Honeywell KXP2290 AVIATION SERVICES TRANSMITTER User Manual 2290im
Honeywell International Inc. AVIATION SERVICES TRANSMITTER 2290im
USERS MANUAL
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| Document ID | 673211 |
| Application ID | agSaegBhX7xyXl82R7yY1A== |
| Document Description | USERS MANUAL |
| Short Term Confidential | No |
| Permanent Confidential | No |
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| Document Type | User Manual |
| Display Format | Adobe Acrobat PDF - pdf |
| Filesize | 63.07kB (788388 bits) |
| Date Submitted | 2006-06-26 00:00:00 |
| Date Available | 2006-08-10 00:00:00 |
| Creation Date | 2006-05-24 07:45:18 |
| Producing Software | Acrobat Distiller 7.0.5 (Windows) |
| Document Lastmod | 2006-05-24 13:11:47 |
| Document Title | 2290im.book |
| Document Creator | FrameMaker 6.0 |
| Document Author: | e050982 |
INSTALLATION MANUAL (Preliminary) KXP 2290 MODE S TRANSPONDER MANUAL NUMBER 006-10689-0000 REVISION 0 JUNE, 2006 THIS PUBLICATION MAY BE CONTROLLED BY THE U.S. DEPARTMENT OF STATE INTERNATIONAL TRAFFIC IN ARMS REGULATIONS (ITAR) 22 CFR 120-130 OR THE U.S. DEPARTMENT OF COMMERCE EXPORT ADMINISTRATION REGULATIONS (EAR), AND MAY NOT BE EXPORTED OUT OF THE UNITED STATE OR BE PROVIDED TO FOREIGN PERSONS (AS DEFINED BY THE ITAR) LOCATED WITHIN THE UNITED STATES, WITHOUT THE APPROPRIATE PRIOR AUTHORIZATIONS FROM THE U.S. GOVERNMENT. DIVERSION CONTRARY TO U.S. EXPORT LAWS AND REGULATIONS IS PROHIBITED. COPYRIGHT NOTICE ©2006 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, 23500 WEST 105th STREET OLATHE KS 66061 TELEPHONE: (913) 782-0400. n KXP 2290 REVISION HISTORY KXP 2290 KXP 2290 Installation Manual Part Number: 006-10689-XXXX For each revision, add, delete, or replace as indicated. Rev. 0c, June/2006 Preliminary 05/24/06 ITEM ACTION New manual No previous manual revision exists. Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page RH-1 n KXP 2290 THIS PAGE IS RESERVED Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page RH-2 n KXP 2290 TABLE OF CONTENTS ITEM PAGE SECTION I GENERAL INFORMATION 1.1 INTRODUCTION............................................................................................................ 1-1 1.2 EQUIPMENT DESCRIPTION ........................................................................................ 1-1 1.3 TECHNICAL CHARACTERISTICS ............................................................................... 1-2 1.3.1 KXP 2290 TECHNICAL CHARACTERISTICS............................................................... 1-2 1.3.2 ANTENNA ...................................................................................................................... 1-2 1.4 UNITS AND ACCESSORIES SUPPLIED ..................................................................... 1-3 1.4.1 CONFIGURATIONS AVAILABLE .................................................................................. 1-3 1.4.2 KXP 2290 INSTALLATION KIT...................................................................................... 1-3 1.5 ACCESSORIES REQUIRED, BUT NOT SUPPLIED .................................................... 1-4 1.6 LICENSING REQUIREMENTS...................................................................................... 1-5 1.7 CONTINUED AIRWORTHINESS INSTRUCTIONS ...................................................... 1-5 1.7.1 EQUIPMENT.................................................................................................................. 1-5 1.7.2 WIRES/COAX CABLES ................................................................................................. 1-5 SECTION II INSTALLATION 2.1 GENERAL INFORMATION ........................................................................................... 2-1 2.2 UNPACKING AND INSPECTING EQUIPMENT ........................................................... 2-1 2.3 EQUIPMENT INSTALLATION ...................................................................................... 2-1 2.3.1 GENERAL ...................................................................................................................... 2-1 2.3.2 KXP 2290 INTERCONNECTION AND CABLE HARNESS FABRICATION .................. 2-2 2.3.3 EQUIPMENT LOCATION .............................................................................................. 2-4 2.3.4 KXP 2290 INSTALLATION ............................................................................................ 2-5 2.3.5 CRIMP TOOL INFORMATION....................................................................................... 2-7 2.4 POST-INSTALLATION CHECKS................................................................................ 2-37 2.4.1 TRANSPONDER SYSTEM CHECKOUT..................................................................... 2-37 SECTION III OPERATION 3.1 GENERAL...................................................................................................................... 3-1 ENVIRONMENTAL QUALIFICATIONS APPENDIX Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page TC-1 n KXP 2290 Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page TC-2 n KXP 2290 PAGE ITEM FIGURE 2-1 FIGURE 2-2 FIGURE 2-3 FIGURE 2-4 FIGURE 2-5 FIGURE 2-6 FIGURE 2-7 FIGURE 2-8 FIGURE 2-9 FIGURE 2-10 FIGURE 2-11 FIGURE 2-12 MAIN CONNECTOR - JKXP2290-1 ............................................................. 