION OF THIS PUBLICATION OR ANY PORTION THEREOF BY ANY MEANS WITHOUT THE EXPRESS WRITTEN PERMISSION OF HONEYWELL IS PROHIBITED, EXCEPT TO THE EXTENT REQUIRED FOR INSTALLATION OR MAINTENANCE OF THE RECIPIENT S EQUIPMENT. FOR FURTHER INFORMATION CONTACT THE MANAGER, TECHNICAL PUBLICATIONS, HONEYWELL, ONE TECHNOLOGY CENTER, WEST 105th STREET OLATHE KS TELEPHONE: (913)

3 System Installation Manual CAS 67A TCAS II Traffic Alert and Collision Avoidance System Including: TPU 67A TCAS II Processor CM 67A Configuration Module CM 2000 Configuration Module ANT 67A Directional Antenna IVA-81A TA/RA/VSI Display IVA-81B RA/VSI Display IVA-81C, IVA-81D TA/RA/VSI Display GC 362A TCAS Graphics Processor MST 67A Mode S Transponder KFS 578A Mode S/TCAS Control Unit CD 671C Mode S/TCAS Control Unit CTA-81A Mode S/TCAS Control Unit CTA-81D Mode S/TCAS Control Unit PS-550 Mode S/TCAS Control Unit PS-578A Mode S/TCAS Control Unit T-1

4 NOTE IF ANY UNUSUAL OR SPECIFIC SERVICE PROBLEMS ARISE, CONTACT HONEYWELL, WEST 105TH STREET, OLATHE, KANSAS, NO EQUIPMENT SHALL BE RETURNED TO THE CUSTOMER SERVICE DEPARTMENT UNTIL A RETURN AUTHORIZATION (RA) FORM IS REQUESTED AND RECEIVED FROM HONEYWELL. PROPRIETARY NOTICE This document contains proprietary information and such information may not be disclosed to others for any purpose, nor used for manufacturing purposes without written permission from Honeywell. PN-1

5 REVISION HIGHLIGHTS Sept/2004 This is a complete reprint. All pages are revised and reformatted. General highlights include updates to PS-550/PS-578 Control Heads and updates to general control head information. Updated TCAS II system drawing. Updated environmental qualification information. Updated TCASDIAG for Windows appendix and antenna test appendix. Specific changes to content are denoted by revision bar. RH-1

6 THIS PAGE IS RESERVED RH-2

7 RECORD OF REVISIONS REV. NO. REVISION DATE DATE INSERTED BY DATE REMOVED BY Complete through Revision 7 RR-1

8 RECORD OF REVISIONS (cont.) REV. NO. REVISION DATE DATE INSERTED BY DATE REMOVED BY RR-2

9 RECORD OF TEMPORARY REVISIONS T.R. NO. DATE DATE INSERTED BY DATE REMOVED BY Complete through Revision TR RTR-1

10 RECORD OF TEMPORARY REVISIONS (cont.) REV. NO. REVISION DATE DATE INSERTED BY DATE REMOVED BY RTR-2

11 TCAS II SERVICE LITERATURE LIST The following are installation bulletins applicable to the CAS 67A TCAS II system. BULLETIN NUMBER DATE COVERAGE IB 372 IB 398 APR/1995 JUL/1997 TO CORRECT ERROR IN TPU CONFIG MODULE PROCEDURE TCASDIAG GUIDE FOR FIELD REFERENCE IB 438 IB 439 IB 447 IB 452 APR/1999 MAR/1999 MAY/1999 JAN/2000 INFORMATION ON TCAS I AND II RETURN-TO-SERVICE FOLLOWING COMPONENT REPAIR OR REPLACEMENT APPROVAL FOR THE REPLACEMENT OF IVA 81A INDICATORS WITH IVA 81C INDICATORS CLARIFICATION OF CAS 67A TCAS II SYSTEM AND ACAS II SYSTEM PILOT S GUIDES INTERCHANGEABILITY OF IVA 81A C AND D TA/VSI TCAS INDICATORS IB 456 IB 457 IB 458 NOV/2000 NOV/1999 FEB/2000 TCASDIAG FOR WINDOWS AND TCAS PROCESSOR FIELD DIAGNOSTIC PROGRAM FOR USER MANUAL TCASDIAG GUIDE CLARIFICATION OF THE ALTITUDE INTERFACE TO THE TCAS PROCES- SOR AND/OR MST 67A TRANSPONDER The following is service literature information applicable to the CAS 67A system and TPU 67A unit. For current service literature information for related units and/or systems, refer to the Installation or Maintenance Manual of the applicable unit. BULLETIN NUMBER DATE COVERAGE EFFECTIVE S/N SA CAS 67A-101 OCT/1997 ADDITION OF RAIN EROSION FILM TO ANTENNA N.A. SA CAS 67A-102 JAN/1998 TEST PROCEDURES FOR SWR AND CABLE LOSS FOR ECS RF TROUBLESHOOTER KIT N.A. SA TPU 67A-101 OCT/1996 FAULT CODE GUIDE N.A. SA TPU 67A-102 FEB/1999 REPLACEMENT FOR OBSOLETE PIN DIODES N.A. SB-1

12 BULLETIN NUMBER DATE COVERAGE EFFECTIVE S/N SA TPU 67A-103 JUN/2000 REPLACEMENT FOR OBSOLETE FLASH AND REAL-TIME CLOCK N.A. SA TPU 67A-104 JAN/2002 REPLACEMENT RECEIVER ASSEMBLY N.A. SB TPU 67A-4 MAY/1997 STABILIZE SWITCHING SPEED OF DISCRETE INPUT CIR- CUITS SB TPU 67A-5 SEP/1998 ADDITIONAL LIGHTNING PROTECTION FOR THE UNIT S +28 VDC POWER LINES SB TPU 67A-6 OCT/1998 MANUFACTURING EFFICIENCY IMPROVEMENT SB TPU 67A-7 MAR/2002 UNIT MOD 13 ALLEVIATE TIMING ISSUES IN CONFIGURA- TION MODULE INTERFACE SB TPU 67A-8 MAR/2002 INCREASE TPU MEANTIME BETWEEN FAILURES SB TPU 67A-9 APR/2002 PREVENT COLD INDUCED AUDIO FAILURES SB TPU 67A-10 JUN/2000 THIS BULLETIN HAS BEEN SUPERSEDED SB TPU 67A-11 APR/2001 INCREASE POWER-HANDLING CAPABILITY AND RELIABIL- ITY OF -250VDC MONITOR CIRCUIT SB TPU 67A-12 NOV/2001 PREVENT ACCIDENTAL WRITES TO THE FLASH MEMORY DUR- ING NORMAL OPERATION VERSION DEPENDENT VERSION DEPENDENT SB TPU-67A-13 JAN/2003 REPLACE TPU S OBSOLETE COMPUTER BOARD VERSION DEPENDENT SB TPU 67A-14 JUN/2002 INCORPORATE REPLACEMENT FOR OBSOLETE REFERENCE BOARD PART NUMBER SB TPU 67A-15 JUN/2002 INCORPORATE REPLACEMENT FOR OBSOLETE SWITCH DRIVER BOARD PART NUMER SB TPU 67A-16 JUN/2002 INCORPORATE REPLACEMENT OF POWER SUPPLY BOARD #2 PART NUMBER SB TPU 67A-17 JUN/2002 INCORPORATE REPLACEMENT OF OBSOLETE VIDEO BOARD PART NUMBER SB TPU 67A-18 AUG/2002 PREVENT THE TPU 67A FRO INTERFERING WITH THE PRI- MUS DME DURING EQUIPMENT START-UP SB TPU 67A-19 FEB/2003 UNIT WILL NOT INITIALIZE AND LED DISPLAY ON THE SIDE OF THE PROCESSOR IS BLANK SB TPU 67A-20 DEC/2002 REPLACEMENT OF INTERCONNECT BD DUE TO ERRONEOUS EXTERNAL FAULT CODES SB TPU 67A-21 MAR/2003 REPLACE THREE TRANSORBS ON INTERCONNECT BOARD WITH A LOWER VOLTAGE VARIETY VERSION DEPENDENT VERSION DEPENDENT VERSION DEPENDENT VERSION DEPENDENT VERSION DEPENDENT VERSION DEPENDENT VERSION DEPENDENT VERSION DEPENDENT SB-2

13 BULLETIN NUMBER DATE COVERAGE SB TPU 67A-22 AUG/2003 REPLACES OBSOLETE RECEIVER ASSY PART NUMBER WITH SB TPU 67A-23 SEP/2003 GIVES ADDITIONAL PROTECTION FROM ARCING BETWEEN THE SWITCH DRIVER BOARD AND THE MAINFRAME CASTING AND INCREASES CONDUCTIVITY AT CERTAIN PIN CONNEC- TIONS SB TPU 67A-24 SEP/2003 GIVES ADDITIONAL PROTECTION FROM ARCING TO THE RF BOARD THE IF BOARD THE TRANSMIT MODULATOR BOARD AND THE REFERENCE BOARD EFFECTIVE S/N VERSION DEPENDENT VERSION DEPENDENT VERSION DEPENDENT SB TPU 67A-M1 MAR/2001 INCORPORATE SOFTWARE 12/01 (CHANGE 7) VERSION DEPENDENT SWB TPU 67A-SW1 AUG/1995 TO INCORPORATE 01/02 SOFTWARE N.A. SWB TPU 67A-SW2 AUG/1995 TO INCORPORATE 01/03 SOFTWARE N.A. SWB TPU 67A-SW3 OCT/1996 TO INCORPORATE 01/11 SOFTWARE SWB TPU 67A-SW4 MAR/2002 INCORPORATE SOFTWARE LEVEL 01/12 VERSION DEPENDENT SWB TPU 67A-SW5 JUN/2000 INCORPORATE SOFTWARE 01/13 COMPATIBLE WITH NEW FLASH OR REAL-TIME CLOCK SWB TPU 67A-SW6 JUN/2000 INCORPORATE SOFTWARE 11/03. CORRECTS INCORRECT TCAS FAIL MESSAGE WHILE UNIT IN STANDBY MODE. ALSO COMPATIBLE WITH NEW FLASH OR REAL-TIME CLOCK SWB TPU 67A-SW7 DEC/2001 INCORPORATE SOFTWARE 11/04. ENABLES UNIT TO INTER- FACE WITH COLLINS TDR 94D TRANSPONDERS N.A. VERSION DEPENDENT VERSION DEPENDENT SB-3

14 THIS PAGE IS RESERVED SB-4

15 LIST OF EFFECTIVE PAGES SUBJECT PAGE DATE Title Page * T-1 Sept/2004 Proprietary Notice * PN-1 Sept/2004 Revision Highlights * RH-1 Sept/2004 * RH-2 Sept/2004 Record of Revisions * RR-1 Sept/2004 * RR-2 Sept/2004 Record of Temporary Revisions * RTR-1 Sept/2004 * RTR-2 Sept/2004 List of Service Bulletins * SB-1 Sept/2004 * SB-2 Sept/2004 * SB-3 Sept/2004 * SB-4 Sept/2004 List of Effective Pages * LEP-1 Sept/2004 * LEP-2 Sept/2004 * LEP-3 Sept/2004 * LEP-4 Sept/2004 * LEP-5 Sept/2004 * LEP-6 Sept/2004 * LEP-7 Sept/2004 * LEP-8 Sept/2004 * LEP-9 Sept/2004 * LEP-10 Sept/2004 * LEP-11 Sept/2004 * LEP-12 Sept/2004 * LEP-13 Sept/2004 * LEP-14 Sept/2004 Table of Contents * TC-1 Sept/2004 * TC-2 Sept/2004 * TC-3 Sept/2004 * TC-4 Sept/2004 * TC-5 Sept/2004 * TC-6 Sept/2004 * TC-7 Sept/2004 * TC-8 Sept/2004 * TC-9 Sept/2004 F INDICATES FOLDOUT PAGES; * INDICATES PAGES CHANGED IN LATEST REVISION LEP-1 Sept/2004

16 Table of Contents (cont). * TC-10 Sept/2004 * TC-11 Sept/2004 * TC-12 Sept/2004 * TC-13 Sept/2004 * TC-14 Sept/2004 Introduction * INTRO-1 Sept/2004 * INTRO-2 Sept/2004 Description and Operation * 1 Sept/2004 * 2 Sept/2004 F * 3 Sept/2004 * 4 Blank * 5 Sept/2004 * 6 Sept/2004 * 7 Sept/2004 * 8 Sept/2004 * 9 Sept/2004 * 10 Sept/2004 * 11 Sept/2004 * 12 Sept/2004 * 13 Sept/2004 * 14 Sept/2004 * 15 Sept/2004 * 16 Sept/2004 * 17 Sept/2004 * 18 Sept/2004 * 19 Sept/2004 * 20 Sept/2004 * 21 Sept/2004 * 22 Sept/2004 * 23 Sept/2004 * 24 Sept/2004 * 25 Sept/2004 * 26 Sept/2004 * 27 Sept/2004 * 28 Sept/2004 * 29 Sept/2004 * 30 Sept/2004 * 31 Sept/2004 * 32 Sept/2004 * 33 Sept/2004 * 34 Sept/2004 * 35 Sept/2004 * 36 Sept/2004 F INDICATES FOLDOUT PAGES; * INDICATES PAGES CHANGED IN LATEST REVISION LEP-2 Sept/2004

17 Description and Operation (cont). * 37 Sept/2004 * 38 Sept/2004 * 39 Sept/2004 * 40 Sept/2004 * 41 Sept/2004 * 42 Sept/2004 * 43 Sept/2004 * 44 Sept/2004 * 45 Sept/2004 * 46 Sept/2004 * 47 Sept/2004 * 48 Sept/2004 * 49 Sept/2004 * 50 Sept/2004 * 51 Sept/2004 * 52 Sept/2004 * 53 Sept/2004 * 54 Sept/2004 * 55 Sept/2004 * 56 Sept/2004 * 57 Sept/2004 * 58 Sept/2004 * 59 Sept/2004 * 60 Sept/2004 * 61 Sept/2004 * 62 Sept/2004 * 63 Sept/2004 * 64 Sept/2004 * 65 Sept/2004 * 66 Sept/2004 * 67 Sept/2004 * 68 Sept/2004 * 69 Sept/2004 * 70 Sept/2004 * 71 Sept/2004 * 72 Sept/2004 * 73 Sept/2004 * 74 Sept/2004 * 75 Sept/2004 * 76 Sept/2004 * 77 Sept/2004 * 78 Sept/2004 * 79 Sept/2004 * 80 Sept/2004 * 81 Sept/2004 F INDICATES FOLDOUT PAGES; * INDICATES PAGES CHANGED IN LATEST REVISION LEP-3 Sept/2004

18 Description and Operation (cont). * 82 Sept/2004 * 83 Sept/2004 * 84 Sept/2004 * 85 Sept/2004 * 86 Sept/2004 * 87 Sept/2004 * 88 Sept/2004 * 89 Sept/2004 * 90 Sept/2004 * 91 Sept/2004 * 92 Sept/2004 * 93 Sept/2004 * 94 Sept/2004 * 95 Sept/2004 * 96 Sept/2004 * 97 Sept/2004 * 98 Sept/2004 * 99 Sept/2004 * 100 Sept/2004 * 101 Sept/2004 * 102 Sept/2004 * 103 Sept/2004 * 104 Sept/2004 * 105 Sept/2004 * 106 Sept/2004 * 107 Sept/2004 * 108 Sept/2004 * 109 Sept/2004 * 110 Sept/2004 * 111 Sept/2004 * 112 Sept/2004 * 113 Sept/2004 * 114 Sept/2004 * 115 Sept/2004 * 116 Sept/2004 * 117 Sept/2004 * 118 Sept/2004 * 119 Sept/2004 * 120 Sept/2004 F * 121 Sept/2004 * 122 Blank F * 123 Sept/2004 * 124 Blank * 125 Sept/2004 * 126 Sept/2004 F INDICATES FOLDOUT PAGES; * INDICATES PAGES CHANGED IN LATEST REVISION LEP-4 Sept/2004