2-9 KXP 2290 INSTALLATION DRAWING ...................................................... 2-11 KXP 2290 BAR CLAMP ASSEMBLY DRAWING....................................... 2-19 KA 61 INSTALLATION DRAWING............................................................. 2-21 KXP 2290 INTERCONNECTION DRAWING ............................................. 2-25 KXP 2290 INTERCONNECTION DRAWING ............................................. 2-27 RF CONNECTOR DRAWING .................................................................... 2-29 RG-400 CABLE CONNECTIONS DRAWING ............................................ 2-31 ECS/ECS-RG-400 CABLE CONNECTIONS DRAWING ........................... 2-32 CABLE CONNECTOR DRAWING ............................................................. 2-33 TYPE “N” AND “C” CONNECTOR ASSEMBLY DRAWING...................... 2-34 BNC CONNECTOR ASSEMBLY DRAWING ............................................. 2-35 Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page TC-3 n KXP 2290 Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page TC-4 n KXP 2290 PAGE ITEM TABLE 2-1 TABLE 2-2 TABLE 2-3 TABLE 2-4 SIZE 22 HIGH DENSITY D-SUB CONTACT TOOLS .................................. 2-7 JKXP2290-1 PIN FUNCTION LIST ............................................................. 2-9 ANTENNA CONNECTORS AND DESCRIPTIONS ................................... 2-10 INSPECTION/CHECK PROCEDURE ........................................................ 2-37 Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page TC-5 n KXP 2290 Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page TC-6 n KXP 2290 SECTION I GENERAL INFORMATION 1.1 INTRODUCTION This manual contains information relative to the physical, mechanical, and electrical characteristics of the Honeywell KXP 2290 Mode S Transponder. Installation and check out procedures are also included. Information relative to the maintenance, alignment, and procurement of the replacement parts may be found in the KXP 2290 Maintenance/Overhaul Manual, P/N 006-15689XXXX. The only current KXP 2290 installation option is as a part of the APEX system. The KXP 2290 is blind-mounted and shares a mounting rack with the KMC 2210 APEX controller. For additional information relating to the APEX system, refer to the APEX System Manual 006-10667XXXX. 1.2 EQUIPMENT DESCRIPTION The KXP 2290 is a Mode S Transponder that is capable of non-diversity or diversity operation. The KXP 2290 Mode S Transponder is designed to meet TSO-C112, ETSO-2C112a for a Class 2A ATCRBS/Mode Select Airborne Transponder System. It replies to ATCRBS Mode A and C, Intermode, and Mode S interrogations. Since the KXP 2290 is a Class 2A transponder, it can handle Comm A & Comm B Mode S data link protocols. The KXP 2290 is compliant with TSO-C112 Class 2A and ETSO-2C112a requirements. The EUROCAE ED-73B transponder functionality is Level 2 (Surveillance and Comm A/ B) and the marking is level 2s. Additionally the ED-73B defined class is "CLASS 1". The KXP 2290 is also designed to meet the Enhanced Surveillance mandated in Europe. The KXP 2290 has the ability to receive an 8-digit alphanumeric Flight ID code. The flight crew enters the Flight ID information via the APEX control panel. The KXP 2290 uses ARINC 735A TCAS interface protocol to interface with TCAS II. As a peripheral to the TCAS II processor, the transponder receives and replies to short and long Air-to-Air surveillance and TCAS Coordination interrogations. Also, it receives and replies to Ground-to-Air surveillance and Comm-A interrogations directed to TCAS. Top and bottom antennas provide the diversity option that allow compatibility with TCAS. The diversity option allows selection of signal receptions from either the top or the bottom antenna based on the characteristics of the received interrogation signals. This improves air-to-air surveillance and communication. An Optional top-mounted omnidirectional antenna is required for diversity. The KXP 2290 contains BITE (Built In Test Equipment) so the operational health of the unit is constantly monitored. When a critical fault is detected, the unit will notify the APEX system. The unit stores detected failures in non-volatile memory for later review. The unit also has a temperature sensor and a timer so that faults can be time stamped and temperature data can be collected and stored. Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 1-1 n 1.3 KXP 2290 TECHNICAL CHARACTERISTICS 1.3.1 KXP 2290 TECHNICAL CHARACTERISTICS TSO COMPLIANCE: TSO-C112, ETSO-2C112a SOFTWARE CERTIFICATION CATEGORY: RTCA/DO-178B SOFTWARE LEVEL “B” ENVIRONMENTAL CATEGORIES: SEE ENVIRONMENTAL QUALIFICATIONS APPENDIX PHYSICAL DIMENSIONS: SEE FIGURE 2-2 KXP 2290 INSTALLATION DRAWING WEIGHT: SEE FIGURE 2-2 KXP 2290 INSTALLATION DRAWING MOUNTING: BLIND-MOUNT (SHARES RACK WITH KMC 2210) TEMPERATURE: SEE ENVIRONMENTAL QUALIFICATIONS APPENDIX ALTITUDE: SEE ENVIRONMENTAL QUALIFICATIONS APPENDIX COOLING: NO FORCED-AIR COOLING REQUIRED. POWER INPUT: 18-32 VOLTS, 30 WATTS 1.3.2 ANTENNA The KXP 2290 will work with any conventional ATCRBS blade or quarter-wave monopole type antenna provided it is certified to TSO-C112/ETSO-2C112a A representative type is the Honeywell KA 61 antenna, P/N 071-00221-0010 (BNC) or 071-00221-0020 (TNC). Refer to FIGURE 2-4 KA 61 INSTALLATION DRAWING for KA 61 technical characteristics, installation, and certification information. NOTE: Two antennas (top and bottom) are required for diversity operation. Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 1-2 n 1.4 1.4.1 KXP 2290 UNITS AND ACCESSORIES SUPPLIED CONFIGURATIONS AVAILABLE P/N 066-01198-0101 is the only version of the KXP 2290 that is currently available. 1.4.2 KXP 2290 INSTALLATION KIT The KXP 2290 Transponder shares a mounting rack with the KMC 2210 APEX controller; therefore, installation kits P/N 050-03683-0000 and P/N 050-03670-0000 are both required to install the KXP 2290. Installation kit P/N 050-03683-0000 contains the following parts: PN DESCRIPTION REV ----------------------------------------------------------------------050-03683-0000 KXP 2290 INSTALLATION KIT ------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0000 ------------------------------------------------------------------------------------------------J1 030-03296-0000 HI DENSITY SUBD44P EA 1.00 J2 030-00101-0002 PANEL MOUNT PLUG EA 1.00 J3 030-00101-0002 PANEL MOUNT PLUG EA 1.00 001-01299-0000 INSTRUCTION FOR HARNESS ASSEMBLY PARTS RF .00 030-01466-0001 CONN, D-SUB, CONTACT, 22AWG, CRIMP, FEMALE EA 44.00 047-11179-0002 STRAIN RELIEF CLAMP MED EA 1.00 057-05944-0060 KIT TSO LABEL, KXP 2290 EA 1.00 073-01076-0004 BACK PLATE W/HARDWARE EA 1.00 073-01120-0002 SUB-D25 BACKSHELL W/FINISH EA 1.00 073-01121-0002 SUB-D25 BACKSHELL COVER W/FINISH EA 1.00 076-03189-0001 SCREW 100DEG FHP 2-56 X 3/8 SPECIAL EA 4.00 089-05903-0004 SCR PHP 4-40X1/4 EA 2.00 089-06008-0004 SCR FHP 4-40X1/4 EA 2.00 089-08303-0000 WASHER EA 2.00 090-00019-0007 RING RTNR .438 EA 2.00 155-01786-0000 INSTALLATION DRAWING KMC 2210/KXP2290 RF .00 200-10452-0000 BAR CLAMP ASSEMBLY -25 EA 1.00 Installation kit P/N 050-03670-0000 contains the following parts: PN DESCRIPTION REV ----------------------------------------------------------------------050-03670-0000 KMC 2210 INSTALLATION KIT ------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0000 ------------------------------------------------------------------------------------------------J1 030-03296-0006 CONN, D-SUB, RECPT, HSNG, SN PLATE, 26 POS EA 1.00 001-01299-0000 INSTRUCTION FOR HARNESS ASSEMBLY PARTS RF .00 030-01466-0001 CONN, D-SUB, CONTACT, 22AWG, CRIMP, FEMALE EA 26.00 047-11179-0002 STRAIN RELIEF CLAMP MED EA 1.00 047-12880-0006 RACK WITH HARDWARE EA 1.00 057-05944-0054 TSO LABEL KMC 2210 EA 1.00 073-01118-0002 SUB-D15 BACKSHELL W/FINISH EA 1.00 073-01119-0002 SUB-D15 BACKSHELL COVER W/FINISH EA 1.00 076-03189-0001 SCREW 100DEG FHP 2-56 X 3/8 SPECIAL EA 4.00 076-03192-0001 SCREW, 100DEG FHP 4-40 X 3/8 EA 2.00 076-03193-0001 SPACER, W/FINISH EA 2.00 155-01786-0000 INSTALLATION DRAWING KMC 2210/KXP2290 RF .00 200-10452-0001 BAR CLAMP ASSEMBLY -15 EA 1.00 Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 1-3 n KXP 2290 Shield braids must be clamped to the connector backshell using bar clamp assembly P/N 20010452-0000 which contains the following parts. See FIGURE 2-2 KXP 2290 INSTALLATION DRAWING and FIGURE 2-3 KXP 2290 BAR CLAMP ASSEMBLY DRAWING for additional information. PN DESCRIPTION REV ----------------------------------------------------------------------200-10452-0000 BAR CLAMP ASSEMBLY -25 ------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0000 ------------------------------------------------------------------------------------------------REF1 300-10452-0000 BAR CLAMP ASSEMBLY KMC 2220 RF .00 047-11178-0001 BACKSHELL BAR CLAMP LONG EA 1.00 076-03190-0001 SCREW PHP 4-40 X 7/16 SPECIAL EA 2.00 187-01943-0001 BACKSHELL GASKET LONG EA 1.00 1.5 ACCESSORIES REQUIRED, BUT NOT SUPPLIED Each antenna will require a connector and a length of coaxial cable to connect it to the KXP 2290 transponder. NOTE: Connector 030-00101-0002, which accommodates RG-400 cable, is included in the installation kit. Connector P/N 030-00102-0001 is for larger diameter cables i.e. P/N 024-00072-0000 and is not included. NOTE: The transmission line loss design value for the KXP 2290 is 0.5 to 2.0 dB. Total line loss between the unit and the antenna must be within this specification. The following are three antenna cable connection options for the KXP 2290; however, they may not have line loss specifications within tolerance in all installations. Refer to (8) Antenna Transmission Line Loss Considerations in SECTION II INSTALLATION for specific cabling information and to ensure a proper line loss value. Use the following parts for installations using FIGURE 2-8 RG-400 CABLE CONNECTIONS DRAWING. HONEYWELL PART NUMBER DESCRIPTION QUANTITY 030-00101-0002 Connector, Coax 024-00051-0060 Cable,Coax 11 ft. 030-00005-0000 Connector, Coax Mod Type BNC Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 1-4 n KXP 2290 Use the following parts for installations using FIGURE 2-9 ECS/ECS-RG-400 CABLE CONNECTIONS