19 Description and Operation (cont). * 127 Sept/2004 * 128 Sept/2004 * 129 Sept/2004 * 130 Sept/2004 * 131 Sept/2004 * 132 Sept/2004 * 133 Sept/2004 * 134 Sept/2004 * 135 Sept/2004 * 136 Sept/2004 * 137 Sept/2004 * 138 Sept/2004 * 139 Sept/2004 * 140 Sept/2004 * 141 Sept/2004 * 142 Sept/2004 * 143 Sept/2004 * 144 Sept/2004 * 145 Sept/2004 * 146 Sept/2004 * 147 Sept/2004 * 148 Sept/2004 * 149 Sept/2004 * 150 Sept/2004 * 151 Sept/2004 * 152 Sept/2004 * 153 Sept/2004 * 154 Sept/2004 * 155 Sept/2004 * 156 Sept/2004 * 157 Sept/2004 * 158 Sept/2004 * 159 Sept/2004 * 160 Sept/2004 * 161 Sept/2004 * 162 Sept/2004 * 163 Sept/2004 * 164 Sept/2004 F * 165 Sept/2004 * 166 Blank F * 167 Sept/2004 * 168 Blank F * 169 Sept/2004 * 170 Blank F * 171 Sept/2004 F INDICATES FOLDOUT PAGES; * INDICATES PAGES CHANGED IN LATEST REVISION LEP-5 Sept/2004

20 Description and Operation (cont). * 172 Blank Fault Isolation * 1001 Sept/2004 * 1002 Sept/2004 * 1003 Sept/2004 * 1004 Sept/2004 * 1005 Sept/2004 * 1006 Sept/2004 * 1007 Sept/2004 * 1008 Sept/2004 * 1009 Sept/2004 * 1010 Sept/2004 * 1011 Sept/2004 * 1012 Sept/2004 * 1013 Sept/2004 * 1014 Sept/2004 * 1015 Sept/2004 * 1016 Sept/2004 * 1017 Sept/2004 * 1018 Sept/2004 * 1019 Sept/2004 * 1020 Sept/2004 * 1021 Sept/2004 * 1022 Sept/2004 * 1023 Sept/2004 * 1024 Sept/2004 * 1025 Sept/2004 * 1026 Sept/2004 * 1027 Sept/2004 * 1028 Sept/2004 * 1029 Sept/2004 * 1030 Sept/2004 Maintenance Practices * 2001 Sept/2004 * 2002 Sept/2004 * 2003 Sept/2004 * 2004 Sept/2004 * 2005 Sept/2004 * 2006 Sept/2004 * 2007 Sept/2004 * 2008 Sept/2004 * 2009 Sept/2004 * 2010 Sept/2004 * 2011 Sept/2004 * 2012 Sept/2004 F INDICATES FOLDOUT PAGES; * INDICATES PAGES CHANGED IN LATEST REVISION LEP-6 Sept/2004

21 Maintenance Practices (cont). * 2013 Sept/2004 * 2014 Sept/2004 * 2015 Sept/2004 * 2016 Sept/2004 * 2017 Sept/2004 * 2018 Sept/2004 * 2019 Sept/2004 * 2020 Sept/2004 * 2021 Sept/2004 * 2022 Sept/2004 * 2023 Sept/2004 * 2024 Sept/2004 * 2025 Sept/2004 * 2026 Sept/2004 * 2027 Sept/2004 * 2028 Sept/2004 * 2029 Sept/2004 * 2030 Sept/2004 * 2031 Sept/2004 * 2032 Sept/2004 * 2033 Sept/2004 * 2034 Sept/2004 * 2035 Sept/2004 * 2036 Sept/2004 * 2037 Sept/2004 * 2038 Sept/2004 * 2039 Sept/2004 * 2040 Sept/2004 * 2041 Sept/2004 * 2042 Sept/2004 * 2043 Sept/2004 * 2044 Sept/2004 * 2045 Sept/2004 * 2046 Sept/2004 * 2047 Sept/2004 * 2048 Sept/2004 * 2049 Sept/2004 * 2050 Sept/2004 * 2051 Sept/2004 * 2052 Sept/2004 * 2053 Sept/2004 * 2054 Sept/2004 * 2055 Sept/2004 * 2056 Sept/2004 * 2057 Sept/2004 F INDICATES FOLDOUT PAGES; * INDICATES PAGES CHANGED IN LATEST REVISION LEP-7 Sept/2004

22 Maintenance Practices (cont). * 2058 Sept/2004 * 2059 Sept/2004 * 2060 Sept/2004 * 2061 Sept/2004 * 2062 Sept/2004 * 2063 Sept/2004 * 2064 Sept/2004 * 2065 Sept/2004 * 2066 Sept/2004 * 2067 Sept/2004 * 2068 Sept/2004 * 2069 Sept/2004 * 2070 Sept/2004 * 2071 Sept/2004 * 2072 Sept/2004 * 2073 Sept/2004 * 2074 Sept/2004 * 2075 Sept/2004 * 2076 Sept/2004 * 2077 Sept/2004 * 2078 Sept/2004 * 2079 Sept/2004 * 2080 Sept/2004 * 2081 Sept/2004 * 2082 Sept/2004 * 2083 Sept/2004 * 2084 Sept/2004 * 2085 Sept/2004 * 2086 Sept/2004 * 2087 Sept/2004 * 2088 Sept/2004 * 2089 Sept/2004 * 2090 Sept/2004 * 2091 Sept/2004 * 2092 Sept/2004 F * 2093 Sept/2004 * 2094 Blank F * 2095 Sept/2004 * 2096 Blank F * 2097 Sept/2004 * 2098 Blank F * 2099 Sept/2004 * 2100 Blank F * 2101 Sept/2004 * 2102 Blank F INDICATES FOLDOUT PAGES; * INDICATES PAGES CHANGED IN LATEST REVISION LEP-8 Sept/2004

23 Maintenance Practices (cont). F * 2103 Sept/2004 * 2104 Blank F * 2105 Sept/2004 * 2106 Blank F * 2107 Sept/2004 * 2108 Blank F * 2109 Sept/2004 * 2110 Blank F * 2111 Sept/2004 * 2112 Blank F * 2113 Sept/2004 * 2114 Blank F * 2115 Sept/2004 * 2116 Blank F * 2117 Sept/2004 * 2118 Blank F * 2119 Sept/2004 * 2120 Blank F * 2121 Sept/2004 * 2122 Blank F * 2123 Sept/2004 * 2124 Blank F * 2125 Sept/2004 * 2126 Blank F * 2127 Sept/2004 * 2128 Blank F * 2129 Sept/2004 * 2130 Blank F * 2131 Sept/2004 * 2132 Blank F * 2133 Sept/2004 * 2134 Blank F * 2135 Sept/2004 * 2136 Blank F * 2137 Sept/2004 * 2138 Blank F * 2139 Sept/2004 * 2140 Blank F * 2141 Sept/2004 * 2142 Blank F * 2143 Sept/2004 * 2144 Blank F * 2145 Sept/2004 * 2146 Blank F * 2147 Sept/2004 F INDICATES FOLDOUT PAGES; * INDICATES PAGES CHANGED IN LATEST REVISION LEP-9 Sept/2004

24 Maintenance Practices (cont). * 2148 Blank F * 2149 Sept/2004 * 2150 Blank F * 2151 Sept/2004 * 2152 Blank F * 2153 Sept/2004 * 2154 Blank F * 2155 Sept/2004 * 2156 Blank F * 2157 Sept/2004 * 2158 Blank F * 2159 Sept/2004 * 2160 Blank F * 2161 Sept/2004 * 2162 Blank F * 2163 Sept/2004 * 2164 Blank F * 2165 Sept/2004 * 2166 Blank F * 2167 Sept/2004 * 2168 Blank F * 2169 Sept/2004 * 2170 Blank F * 2171 Sept/2004 * 2172 Blank F * 2173 Sept/2004 * 2174 Blank F * 2175 Sept/2004 * 2176 Blank F * 2177 Sept/2004 * 2178 Blank F * 2179 Sept/2004 * 2180 Blank F * 2181 Sept/2004 * 2182 Blank F * 2183 Sept/2004 * 2184 Blank F * 2185 Sept/2004 * 2186 Blank F * 2187 Sept/2004 * 2188 Blank F * 2189 Sept/2004 * 2190 Blank F * 2191 Sept/2004 * 2192 Blank F INDICATES FOLDOUT PAGES; * INDICATES PAGES CHANGED IN LATEST REVISION LEP-10 Sept/2004