DRAWING. (ECS cable only) HONEYWELL PART NUMBER DESCRIPTION QUANTITY 030-00102-0001 Connector, Type Unit 024-00072-0000 Cable,Coax 25 ft. 030-00435-0000 Connector, Antenna Use the following parts for installations using FIGURE 2-9 ECS/ECS-RG-400 CABLE CONNECTIONS DRAWING. (ECS cable with RG-400 cable). HONEYWELL PART NUMBER DESCRIPTION QUANTITY 030-00101-0002 Connector Type Unit 024-00051-0060 Cable, Coax 6 in. 024-00071-0000 Cable, Coax 32.5 ft. 030-00138-0000 Connector, Unit extension to antenna connector 6 in. 030-00434-0000 Connector, Antenna 1.6 LICENSING REQUIREMENTS This equipment has been type accepted by the FCC and entered on the type accepted equipment list, as FCC ID: ASYKXP2290??. For non-US registered aircraft, follow applicable licensing requirements as required. 1.7 1.7.1 CONTINUED AIRWORTHINESS INSTRUCTIONS EQUIPMENT FAA requires that transponders, including the KXP 2290, be tested and inspected and found to comply with Federal Aviation Regulation (FAR) Appendix F of Part 43 of chapter 91.413, ATC transponder tests and inspections This requirement is applicable previous to or at the time of installation of a new unit and again at two year intervals for any unit. Other than the FAR noted above, there are no periodic service requirements necessary to maintain continued airworthiness. No maintenance is required until the equipment does not properly perform its intended function. When service is required, a complete performance test should be accomplished following any repair action. Consult the appropriate unit Maintenance/Overhaul Manual for complete performance test information. 1.7.2 WIRES/COAX CABLES During on-condition or regularly scheduled maintenance, inspect the wires and coax cables following the guidelines listed in AC 43,13-1 Chapter 15 as necessary. Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 1-5 n KXP 2290 THIS PAGE IS RESERVED Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 1-6 n KXP 2290 SECTION II INSTALLATION 2.1 GENERAL INFORMATION This section contains suggestions and factors to consider before installing the KXP 2290 Mode S Transponder. Close adherence to these suggestions will assure a more satisfactory performance from the equipment. The conditions and test 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. 2.2 UNPACKING AND INSPECTING EQUIPMENT Exercise extreme caution when unpacking the unit. Make a visual inspection of the unit for evidence of damage incurred during shipment. If a claim for a damage is to be made, save the shipping container to substantiate the claim. When all equipment is removed, place all packing materials in the shipping container for future storage or reshipment of the unit. 2.3 2.3.1 EQUIPMENT INSTALLATION GENERAL The following paragraphs contain information pertaining to the initial installation of the KXP 2290 Mode S Transponder, including instructions concerning the location and mounting of the supporting antenna(s). The equipment should be installed in the aircraft in a manner consistent with acceptable workmanship and engineering practices and in accordance with the instructions set forth in this publication. To ensure that the system has been properly and safely installed in the aircraft, the installer should make a through visual inspection and conduct an overall operational check of the system on the ground prior to flight. CAUTION: AFTER INSTALLATION OF THE CABLING AND BEFORE INSTALLATION OF THE EQUIPMENT, A CHECK SHOULD BE MADE WITH THE AIRCRAFT PRIMARY POWER SUPPLIED TO THE MOUNTING CONNECTOR TO ENSURE THAT POWER IS APPLIED ONLY TO THE PINS SPECIFIED IN THE INTERCONNECTION DRAWING, FIGURE 2-5 KXP 2290 INTERCONNECTION DRAWING. Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-1 n KXP 2290 The installation should be installed in accordance with standards established by the customer’s installing agency and existing conditions as to unit location and type of installation. However, the following suggestions should be considered before installing the system. Close adherence to these suggestions will assure a more satisfactory performance from the equipment. The installing agency will supply and fabricate all external cables. The connectors required are supplied by Honeywell. NOTE: The TSO identifies the minimum performance standards, tests, and other conditions applicable for issuance of design and production approval of the article. The TSO applicant is responsible for documenting all limitations and conditions suitable for installation of the article. An applicant requesting approval for installation of the article within a specific type or class of product is responsible for determining environmental and functional compatibility. 