25 Maintenance Practices (cont). F * 2193 Sept/2004 * 2194 Blank F * 2195 Sept/2004 * 2196 Blank F * 2197 Sept/2004 * 2198 Blank F * 2199 Sept/2004 * 2200 Blank F * 2201 Sept/2004 * 2202 Blank F * 2203 Sept/2004 * 2204 Blank F * 2205 Sept/2004 * 2206 Blank F * 2207 Sept/2004 * 2208 Blank F * 2209 Sept/2004 * 2210 Blank F * 2211 Sept/2004 * 2212 Blank F * 2213 Sept/2004 * 2214 Blank F * 2215 Sept/2004 * 2216 Blank F * 2217 Sept/2004 * 2218 Blank Diagnostic Appendices * APP-1 Sept/2004 * APP-2 Sept/2004 * APP-3 Sept/2004 * APP-4 Sept/2004 * APP-5 Sept/2004 * APP-6 Sept/2004 * APP-7 Sept/2004 * APP-8 Sept/2004 * APP-9 Sept/2004 * APP-10 Sept/2004 * APP-11 Sept/2004 * APP-12 Sept/2004 * APP-13 Sept/2004 * APP-14 Sept/2004 * APP-15 Sept/2004 * APP-16 Sept/2004 * APP-17 Sept/2004 * APP-18 Sept/2004 F INDICATES FOLDOUT PAGES; * INDICATES PAGES CHANGED IN LATEST REVISION LEP-11 Sept/2004

26 Diagnostic Appendices (cont). * APP-19 Sept/2004 * APP-20 Sept/2004 * APP-21 Sept/2004 * APP-22 Sept/2004 * APP-23 Sept/2004 * APP-24 Sept/2004 * APP-25 Sept/2004 * APP-26 Sept/2004 * APP-27 Sept/2004 * APP-28 Sept/2004 * APP-29 Sept/2004 * APP-30 Sept/2004 * APP-31 Sept/2004 * APP-32 Sept/2004 * APP-33 Sept/2004 * APP-34 Sept/2004 * APP-35 Sept/2004 * APP-36 Sept/2004 * APP-37 Sept/2004 * APP-38 Sept/2004 * APP-39 Sept/2004 * APP-40 Sept/2004 * APP-41 Sept/2004 * APP-42 Sept/2004 * APP-43 Sept/2004 * APP-44 Sept/2004 * APP-45 Sept/2004 * APP-46 Sept/2004 * APP-47 Sept/2004 * APP-48 Sept/2004 * APP-49 Sept/2004 * APP-50 Sept/2004 * APP-51 Sept/2004 * APP-52 Sept/2004 * APP-53 Sept/2004 * APP-54 Sept/2004 * APP-55 Sept/2004 * APP-56 Sept/2004 * APP-57 Sept/2004 * APP-58 Sept/2004 * APP-59 Sept/2004 * APP-60 Sept/2004 * APP-61 Sept/2004 * APP-62 Sept/2004 * APP-63 Sept/2004 F INDICATES FOLDOUT PAGES; * INDICATES PAGES CHANGED IN LATEST REVISION LEP-12 Sept/2004

27 Diagnostic Appendices (cont). * APP-64 Sept/2004 * APP-65 Sept/2004 * APP-66 Sept/2004 * APP-67 Sept/2004 * APP-68 Sept/2004 * APP-69 Sept/2004 * APP-70 Sept/2004 * APP-71 Sept/2004 * APP-72 Sept/2004 * APP-73 Sept/2004 * APP-74 Sept/2004 * APP-75 Sept/2004 * APP-76 Sept/2004 * APP-77 Sept/2004 * APP-78 Sept/2004 * APP-79 Sept/2004 * APP-80 Sept/2004 * APP-81 Sept/2004 * APP-82 Sept/2004 * APP-83 Sept/2004 * APP-84 Sept/2004 * APP-85 Sept/2004 * APP-86 Sept/2004 * APP-87 Sept/2004 * APP-88 Sept/2004 * APP-89 Sept/2004 * APP-90 Sept/2004 F INDICATES FOLDOUT PAGES; * INDICATES PAGES CHANGED IN LATEST REVISION LEP-13 Sept/2004

28 THIS PAGE IS RESERVED F INDICATES FOLDOUT PAGES; * INDICATES PAGES CHANGED IN LATEST REVISION LEP-14 Sept/2004

29 TABLE OF CONTENTS ITEM PAGE SYSTEM DESCRIPTION 1. General System Configuration...1 A. TPU 67A TCAS II Processor...2 B. CM 67A/CM 2000 Configuration Module...9 C. ANT 67A Directional Antenna...10 D. L-Band Omnidirectional Antenna...13 E. IVA-81A TA/RA/VSI...14 F. IVA-81B RA/VSI...19 G. IVA-81C/IVA-81D TA/RA/VSI...21 H. GC 362A TCAS Graphics Processor...24 I. MST 67A Mode S Transponder...26 J. KFS 578A Mode S/TCAS II Control Unit Configurations...31 K. PS-578A Mode S/TCAS II Control Unit Configurations...34 L. PS-550 Mode S/TCAS II Control Unit Configurations...41 M. CD 671C Control Unit...44 N. CTA-81A Control Unit...47 O. CTA-81D Control Unit...50 P. Optional Displays and Control Units Environmental Certification Related Publications CAS 67A TCAS II Installation Kits...95 A. TPUDIAG/TCASDIAG Config. Module/Diagnostic Software Kits...95 B. TPU 67A Installation Kit (New Installation)...95 C. TPU 67A Installation Kit (TCAS I to TCAS II Upgrade)...97 D. ANT 67A Antenna Adapter Kits...98 E. Omnidirectional Antenna Installation Kit...98 TC-1

30 ITEM PAGE F. IVA-81A/IVA-81B/IVA-81C/IVA-81D Installation Kits...99 G. GC 362A Installation Kit H. MST 67A Installation Kit I. KFS 578A / PS-578A Installation Kit J. PS-578A Configuration Programming Harness K. PS-550 Connector Assembly L. CD 671C Installation Kit M. CTA-81A/CTA-81D Installation Kit System Description A. General B. TCAS II Functional Overview C. System Integration System Component Functions A. TCAS Processor B. Directional Antenna C. TCAS Omnidirectional Antenna D. TA/RA/VSI Display E. RA/VSI Display F. Mode S Transponder G. Control Units System Control and Indicator Functions A. General B. TCAS Input Power Control C. TCAS II Control Units D. GC 362A TCAS Graphics Processor E. TA/RA/VSI F. RA/VSI G. Weather Radar/TCAS Display H. Optional Aural/Lamp Advisory Outputs I. Audio Message Alerts TC-2

31 ITEM PAGE J. TCAS Processor and Mode S Transponder Fault Indicators K. Optional Advisory Cancel Switch L. Range Selection and Range Rings FAULT ISOLATION 1. General Fault Isolation A. General B. Fault Isolation Using the Mode S/TCAS Control Unit C. Fault Isolation Using TCAS Processor LED Fault Codes D. Fault Isolation Using the Diagnostic Computer INSTALLATION AND MAINTENANCE 1. General Unpacking Pre-Installation Testing Equipment Changes and Markings Equipment Location and Interwiring A. General B. Location of Equipment C. Interwiring and Cable Fabrication Equipment Installation A. TPU 67A TCAS Processor Installation B. Configuration Module Installation C. TCAS Directional Antenna Installation D. TCAS Omnidirectional Antenna Installation E. IVA-81A/C/D TA/RA/VSI and IVA-81B RA/VSI Installation F. Transponder and Mounting Tray Installation G. KFS 578A/PS-578A/PS-550/CD 671C Control Unit Installation TC-3

32 ITEM PAGE H. GC 362A TCAS Graphics Processor Installation Inspection and System Checkout A. System Interwiring Check B. Visual Inspection C. Post-Installation Test D. Flight Test (Required for STC) Removal and Replacement A. TPU 67A TCAS Processor B. Directional Antenna C. Omnidirectional Antenna D. TCAS Control Unit E. 3ATI Traffic Displays F. GC 362A TCAS Graphics Processor G. CM 67A/CM 2000 Configuration Module Maintenance Procedures A. In-Aircraft Adjustments B. System Protection C. Lubrication D. Cleaning Aircraft Maintenance Programs A. General B. Honeywell TCAS Maintenance Recommendations ANT 67A Directional Antenna Adapter Plate Installation A. General Information B. Installation Procedure A C. Installation Procedure B D. Recommended Materials E. Bonding Requirements TC-4

33 ITEM PAGE DIAGNOSTIC APPENDICES TC-5

34 THIS PAGE IS RESERVED TC-6

35 ITEM PAGE Figure 1 CAS 67A TCAS II System Components...3 Figure 2 TPU 67A Environmental Qualification Form...52 Figure 3 CM 67A Environmental Qualification Form...57 Figure 4 CM 2000 Environmental Qualification Form...60 Figure 5 ANT 67A Environmental Qualification Form...63 Figure 6 CD 671C Environmental Qualification Form...64 Figure 7 KFS 578A Environmental Qualification Form (-0000)...66 Figure 8 KFS 578A Environmental Qualification Form (-0010)...67 Figure 9 PS-578A Environmental Qualification Form...69 Figure 10 PS-550 Environmental Qualification Form...72 Figure 11 CTA 81() Environmental Qualification Form...75 Figure 12 MST 67A Environmental Qualification Form (-0000)...82 Figure 13 MST 67A Environmental Qualification Form (-0010)...83 Figure 14 MST 67A Environmental Qualification Form (-0020)...85 Figure 15 GC 362A Environmental Qualification Form...88 Figure 16 IVA 81A/B Environmental Certification Categories...90 Figure 17 IVA 81C Environmental Qualification Form...91 Figure 18 IVA 81D Environmental Qualification Form...92 Figure 19 PS-578A Configuration Programming Harness Figure 20 TPU 67A TCAS II Processor, Inputs/Outputs Figure 21 Mode S and ATCRBS Mode C Interrogation Formats Figure 22 Mode S and ATCRBS Mode C Transponder Reply Message Formats.133 Figure 23 TCAS Directional Antenna Transmit/Receive Beam Patterns Figure 24 IVA-81A/IVA-81C/IVA-81D TA/RA/VSI Figure 25 IVA-81B RA/VSI Figure 26 KFS 578A Control Unit Controls TC-7

36 ITEM PAGE Figure 27 PS-578A Control Unit Controls Figure 28 PS-550 Control Unit Controls Figure 29 CD 671C Control Unit Controls Figure 30 CTA-81 ( ) Control Unit Controls Figure 31 GC 362A TCAS Graphics Processor, TCAS and Radar Displays Figure 32 Collins IND270 Indicator, TCAS and Radar Displays Figure 33 Honeywell WI650 Radar Indicator, TCAS and Radar Displays Figure 34 Honeywell P90 Radar Indicator, TCAS and Radar Displays Figure 1001 TCAS Test Pattern Figure 2001 TPU 67A TCAS Processor Rear Connector Key & Pin Locations.2010 Figure 2002 IVA-81A/B/C/D Rear Connector Locations Figure 2003 IVA-81A/B/C/D Electrical Connector Pin Locations Figure 2004 KFS 578A Control Unit, Rear Connectors Figure 2005 PS-578A Mode S/TCAS Control Unit Rear Connector (J1) Figure 2006 PS-578A Mode S/TCAS Control Unit Rear Connector (J2) Figure 2007 PS-550 Mode S/TCAS Control Unit Rear Connector Figure 2008 CD 671C Control Unit, Rear Connectors Figure 2009 GC 362A TCAS Graphics Processor, Rear Connector Figure 2010 TCAS Bearing Measurements Figure 2011 ANT 67A Directional Antenna Adapter and Moldable Shim Figure 2012 TPU 67A TCAS II Processor Outline Drawing Figure 2013 CM 67A/CM 2000 Configuration Module Outline Drawing Figure 2014 ANT 67A Directional Antenna Outline Drawing Figure 2015 IVA 81A (TA/RA/VSI) Outline Drawing Figure 2016 IVA 81B (RA/VSI) Outline Drawing Figure 2017 IVA 81C (TCAS) Outline Drawing TC-8

37 ITEM PAGE Figure 2018 IVA 81D (TCAS) Outline Drawing Figure 2019 GC 362 TCAS Graphics Processor Outline Drawing Figure 2020 KFS 578A Control Unit Outline Drawing Figure 2021 PS-578A Control Unit Outline Drawing Figure 2022 PS-550 Control Unit Outline Drawing Figure 2023 CD 671C Control Unit Outline Drawing Figure 2024 TPU 67A Interconnect Drawing Family Figure 2025 TPU 67A Pinout Drawing Figure 2026 TCAS II Configuration Pins Interface Drawing Figure 2027 TCAS II Discrete Interface Drawing Figure 2028 TCAS Radar/Baro Altitude Interface Drawing Figure 2029 Attitude/Heading Interface Drawing Figure 2030 Antenna/Suppression Interface Drawing Figure 2031 Power Interface Drawing Figure 2032 Lear 31/EFS 40/50 TCAS Interface Drawing Figure 2033 GC 362/Bendix TCAS Interface Drawing Figure 2034 GC 362/Honeywell TCAS Interface Drawing Figure 2035 GC 362/Collins TCAS Interface Drawing Figure 2036 RA Display (ARINC 429 Low Speed) Interface Drawing Figure 2037 TA/RA Display (ARINC 429 High Speed) Interface Drawing Figure 2038 Citation VB Honeywell EFIS/TCAS Interface Drawing Figure 2039 Jetstream 41 Honeywell EFIS/TCAS Interface Drawing Figure 2040 Diagnostic/Data Recorder Interface Drawing Figure 2041 TCAS II ATE Interface Drawing Figure 2042 MST 67A Mode S Interface Drawing Figure 2043 Collins TDR-94D Mode S Interface Drawing TC-9

38 ITEM PAGE Figure 2044 Honeywell Primus II/TCAS Interface Drawing Figure 2045 CAS 67A TCAS II System Interface Drawing TC-10

39 ITEM PAGE Table 1 CAS 67A TCAS II System Components...1 Table 2 TPU 67A TCAS II Processor Versions...2 Table 3 TPU 67A TCAS II Processor Features...2 Table 4 TPU 67A TCAS II Processor Specifications...5 Table 5 CM 67A/CM 2000 Configuration Module Versions...9 Table 6 CM 67A/CM 2000 Configuration Module Features...9 Table 7 CM 67A/CM 2000 Configuration Module Specifications...9 Table 8 ANT 67A Directional Antenna Versions...10 Table 9 ANT 67A Directional Antenna Features...10 Table 10 ANT 67A Directional Antenna Specifications...11 Table 11 Omnidirectional Antenna Versions...13 Table 12 Omnidirectional Antenna Features...13 Table 13 IVA-81A TA/RA/VSI Versions...14 Table 14 IVA-81A TA/RA/VSI Features...17 Table 15 IVA-81A TA/RA/VSI Specifications...18 Table 16 IVA-81B RA/VSI Versions...19 Table 17 IVA-81B RA/VSI Features...19 Table 18 IVA-81B RA/VSI Specifications...20 Table 19 IVA-81C TA/RA/VSI Versions...21 Table 20 IVA-81C TA/RA/VSI Features...21 Table 21 IVA-81D TA/RA/VSI Versions...22 Table 22 IVA-81D TA/RA/VSI Features...22 Table 23 IVA-81C/IVA-81D TA/RA/VSI Specifications...23 Table 24 GC 362A TCAS Graphics Processor Versions...24 Table 25 GC 362A TCAS Graphics Processor Features...24 Table 26 GC 362A TCAS Graphics Processor Specifications...25 TC-11