2.3.2 KXP 2290 INTERCONNECTION AND CABLE HARNESS FABRICATION 2.3.2.1 General The KXP 2290 Mode S Transponder receives primary power from the aircraft power source. Power connections, voltage requirements, and circuit breaker requirements are shown on the interconnect diagrams (FIGURE 2-5 KXP 2290 INTERCONNECTION DRAWING). The length of the wires to parallel pins should be approximately the same length, so that the best distribution of current can be effected. Honeywell recommends that all wires, including spares as shown on the interconnect diagram be included in the fabrication of the wiring harness. However; if full wiring is not desired, the installer should ensure that the minimum wiring requirements for the features and functions to be used have been incorporated. When cables are installed in the aircraft, they must be supported firmly enough to prevent movement and should be carefully protected against chaffing. Additional protection should also be provided in all locations where the cable may be subjected to abuse. In wire bundles, the cabling should not be tied tightly together as this tends to increase the possibility of noise pickup and similar interference. When routing cables through the aircraft the cables should cross high level rf lines at right angles. Prior to installing any equipment, make a continuity check of all wires and cables associated with the system. Then apply power and check for proper voltages at system connectors, and then remove power before completing the installation. Please note the following guidelines: (1) The installing facility will supply and fabricate all external cables. The required connectors are supplied as part of the installation kit (P/N 050-03451-0000). (2) The KXP 2290 must be kept a minimum of three feet from the antenna(s). Additionally, the antenna coax cable(s) should not be bundled with the other wiring harnesses to the KXP 2290. Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-2 n KXP 2290 (3) The length and routing of the external cables must be carefully planned before attempting the actual installation. Avoid sharp bends or locating the cable near aircraft control cables. The cables should be of a length to allow for a “maintenance loop”. That is, the length should be adequate to access and extend the connectors aft of the panel for future maintenance purposes. Excess cabling should be secured and stowed by tie-wrapping until such maintenance is required. (4) The cables should be supported firmly enough to prevent movement. They should be carefully protected wherever one may chafe against another or against some other object. Extra protection should be provided in all locations where the cables may be subject to abuse. Shields on shielded wires should be grounded as shown on the system interconnection diagrams. (5) Shields should be carried through any obstruction via a thru-bulkhead connector. If shielding cannot be carried through by use of a bulkhead/connector pin, precautions should be taken to ensure each segment of the shielded lead be grounded at only one point. A ground connection of not more than two inches in length should be used. The preceding discussion does not apply to coaxial and quadraxial cable. (6) Avoid routing cabling near high noise and high power sources. (7) Do not route the transponder antenna coax(s) near ADF sense or loop antenna cables. (8) Antenna Transmission Line Loss Considerations NOTE: The total losses in the coaxial cable run and interconnects between the antenna(s) and the KXP 2290 transponder must not be less than 0.5 dB and must not be more than 2.0 dB at 1030MHz. NOTE: The antenna cabling information noted in this section, in particular by FIGURE 2-8 RG-400 CABLE CONNECTIONS DRAWING, FIGURE 2-9 ECS/ ECS-RG-400 CABLE CONNECTIONS DRAWING, FIGURE 2-10 CABLE CONNECTOR DRAWING, FIGURE 2-11 TYPE “N” AND “C” CONNECTOR ASSEMBLY DRAWING, and FIGURE 2-12 BNC CONNECTOR ASSEMBLY DRAWING, is provided as possible antenna connection solutions and is provided for reference only. While the options noted in the figures will be applicable to many installations, adherence to the following sub-sections will ensure that the total cable/interconnection losses are within specification. Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-3 n KXP 2290 (a) Consult manufacturer’s coaxial cable data sheet specifications. Using the length of the top and/or bottom antenna cables and the manufacturer specified dB loss per foot of cable type, select a particular type or types of cable that meet the top and bottom cable loss limitations. In anticipation of aging factors, it is advisable to select a cable type that has an insertion loss that when combined with interconnect losses will equal a dB loss significantly lower than 2 dB. (b) In diversity installations, it is conceivable that the type of cable selected to meet the dB loss requirements of the top antenna cable will be different than the type of cable selection required to meet the dB loss requirements of the bottom antenna. For example: if the antenna run to one antenna is relatively lengthy, and the antenna run to the other antenna is relatively short, the longer run may require low loss antenna cable to meet the less than 2 dB antenna cable/interconnect requirement while the short run may require a relatively higher loss cable to exceed the 0.5 dB antenna cable/interconnect loss requirement NOTE: For installations with diversity transponder antennas (top and bottom) the cable lengths must be within 10 feet of each other. (c) 2.3.2.2 Consult manufacturer’s data sheets to determine the nanosecond delay per foot (at 1030 MHz) for the type or types of cable selected. Primary Power and Circuit Breaker Requirements and Wiring The KXP 2290 transponder receives primary power from the aircraft power circuit breakers. The KXP 2290 is designed to operate over the range of 18-32V dc. Power connections, wire sizes, and circuit breaker requirements are shown on the interconnection diagrams FIGURE 2-5 KXP 2290 INTERCONNECTION DRAWING. 