40 ITEM PAGE Table 27 MST 67A Mode S Transponder Versions...26 Table 28 MST 67A Mode S Transponder Features...27 Table 29 MST 67A Mode S Transponder Specifications...28 Table 30 KFS 578A Control Unit Versions...31 Table 31 KFS 578A Control Unit Features...32 Table 32 KFS 578A Control Unit Specifications...33 Table 33 KFS 578A - PS-578A Configuration Cross-Reference (TCAS II)..34 Table 34 PS-578A Control Unit Versions...38 Table 35 PS-578A Control Unit Features...39 Table 36 PS-578A Control Unit Specifications...40 Table 37 PS-550 Control Unit Versions...41 Table 38 PS-550 Control Unit Features...42 Table 39 PS-550 Control Unit Specifications...43 Table 40 CD 671C Control Unit Versions...44 Table 41 CD 671C Control Unit Features...45 Table 42 CD 671C Control Unit Specifications...46 Table 43 CTA-81A Control Unit Versions...47 Table 44 CTA-81A Control Unit Features...48 Table 45 CTA-81A/CTA-81D Control Unit Specifications...49 Table 46 CTA-81D Control Unit Versions...50 Table 47 CTA-81D Control Unit Features...50 Table 48 Optional Displays and Control Units...51 Table 49 Related Publications...93 Table 50 TPUDIAG/TCASDIAG Config. Module/Diagnostic Software Kits...95 Table 51 TPU 67A TCAS II Processor Installation Kit...96 Table 52 TPU 67A TCAS II Processor Upgrade Installation Kit...97 TC-12

41 ITEM PAGE Table 53 TPU 67A TCAS II Processor Upgrade Installation Kit...97 Table 54 ANT 67A Antenna Adapter Kits...98 Table 55 IVA-81A/IVA-81B/IVA-81C/IVA-81D Installation Kit...99 Table 56 IVA-81A/IVA-81B/IVA-81C/IVA-81D Installation Kit...99 Table 57 IVA-81A/IVA-81B/IVA-81C/IVA-81D Installation Kit...99 Table 58 GC 362A Installation Kit Table 59 MST 67A Installation Kit Table 60 KFS 578A / PS-578A Installation Kit Table 61 CD 671C Installation Kit Table 62 CTA-81A/CTA-81D Installation Kit Table 63 TCAS II System Integration Matrix Table 64 Control Unit Control and Indicator Functions Table 1001 TCAS/Weather Radar Display Fault Annunciations Table 1002 Catastrophic Single Letter Failure Codes Table 1003 TCAS Processor Fault Codes Table 2001 TPU 67A TCAS Processor, Rear Connector Pin Names Table 2002 Configuration Module, Connector Pin Names Table 2003 IVA-81A/B/C/D Electrical Connector Pin Names Table 2004 KFS 578A Control Unit Connector (P5782) Pin Definitions Table 2005 KFS 578A Control Unit Connector Pin Names (P5781) Table 2006 PS-578A Control Unit Connector (J1) Pin Definitions Table 2007 PS-578A Control Unit Connector (J2) Pin Definitions Table 2008 PS-550 Control Unit Connector Pin Name Definitions Table 2009 CD 671C Control Unit, Connector Pin Names Table 2010 GC 362A TCAS Graphics Proc , Connector Pin Names Table 2011 GC 362A TCAS Graphics Proc , Connector Pin Names TC-13

42 ITEM PAGE Table 2012 GC 362A TCAS Graphics Proc , Connector Pin Names Table 2013 Inspection/Check Procedure TC-14

43 INTRODUCTION This manual includes description, installation, fault isolation, and flight-line checkout procedures for the Honeywell CAS 67A (TCAS II) Traffic Alert and Collision Avoidance System. The conditions and tests required for the TSO and MOPS approval of this article are minimum performance standards. It is the responsibility of those installing this article either on or with a specified type or class of aircraft to determine that the aircraft installation conditions are within the TSO and MOPS standards. These articles must have separate approval for installation in an aircraft. Any features in this equipment outside the requirements of this applicable TSO and MOPS must be evaluated and approved as part of the installation approval. The article may be installed only if performed under 14 CFR part 43 or the applicable airworthiness requirements. INTRO-1

44 THIS PAGE IS RESERVED INTRO-2

45 1. General SYSTEM DESCRIPTION SYSTEM DESCRIPTION contains functional descriptions, equipment part numbers, and specifications for the Honeywell CAS 67A TCAS II Traffic Alert and Collision Avoidance System. The CAS 67A TCAS II system monitors airspace around its "own" aircraft by interrogating an "intruder" aircraft s transponder. The TCAS processor computes the range, differential altitude, bearing and closure rate of the intruder. It then compares this data to its own position and determines the potential for collision. Audio messages and visual displays of traffic advisories (TAs) and collision resolution advisories (RAs) are produced when required. 2. System Configuration Components of the CAS 67A TCAS II system are listed in Table 1 CAS 67A TCAS II System Components and shown in Figure 1 CAS 67A TCAS II System Components. Versions, features, and specifications of system components are listed in following paragraphs. NOTE: Some part numbers may not be currently available. Consult the current Honeywell catalog or contact a Honeywell representative for equipment availability. PROCESSOR ANTENNA (TOP) ANTENNA (BOTTOM) DISPLAYS TRANSPONDER CONTROL UNIT TPU 67A TCAS II Processor and CM 67A/CM 2000 Configuration Module ANT 67A Directional Antenna ANT 67A Directional Antenna OR: L-band Omnidirectional antenna (dc shorted) optional Dual resolution advisory displays and a traffic display required: Two IVA-81A/IVA-81C/IVA-81D TA/RA/VSI Traffic Advisory/Resolution Advisory/ Vertical Speed Indicators. OR: IVA-81B RA/VSI Resolution Advisory/Vertical Speed Indicator and a radar/traffic display via GC 362A TCAS Graphics Processor. OR: KAD 480T Air Data System and an EFIS 40/50 MFD Display via symbol generator. MST 67A ATC Mode S (diversity) Transponder KFS 578A/PS-578A/PS-550 Mode S Transponder/TCAS Control Unit OR: CD 671C Mode S Transponder/TCAS Control Unit OR: CTA-81A/CTA-81D Mode S Transponder/TCAS Control Unit OR: RMS 555 Radio Management System Table 1 CAS 67A TCAS II System Components Page 1

46 A. TPU 67A TCAS II Processor Listed below are versions, features, and specifications of the TPU 67A TCAS II processor. HONEYWELL PART NUMBER VERSION NUMBER PRIMARY POWER SINGLE OR DUAL DIRECTIONAL ANT EXTENDED ENVIRONMENTAL PROTECTION SECONDARY ATT/HDG INPUT Vdc X Vdc X X X Vdc X X Vdc X X X X Table 2 TPU 67A TCAS II Processor Versions CHANGE 7 SOFTWARE ACAS II FEATURE Basic Unit Primary Power Single or Dual Directional Antenna Extended Environmental Protection Attitude/Heading Secondary Input DESCRIPTION TCAS II transmitter-receiver. Primary component of CAS 67A system. Contains circuitry necessary for functions of a TCAS II system and interfacing with configuration module, antennas, graphic processors, controls, and displays. 28 Vdc power input Designed for installations having top-mounted directional antenna, and bottom-mounted directional or omnidirectional antenna. TPU 67A p/n s ,-1211 have been TSO d with additional environmental testing (Radio Frequency Susceptibility [Radiated and Conducted], Emission of Radio Frequency Energy, and Lightning Induced Transient Susceptibility categories). Refer to Figure 2 TPU 67A Environmental Qualification Form for details. TPU 67A p/n s ,-1211 have an additional secondary ARINC429 AHRS/IRU Attitude/Heading Input Port. NOTE: One or two directional antennas may be used in a TCAS II system. A top-mounted ANT 67A is always required. For intruder bearing to be determined on the bottom-antenna an ANT 67A must be used on bottom of aircraft. Table 3 TPU 67A TCAS II Processor Features Page 2

47 Figure 1 CAS 67A TCAS II System Components Page 3/4

48 CHARACTERISTIC Form Factor Physical Dimensions Weight Power Requirements Primary DESCRIPTION 4 MCU ARINC 600 (1/2 long ATR) See Figure 2012 TPU 67A TCAS II Processor Outline Drawing See Figure 2012 TPU 67A TCAS II Processor Outline Drawing +28 Vdc (22-30 Vdc), 70 watts (maximum) Reference 26 Vac synchro reference power (ARINC 413A) Altitude Temperature Range Operating Storage Cooling Surveillance Capacity Voice Synthesizer Output Receiver Minimum Trigger Level (MTL) Decoding Ratio Input at -78 dbm or less at antenna Input at MTL +3 db to -21 dbm Out-of-Band Rejection (reply signal level required to provide 90% decoding ratio) At and MHz At 1075 and 1105 MHz At 1065 and 1115 MHz Dynamic Minimum Trigger Level (DMTL) Threshold ATCRBS Mode S Minimum Pulse Width Maximum Pulse Rise Time Category A2 15,000 ft; F2 55,000 ft -55 C to +70 C -55 C to +85 C Convection 45 aircraft. Some TCAS display up to 30 of the closest-range intruders. Speaker: 6.5 watts into 8 ohms. Headphones: 40 milliwatts (nominal) into 600 ohms (strap selectable). Frequency 1087 to 1093 MHz -74 dbm ±2 db at antenna end of coax 10% maximum 99% minimum 3 db above MTL minimum 40 db above MTL minimum 60 db above MTL minimum MTL + 13 db MTL + 10 db 300 µsec 0.50 µsec Table 4 TPU 67A TCAS II Processor Specifications (Sheet 1 of 4) Page 5

49 CHARACTERISTIC Delay Difference (between top and bottom antenna channels, including transmission lines) DESCRIPTION 0.05 µsec Transmitter: Frequency ±0.01 MHz Warm up time 3 minutes for frequency stabilization Input VSWR: 1.35:1 Rf Peak Output Power at unit connector Omni Antenna Minimum dbm (50 W) Maximum dbm (126 W) Directional Antenna (per port) Minimum +47 dbm (50 W) Maximum +51 dbm (126 W) Nominal +49 dbm (79 W) Unwanted Output Power -70 dbm maximum (inactive state) Interrogation Repetition 1 second Interval Broadcast Interrogation 10 seconds in each direction (nominal) Interval Interrogation Interval Jitter Mode S and ATCRBS Mode C +0.1 to -0.1 seconds about the nominal 1-second interval. TCAS Broadcast -1.0 to +1.0 seconds about the nominal 10-second interval. Transmitter Delay Difference µsec maximum (between top and bottom antenna channels, including transmission lines) Table 4 TPU 67A TCAS II Processor Specifications (Sheet 2) Page 6

50 CHARACTERISTIC DESCRIPTION Transmitter (Cont.) Transmitter Pulse Characteristics Mode C Only All-Call (S1, P1, P2, P3, P4) Pulse Duration 0.80 ±0.05 µsec Rise Time 0 to 0.10 µsec Decay Time 0 to 0.20 µsec Pulse Spacing P1 to P ±0.10 µsec P1 to P ±0.10 µsec P3 to P ±0.04 µsec S1 to P ±0.10 µsec Mode S Pulse Duration P1, P ±0.05 µsec P6 (short) ±0.125 µsec P6 (long) ±0.125 µsec Rise Time 0.05 to 0.10 µsec Decay Time 0.05 to 0.20 µsec S1 Pulse 10 db below the P1 pulse in the current set of pulses. The level is dependent on the whisper-shout level. Table 4 TPU 67A TCAS II Processor Specifications (Sheet 3) Page 7

51 CHARACTERISTIC Transmitter Pulse Pulse Spacing P1 to P2 P2 to P6 sync phase reversal P6 leading edge to P6 sync phase reversal High Resolution Whisper-Shout Mode C Power Levels S1 Pulse Minimum Basic Whisper-Shout Mode C Power Levels ( ,-1211 only) Connectors DESCRIPTION 2.00 ±0.04 µsec 2.75 ±0.04 µsec 1.25 ±0.04 µsec 2 db or 3 db below the P1 pulse in the current set of pulses. The level is dependent on the whispershout level. ARINC 404. See Figure 2001 TPU 67A TCAS Processor Rear Connector Key & Pin Locations TSO C119a p/n ,-0201 C119b p/n ,-1211 Environmental Certification See Figure 2 TPU 67A Environmental Qualification Form Table 4 TPU 67A TCAS II Processor Specifications (Sheet 4) Page 8

52 B. CM 67A/CM 2000 Configuration Module Listed below are versions, features, and specifications of the CM 67A/CM 2000 configuration module. HONEYWELL PART NUMBER VERSION NUMBER BASIC UNIT INITIALIZED W/ DEFAULTS NUMBER OF MOUNTING SCREWS TSO COMPLIANCE CM 67A X 2 C63c, C119a CM C63c, C119a Table 5 CM 67A/CM 2000 Configuration Module Versions FEATURE Basic Unit DESCRIPTION Contains two 9356 EEPROMS stored with hardware strap and bearing calibration information. Screw mounted within two (2) feet of wire harness from the TCAS processor rack. Table 6 CM 67A/CM 2000 Configuration Module Features CHARACTERISTIC Physical Dimensions Weight Components Mounting Power Requirements Temperature Electrical Connector TSO Environmental Certification DESCRIPTION See Figure 2013 CM 67A/CM 2000 Configuration Module Outline Drawing See Figure 2013 CM 67A/CM 2000 Configuration Module Outline Drawing Solid state, no mechanical parts Remote. See Figure 2013 CM 67A/CM 2000 Configuration Module Outline Drawing +5 Vdc, via TPU 67A TCAS II processor -55 C to +70 C See Figure 2013 CM 67A/CM 2000 Configuration Module Outline Drawing C119a and C63c See Figure 3 CM 67A Environmental Qualification Form or Figure 4 CM 2000 Environmental Qualification Form Table 7 CM 67A/CM 2000 Configuration Module Specifications Page 9

53 HONEYWELL PART NUMBER C. ANT 67A Directional Antenna Listed below are versions, features, and specifications of the ANT 67A directional antenna. VERSION NUMBER ANTENNA SHAPE COAX CONN BASIC SHAPE NUMBER OF MOUNTING SCREWS Teardrop 1.50" Flat Teardrop 0.73" Flat 4 Table 8 ANT 67A Directional Antenna Versions FEATURE Basic Unit DESCRIPTION Four-element passive array. Screw mounted to aircraft fuselage. Radiates 1030 MHz, pulse-modulated inputs from TPU 67A TCAS processor. Detects radiated 1090 MHz, pulse-modulated signals. Table 9 ANT 67A Directional Antenna Features Page 10

54 CHARACTERISTIC DESCRIPTION Form Factor ARINC 735 (teardrop shape) Physical Dimensions See Figure 2014 ANT 67A Directional Antenna Outline Drawing Weight See Figure 2014 ANT 67A Directional Antenna Outline Drawing Antenna Base Types Flat base ( ,-0200) Altitude Category F2 55,000 ft. Temperature Range Operating -55 C to +70 C Storage -55 C to +85 C Antenna Mounting Footprint See Figure 2014 ANT 67A Directional Antenna Outline Drawing Antenna Mounting Mounts directly to aircraft using mounting instructions, defined in Figure 2011 ANT 67A Directional Antenna Adapter and Moldable Shim, Figure 2014 ANT 67A Directional Antenna Outline Drawing, and paragraph 11. ANT 67A Directional Antenna Adapter Plate Installation. An antenna adapter is required for mounting flatbase antenna on a curved surface. Exterior Material High-strength composite Number of Antenna Array Elements Four Polarization Vertical Power Requirements None Transmission Frequency 1030 ±1 MHz Receiving Frequency 1090 ±3 MHz Connectors See Figure 2014 ANT 67A Directional Antenna Outline Drawing Quantity Four Type See Figure 2014 ANT 67A Directional Antenna Outline Drawing Pressurization Withstands a pressure differential of 25 P.S.I.A. Lighting Protection Meets swept zone 2A lightning strike requirements Table 10 ANT 67A Directional Antenna Specifications (Sheet 1 of 2) Page 11

55 CHARACTERISTIC DESCRIPTION Main Beam Characteristics Operational Beam Positions 4 Half Power Azimuth Beam Width > 90 degrees (measured over -15 to +20 elevation) Steering Quantization 90 Omni Beam Characteristics Operational Beam Positions 360 Beam Null Compared to Main Beam (at each elevation from -15 to +20) Input Port VSWR Antenna Cable Loss Requirement > 9 db 1.35:1 maximum 2.5 ± 0.5 db at 1030 MHz for each coaxial cable including connectors Antenna Cable Differential Phase Delay 135 maximum electrical length Maximum Peak Input Power 1000 W pulsed Maximum Average Input Power 10 W continuous ARINC Characteristic ARINC 735 TSO C118 and C119a Environmental Certification See Figure 5 ANT 67A Environmental Qualification Form Table 10 ANT 67A Directional Antenna Specifications (Sheet 2) Page 12