2.3.3 EQUIPMENT LOCATION 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 consistent with the TSO environmental limits. Refer to the mechanical installation drawing (FIGURE 2-2 KXP 2290 INSTALLATION DRAWING), cable and connector assembly diagrams (FIGURE 2-7 RF CONNECTOR DRAWING, FIGURE 28 RG-400 CABLE CONNECTIONS DRAWING, FIGURE 2-9 ECS/ECS-RG-400 CABLE CONNECTIONS DRAWING, FIGURE 2-10 CABLE CONNECTOR DRAWING, FIGURE 2-11 TYPE “N” AND “C” CONNECTOR ASSEMBLY DRAWING, FIGURE 2-12 BNC CONNECTOR ASSEMBLY DRAWING), interconnection drawing(s) (FIGURE 2-5 KXP 2290 INTERCONNECTION DRAWING), and connector pin assignments diagrams (FIGURE 2-1 MAIN CONNECTOR JKXP2290-1, TABLE 2-2 JKXP2290-1 PIN FUNCTION LIST) as required. Determine the mounting location for system components following the guidelines below. Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-4 n 2.3.3.1 KXP 2290 Transponder And Mounting Tray Locations The KXP 2290 Mode S Transponder shares a mounting tray with the Honeywell APEX KMC 2210 controller and is part of the APEX cockpit panel configuration. Except for antenna cables the lengths of the cables from the KXP 2290 transponder mounting tray connector to other system units are not critical because unit interfaces are designed with high impedance inputs, low impedance outputs, and low noise susceptibility characteristics. 2.3.3.2 Antenna(s) The antenna(s) should be well removed from other antenna projections, the engine(s), and propeller(s). It should also be well removed from landing gear doors, access doors, or other openings which will break the ground plane for the antenna(s). The surface directly beneath the antenna(s) should be a flat plane over as large an area as possible. A back-up plate for each antenna should be used for added strength on thin-skinned aircraft. The antenna(s) need to be within 5 degrees of the centerline To prevent rf interference, the antenna(s) must be physically mounted a minimum distance of three feet from the KXP 2290 and the wiring harness. The transponder antenna(s) should be mounted a minimum of 30 inches away from the TCAS or DME antennas and four feet from the ADF sense antenna. Where practical, plan the antenna location(s) to keep cable lengths as short as possible and avoid sharp bends in the cable to minimize the VSWR. Avoid running other cables or wires near the antenna cable(s). On pressurized aircraft, the antenna(s) should be sealed using an approved sealant, such as RTV No. 3145 (P/N 016-01082-0000) or equivalent, around the connector and mounting hardware. The antenna mounting(s) should be sealed from the outside for moisture protection using RTV or equivalent. Mount the antenna(s) in as clean as environment as possible, away from exhaust gases and oils. The antenna(s) should be kept clean. If left dirty (oil covered), the range of the transponder may be affected. For installations with diversity transponder antennas (top and bottom) the distance between the top and bottom antennas on the horizontal plane of the aircraft fuselage must not exceed 25 feet (7.62m). 2.3.4 KXP 2290 INSTALLATION 2.3.4.1 General The mounting tray for the transponder/control unit should be mounted using the dimensions specified in the outline and mounting drawing, FIGURE 2-2 KXP 2290 INSTALLATION DRAWING. KXP 2290 wiring should be per the system interconnect diagram, FIGURE 2-5 KXP 2290 INTERCONNECTION DRAWING. 2.3.4.2 Transponder (1) Slide the transponder into the tray until the front lobe touches the mounting tray. (2) Turn the Allen wrench clockwise until the rear lobe engages the mounting tray slot. Continue turning the wrench clockwise until tight. CAUTION: DO NOT OVERTIGHTEN THE LOCKING FASTENER Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-5 n (3) KXP 2290 For removal, turn the 3-32 inch Allen wrench counter-clockwise until the unit disengages from the mounting tray slot. If all connectors are removed, the unit can be pulled completely out of the rack. For additional KXP 2290 installation information, refer to FIGURE 2-2 KXP 2290 INSTALLATION DRAWING as required 2.3.4.3 Aircraft Address Programming Options The Mode S aircraft address and maximum airspeed data must be programmed for use for the KXP 2290. This information is received from the APEX system via the ARINC 429 bus. NOTE: THE AIRCRAFT MODE S ADDRESS MUST BE OBTAINED FROM FAA AND PROGRAMMED INTO THE KXP 2290. FOR US REGISTERED AIRCRAFT, THE ICAO AIRCRAFT ADDRESS CODE CAN BE FOUND ON THE AIRCRAFT REGISTRATION. AIRCRAFT MODE S ADDRESSES MAY BE OBTAINED BY CALLING THE FAA AIRMAN AND AIRCRAFT REGISTRY DIVISION AT (405)-954-3116. IF THREE (3) OR MORE ADDRESSES ARE NEEDED, WRITE TO AIRCRAFT REGISTRATION BRANCH, ANV-450, P.O. BOX 25082, OKLAHOMA CITY, OK 73125. 