56 D. L-Band Omnidirectional Antenna Listed below are versions and features of the omnidirectional antenna. VENDOR NAME MODEL VENDOR PART NUMBER Dorne & Margolin DMNI 50- Series LRU DESCRIPTION IMPEDANCE/ RF/DC Table 11 Omnidirectional Antenna Versions TSO COMPLIANCE DMNI L-Band 50 Ω/Short C66a, C74c FEATURE Basic Unit DESCRIPTION Screw mounted to aircraft fuselage. Radiates 1030 MHz, pulse-modulated inputs from TPU 67A TCAS processor. Detects radiated 1090 MHz, pulsemodulated signals. Vertically polarized. Table 12 Omnidirectional Antenna Features Page 13

57 E. IVA-81A TA/RA/VSI Listed below are versions, features, and specifications of the IVA- 81A TA/RA/VSI. HONEYWELL PART NUMBER VERSION NUMBER FACE PLATE PRIMARY POWER PANEL LIGHTING UP DN RANGE CONTROL TA SELECT SWITCH DIM (POT) SW IDENT Black 115 Vac 5 Vac/Vdc 01/ Gray 115 Vac 5 Vac/Vdc 01/ Brown 115 Vac 5 Vac/Vdc 01/ Blue 115 Vac 5 Vac/Vdc 01/ Black 115 Vac 5 Vac/Vdc X 01/ Gray 115 Vac 5 Vac/Vdc X 01/ Brown 115 Vac 5 Vac/Vdc X 01/ Blue 115 Vac 5 Vac/Vdc X 01/ Black 115 Vac 5 Vac/Vdc X X 01/ Gray 115 Vac 5 Vac/Vdc X X 01/ Brown 115 Vac 5 Vac/Vdc X X 01/ Blue 115 Vac 5 Vac/Vdc X X 01/ Black 28 Vdc 5 Vac/Vdc 01/ Gray 28 Vdc 5 Vac/Vdc 01/ Black 28 Vdc 5 Vac/Vdc X 01/ Gray 28 Vdc 5 Vac/Vdc X 01/ Black 28 Vdc 5 Vac/Vdc X X 01/ Gray 28 Vdc 5 Vac/Vdc X X 01/ Black 28 Vdc 28 Vdc 01/ Gray 28 Vdc 28 Vdc 01/ Black 28 Vdc 28 Vdc X 01/ Gray 28 Vdc 28 Vdc X 01/ Black 28 Vdc 28 Vdc X X 01/ Gray 28 Vdc 28 Vdc X X 01/ Black 28 Vdc 5 Vac/Vdc X 02/ Gray 28 Vdc 5 Vac/Vdc X 02/ Black 28 Vdc 5 Vac/Vdc X X 02/03 Table 13 IVA-81A TA/RA/VSI Versions (Sheet 1 of 4) Page 14

58 HONEYWELL PART NUMBER VERSION NUMBER FACE PLATE PRIMARY POWER PANEL LIGHTING UP DN RANGE CONTROL TA SELECT SWITCH DIM (POT) SW IDENT Gray 28 Vdc 5 Vac/Vdc X X 02/ Black 28 Vdc 28 Vdc X 02/ Gray 28 Vdc 28 Vdc X 02/ Black 28 Vdc 28 Vdc X X 02/ Gray 28 Vdc 28 Vdc X X 02/ Black 115 Vac 5 Vac/Vdc X X 03/ Gray 115 Vac 5 Vac/Vdc X X 03/ Black 115 Vac 5 Vac/Vdc X X 04/ Gray 115 Vac 5 Vac/Vdc X X 04/ Black 28 Vdc 5 Vac/Vdc X X 04/ Gray 28 Vdc 5 Vac/Vdc X X 04/ Black 28 Vdc 28 Vdc X X 04/ Gray 28 Vdc 28 Vdc X X 04/ Black 28 Vdc 5 Vac/Vdc X 04/ Gray 28 Vdc 5 Vac/Vdc X 04/ Black 28 Vdc 5 Vac/Vdc X X 04/ Gray 28 Vdc 5 Vac/Vdc X X 04/ Black 28 Vdc 28 Vdc X 04/ Gray 28 Vdc 28 Vdc X 04/ Black 28 Vdc 28 Vdc X X 04/ Gray 28 Vdc 28 Vdc X X 04/ Black 115 Vac 5 Vac/Vdc X 04/ Gray 115 Vac 5 Vac/Vdc X 04/ Black 115 Vac 5 Vac/Vdc X X 04/ Gray 115 Vac 5 Vac/Vdc X X 04/ Black 115 Vac 5 Vac/Vdc X X 05/ Black 115 Vac 5 Vac/Vdc X X 06/01 Table 13 IVA-81A TA/RA/VSI Versions (Sheet 2) Page 15

59 SOFTWARE RANGE SELECTION OPTIONS BY SOFTWARE TYPE RANGE OPTION: 01/06 02/03 03/03 04/03 05/03 06/01 Fixed at 6.5 nm X X X X X X Fixed at 10.0 nm X X 3, 5, 10, 15 nm X X X Transponder Panel X X X X X X 5, 10, 20, 40 nm X X X 3, 5, 10, 20, 40 nm X 1, 3, 5, 10, 20, 40 nm X X Table 13 IVA-81A TA/RA/VSI Versions (Sheet 3) OPTIONS BY SOFTWARE TYPE FUNCTION: 01/06 02/03 03/03 04/03 05/03 06/01 RLS Capability X X Type A Flags/ MSGs X X BLS Compensation X X X X NVIS Compatible X X Day/Night Display X X NON-Standard ARINC 419 X X X E-TCAS Compatible X Vertical Speed m/sec X Strap selectable Dim Knob X X X X TSO d X X X X Table 13 IVA-81A TA/RA/VSI Versions (Sheet 4) Page 16

60 FEATURE Basic Unit Faceplate Primary Power Panel Lighting UP/DN Range Control TA SEL Switch BRT Control DESCRIPTION Displays resolution advisories, traffic advisories, and indicates vertical speed. Choice of faceplate colors Choice of 115 Vac or 28 Vdc versions Choice of 5 Vac/Vdc or 28 Vdc versions Pushbutton range control mounted on front panel of TA/RA/VSI display. The range control allows the selection of 1, 3, 5, 10, 15, 20, or 40 nautical mile display ranges. Specific ranges and range groups available are defined by the software version in use. Declutters all traffic symbols from display. If a TA or RA occurs, the All Traffic is automatically displayed. Allows manual adjustment of display brightness Table 14 IVA-81A TA/RA/VSI Features Page 17

61 CHARACTERISTIC DESCRIPTION Form Factor 3 ATI x 7.5 inches deep Components Solid state. No mechanical parts Physical Dimensions See Figure 2015 IVA 81A (TA/RA/VSI) Outline Drawing Weight See Figure 2015 IVA 81A (TA/RA/VSI) Outline Drawing Mounting Front, panel mount Primary Power 115 V 400 Hz, 22 W; or 28 Vdc, 29 W. Reference Power +/-12 Vdc reference power if altitude rate source input is ARINC 575 analog. 26 Vac reference power if altitude rate source input is ARINC 565 analog. Lighting Power 5 Vac or 5 Vdc, 195 ma; or 28 Vdc, 135 ma. Operating Temperature Range -15 C to + 70 C Number of Intruder Symbol 3-30 Maximum determined by TCAS processor program strap configuration. Display High resolution, full color dot matrix LCD. Combination vertical speed and traffic display. Vertical Speed Input The IVA-81A meets the requirements of both type B and type C VSI indicators, pneumatic or air data electrical input. Both ARINC 500 and 700 series air data input accepted. Data Input High-speed ARINC 429 Front-Mounted Range Control Optional Front-Mounted TA SEL Switch and BRT Optional Control Pneumatic Connector (Located on indicator rear panel) Electrical Connector (Located on indicator rear panel) TSO Environmental Certification See Figure 2002 IVA-81A/B/C/D Rear Connector Locations See Figure 2003 IVA-81A/B/C/D Electrical Connector Pin Locations C119a, C8c See Figure 16 IVA 81A/B Environmental Certification Categories Table 15 IVA-81A TA/RA/VSI Specifications Page 18