2.3.4.4 Antenna For KA 61 antenna installation information, refer to FIGURE 2-4 KA 61 INSTALLATION DRAWING. For other L-band blade antenna outline drawings, installation procedures, and mounting dimensions, refer to the manufacturer’s instructions. Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-6 n 2.3.5 KXP 2290 CRIMP TOOL INFORMATION The following is a listing of crimp tools and accessories for use with the KXP 2290. SOURCE * CRIMP TOOL HONEYWELL 005-02012-0034 Not Available Not Available MIL-SPEC M22520/2-01 M22520/2-06 M81969/1-04 *** DANIELS MFG. AFM8 (M22520/2-01) K41 (M22520/2-06) POSITRONICS 9507-0-0 9502-3 (K41) ASTRO (BUCHANAN) 615717 (M22520/2-01) 615722 (M22520/2-06) ** *** POSITIONER 22-30 AWG ** INSERTION/EXTRACTION TOOL All source tools and positioners are to Mil-Spec Standard and are interchangeable. Positioner wire gauge (AWG) refers to barrel only. SUPERCEDES MIL SPEC P/N M24308/18-1. ORDER FROM POSITRONICS, DANIELS, OR ASTRO BY MIL SPEC P/N. NOTE: Selections in parentheses denote optional ordering number from source. Vendor Ordering Information: Astro Tool Company 21615 SW TV Hwy, Beaverton, OR 97006 (503) 642-9853 * Fax: 503-591-7766 * Email: sales@astrotool.com Daniels Manufacturing Company (DMC) 526 Thorpe Road, Orlando, FL 32824-8133 USA Tel: 407-855-6161 * Fax: 407-855-6884 * Email: dmc@dmctools.com Positronics Industries, Inc. 423 N. Campbell Ave P.O. Box 8247, Springfield, MO 65801 Tel: 800-641-4054 * Fax: 417-866-4115 * Email: info@connectpositronics.com TABLE 2-1 SIZE 22 HIGH DENSITY D-SUB CONTACT TOOLS Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-7 n KXP 2290 THIS PAGE IS RESERVED Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-8 n KXP 2290 FIGURE 2-1 MAIN CONNECTOR - JKXP2290-1 Front View Pin # I/O Description Specification +28 Vdc Power In Aircraft Power +18 to +32 Vdc Ext Standby ~ Discrete input. GND (< 10 ohms-to-ground) on this pin forces the unit to Standby. Resistance-toground > 100K on this pin keeps the present mode. TCAS 429 RX - A TCAS II compatibility Spare 1 429 RX - A Reserved Spare 2 429 RX - A Reserved Spare 3 429 RX - A Reserved XPDR 1/2 Reserved Serial Data In Reserved Serial Clk Reserved 10 Conc 429 RX - A Concentrated A429 input bus 11 Spare 4 429 RX - A Reserved 12 GPS 1 429 RX - A GPS ARINC 429 input 13 GPS 2 429 RX - A GPS ARINC 429 input 14 GP 2 429 TX - B Reserved 15 GP 2 429 TX - A Reserved 16 +28 Vdc Power Return Aircraft Ground 17 +28 Vdc Power In Aircraft Power +18 to +32 Vdc 18 TCAS 429 RX - B TCAS II compatibility 19 Spare 1 429 RX - B Reserved 20 Spare 2 429 RX - B Reserved 21 Spare 3 429 RX - B Reserved 22 RS232 Return Reserved TABLE 2-2 JKXP2290-1 PIN FUNCTION LIST Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-9 n Pin # KXP 2290 I/O Description Specification 23 Ext Ident Reserved 24 Ext Air/Gnd Reserved 25 Conc 429 RX - B Concentrated A429 input bus 26 Spare 4 429 RX - B Reserved 27 GPS 1 429 RX - B GPS ARINC 429 input 28 GPS 2 429 RX - B GPS ARINC 429 input 29 GP 1 429 TX - B General Purpose A429 output bus 30 GP 1 429 TX - A General Purpose A429 output bus 31 +28 Vdc Power Return Aircraft Ground 32 GPS Mark 1 - A GPS Time Mark for precision ADS-B 33 GPS Mark 1 - B GPS Time Mark for precision ADS-B 34 GPS Mark 2 - A GPS Time Mark for precision ADS-B 35 Serial Data Out Reserved 36 GPS Mark 2 - B GPS Time Mark for precision ADS-B 37 XPDR 1/2 Parity Reserved 38 + 3.3 Vdc Reserved 39 EXT EEPROM CS Reserved 40 RS232 Diag - RX Diagnosis Input 41 RS232 Diag - TX Diagnosis Output 42 I/O ARINC Supr I-O As an input: voltage >= 18 V and <= 70 V will cause suppression. A steady state voltage >= 18 V will cause the suppression to cease. As an output: this pin will go >= 18 V when the transponder transmits. This line conforms to ARINC 718A Attachment 6. 43 TCAS 429 TX - A TCAS II compatibility 44 TCAS 429 TX - B TCAS II compatibility TABLE 2-2 JKXP2290-1 PIN FUNCTION LIST NOTE: Do not connect to pins marked “Reserved” as the functionality is for future application. Connector Pin I/O Description JKXP2290-2 J2 I/O RX/TX Port - Bottom Antenna (BNC) JKXP2290-3 J3 I/O RX/TX Port - Top Antenna (BNC) TABLE 2-3 ANTENNA CONNECTORS AND DESCRIPTIONS Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-10 n KXP 2290 FIGURE 2-2 KXP 2290 INSTALLATION DRAWING (Dwg. 155-01786-0000 Rev. B, Sheet 1 of 4) Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-11 n KXP 2290 FIGURE 2-2 KXP 2290 INSTALLATION DRAWING (Dwg. 155-01786-0000 Rev. B, Sheet 2 of 4) Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-13 n KXP 2290 FIGURE 2-2 KXP 2290 INSTALLATION DRAWING (Dwg. 155-01786-0000 Rev. B, Sheet 3 of 4) Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-15 n KXP 2290 FIGURE 2-2 KXP 2290 INSTALLATION DRAWING (Dwg. 155-01786-0000 Rev. B, Sheet 4 of 4) Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-17 n KXP 2290 FIGURE 2-3 KXP 2290 BAR CLAMP ASSEMBLY DRAWING (300-10452-0000, Rev. -) Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-19 n KXP 2290 FIGURE 2-4 KA 61 INSTALLATION DRAWING (Sheet 1 of 2) Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-21 n KXP 2290 FIGURE 2-4 KA 61 INSTALLATION DRAWING (Sheet 2 of 2) Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-23 n KXP 2290 FIGURE 2-5 KXP 2290 INTERCONNECTION DRAWING (Dwg. 155-0xxxx-000x Rev. -, Sheet 1 of 2) Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-25 n KXP 2290 FIGURE 2-6 KXP 2290 INTERCONNECTION DRAWING (Dwg. 155-0xxxx-000x Rev. -, Sheet 2 of 2) Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-27 n KXP 2290 FIGURE 2-7 RF CONNECTOR DRAWING Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-29 n KXP 2290 FIGURE 2-8 RG-400 CABLE CONNECTIONS DRAWING (Option For Short Antenna Cable Lengths) Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-31 n KXP 2290 FIGURE 2-9 ECS/ECS-RG-400 CABLE CONNECTIONS DRAWING (Options For Longer Antenna Cable Lengths) Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-32 n KXP 2290 FIGURE 2-10 CABLE CONNECTOR DRAWING Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-33 n PART NUMBER KXP 2290 SIZE RG/U CABLE DIMENSION 024-00075-0000 393 9/32 1/8 5/32 3/64 024-00051-0060 400 9/32 1/8 5/32 3/64 FIGURE 2-11 TYPE “N” AND “C” CONNECTOR ASSEMBLY DRAWING Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-34 n KXP 2290 FIGURE 2-12 BNC CONNECTOR ASSEMBLY DRAWING Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-35 n KXP 2290 THIS PAGE IS RESERVED Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-36 n 2.4 KXP 2290 POST-INSTALLATION CHECKS 2.4.1 TRANSPONDER SYSTEM CHECKOUT The post-installation test is used to apply power and functionally checkout the system. Successful completion of the post-installation test verifies the proper operation of the KXP 2290 Mode S Transponder System. TABLE 2-4 INSPECTION/CHECK PROCEDURE is a visual inspection/check procedure that should be performed after system installation as part of a system checkout. A post-installation test per paragraph 2.4.1.2 Post-Installation Checkout/Operation should be performed. In addition, the procedure should be used as a periodic maintenance inspection check. EQUIPMENT INSPECTION/CHECK PROCEDURE KXP 2290 Mode S A. Inspect external surface for damage. Transponder B. Check that the unit is securely installed and that retaining mechanism is securely tightened. C. Ensure that all connections in the mounting tray are properly mounted and secure. Antennas A. Inspect external surfaces for damage. B. Check that antenna is properly mounted and mounting screws are tight. C. Ensure that antenna coaxial cable connectors are properly mated and secure. TABLE 2-4 INSPECTION/CHECK PROCEDURE 2.4.1.1 Inspection Perform the following inspection on the overall system: (1) Check that cables do not interfere with aircraft controls or other equipment. (2) Check cabling for proper routing and check security of tie-down points. Inspect and adjust cable runs to ensure that cables are not strained, kinked, or severely twisted and are not exposed to rough or sharp surfaces. 2.4.1.2 Post-Installation Checkout/Operation (1) General Installation of the transponder system requires three stages of testing to ensure the proper operation of the Mode S transponder. Initially, prior to the installation of the transponder and antenna, a system interwiring check should be performed. This check verifies that the aircraft and all transponder interconnections are correct, before power is applied. After the units are installed a visual inspection of the equipment and connections is made. Finally, a post-Installation test is performed. Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-37 n (2) KXP 2290 System Interwiring Check To check the aircraft and transponder system interconnections proceed as follows: (3) (a) Check that all cables and interwiring are installed in accordance with the Interwiring and Cable Harness Fabrication instructions (paragraph 2.3.2 KXP 2290 INTERCONNECTION AND CABLE HARNESS FABRICATION). (b) Using the interconnect diagram (see FIGURE 2-5 KXP 2290 INTERCONNECTION DRAWING), check wiring for proper destination, opens, and shorts. (c) Check rf cables for insertion loss and VSWR. Visual Inspection In conjunction with system installation, perform the inspection/check procedure (TABLE 2-4 INSPECTION/CHECK PROCEDURE). (4) Post-Installation Test Perform the ATC transponder tests and inspections noted in section 1.7.1 EQUIPMENT (per Federal Aviation Regulation Part 43). Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 2-38 n KXP 2290 SECTION III OPERATION 3.1 GENERAL The only current operational function of the KXP 2290 is as a part of the Honeywell APEX system. Consult the applicable APEX system operation handbook(s) as required. Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 3-1 n KXP 2290 THIS PAGE IS RESERVED Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page 3-2 n KXP 2290 ENVIRONMENTAL QUALIFICATIONS APPENDIX ENVIRONMENTAL QUALIFICATION FORM(S) Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page TSO-1 n KXP 2290 THIS PAGE IS RESERVED Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page TSO-2 n Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA KXP 2290 Page TSO-3 n Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA KXP 2290 Page TSO-4 n Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA KXP 2290 Page TSO-5 n KXP 2290 THIS PAGE IS RESERVED Rev. 0c, June/2006 Preliminary 05/24/06 10689I00.JA Page TSO-6
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