KFS-576A Maintenance Manual
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Description
MAINTENANCEMANUAL KFS 576A CONTROL UNIT Manual Number 006-15718-0000 Revision 0, Apr/2007 This document contains technical data and is subject to U.S. export regulations. These commodities, technology, or software were exported from the United States in accordance with the export administration regulations. Diversion contrary to U.S. law is prohibited. Honeywell - Confidential THIS DOCUMENT AND ALL INFORMATION AND EXPRESSION CONTAINED HEREIN ARE THE PROPERTY OF HONEYWELL INTERNATIONAL INC., ARE PROVIDED IN CONFIDENCE, AND MAY BE USED BY PERSONS REQUIRED BY FEDERAL AVIATION REGULATION PART 21.50 TO COMPLY WITH ANY OF THE TERMS OF THESE INSTRUCTIONS. EXCEPT AS SET FORTH ABOVE, NO PERSON MAY, IN WHOLE OR IN PART, USE, DUPLICATE OR DISCLOSE THIS INFORMATION FOR ANY PURPOSE WITHOUT THE PRIOR WRITTEN PERMISSION OF HONEYWELL INTERNATIONAL INC. KFS 576A Honeywell Materials License Agreement The documents and information contained herein ("the Materials") are the proprietary data of Honeywell International Inc. and Honeywell Intellectual Properties Inc (collectively "Honeywell"). These Materials are provided for the exclusive use of Honeywell Service Centers; Honeywell-authorized repair facilities; operators of Honeywell aerospace products subject to an applicable product support agreement, their wholly owned-subsidiaries or a formally designated third party service provider thereunder; and direct recipients of Materials from Honeywell's Aerospace Technical Publication Distribution. The terms and conditions of this License Agreement govern your use of these Materials, except to the extent that any terms and conditions of another applicable agreement with Honeywell regarding the operation, maintenance, or repair of Honeywell aerospace products conflict with the terms and conditions of this License Agreement, in which case the terms and conditions of the other agreement will govern. However, this License Agreement will govern in the event of a conflict between its terms and conditions and those of a purchase order or acknowledgement. 1. License Grant - If you are a party to an applicable product support agreement, a Honeywell Service Center agreement, or an authorized repair facility agreement, Honeywell hereby grants you a limited, non-exclusive license to use these Materials to operate, maintain, or repair Honeywell aerospace products only in accordance with that agreement. If you are a direct recipient of these Materials from Honeywell's Aerospace Technical Publication Distribution and are not a party to an agreement related to the operation, maintenance or repair of Honeywell aerospace products, Honeywell hereby grants you a limited, non-exclusive license to use these Materials to maintain or repair the subject Honeywell aerospace products only at the facility to which these Materials have been shipped ("the Licensed Facility"). Transfer of the Materials to another facility owned by you is permitted only if the original Licensed Facility retains no copies of the Materials and you provide prior written notice to Honeywell. 2. Rights In Materials - Honeywell retains all rights in these Materials and in any copies thereof that are not expressly granted to you, including all rights in patents, copyrights, trademarks, and trade secrets. No license to use any Honeywell trademarks or patents is granted under this License Agreement. 3. Confidentiality - You acknowledge that these Materials contain information that is confidential and proprietary to Honeywell. You agree to take all reasonable efforts to maintain the confidentiality of these Materials. 4. Assignment And Transfer - This License Agreement may be assigned to a formally designated service designee to the extent allowed under an applicable product support agreement or transferred to a subsequent owner or operator of an aircraft containing the subject Honeywell aerospace products. However, the recipient of any such assignment or transfer must assume all of your obligations under this License Agreement. No assignment or transfer shall relieve any party of any obligation that such party then has hereunder. 5. Copies of Materials - Unless you have the express written permission of Honeywell, you may not make or permit making of copies of the Materials. Notwithstanding the foregoing, you may make copies of only portions of the Material for your internal use. You agree to return the Materials and any copies thereof to Honeywell upon the request of Honeywell. Rev 0, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. MLA-1 KFS 576A 6. Term - This License Agreement is effective until terminated as set forth herein. This License Agreement will terminate immediately, without notice from Honeywell, if you fail to comply with any provision of this License Agreement or will terminate simultaneously with the termination or expiration of your applicable product support agreement, authorized repair facility agreement, or your formal designation as a third party service provider. Upon termination of this License Agreement, you will return these Materials to Honeywell without retaining any copies and will have one of your authorized officers certify that all Materials have been returned with no copies retained. 7. Remedies - Honeywell reserves the right to pursue all available remedies and damages resulting from a breach of this License Agreement. 8. Limitation of Liability - IN NO EVENT WILL HONEYWELL BE LIABLE FOR ANY INCIDENTAL DAMAGES, CONSEQUENTIAL DAMAGES, SPECIAL DAMAGES, INDIRECT DAMAGES, LOSS OF PROFITS, LOSS OF REVENUES, OR LOSS OF USE, EVEN IF INFORMED OF THE POSSIBILITY OF SUCH DAMAGES. TO THE EXTENT PERMITTED BY APPLICABLE LAW, THESE LIMITATIONS AND EXCLUSIONS WILL APPLY REGARDLESS OF WHETHER LIABILITY ARISES FROM BREACH OF CONTRACT, WARRANTY, TORT (INCLUDING BUT NOT LIMITED TO NEGLIGENCE), BY OPERATION OF LAW, OR OTHERWISE. 9. Controlling Law - This License shall be governed and construed in accordance with the laws of the State of New York without regard to the conflicts of laws provisions thereof. This license sets forth the entire agreement between you and Honeywell and may only be modified by a writing duly executed by the duly authorized representatives of the parties. Copyright - Notice Copyright 2007 Honeywell International Inc. All rights reserved. Rev 0, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. MLA-2 KFS 576A REVISION HIGHLIGHTS Part Number 006-15718-0000 Rev 0, Apr/2007 Rev 0 Date Apr/2007 Description Original Issue. ©Honeywell International Inc. Do not print without express permission of Honeywell. RH-1 KFS 576A REVISION HIGHLIGHTS Part Number Rev 0, Apr/2007 Rev Date Description ©Honeywell International Inc. Do not print without express permission of Honeywell. RH-2 . . . . .7 4. . . . . . DISPLAY CIRCUITRY . . . . . . .3. . . . . . . . Do not print without express permission of Honeywell. . . . . . . .1 4. . . .2. . . . . . . . . .2. . . GENERAL CIRCUIT THEORY. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2. . . . . . . . . . . . . . . . EEPROM . . . . .10 4. . . . . . . .3 4. . . . . . . . . . . . . . . . . . . . .1 5. . . . . .6 4. . . ALTITUDE INPUTS . . . . . . . . . . . . . . . . . . STROBE AND SERIAL DATA . . . . . . . . . . .5 4. . . EEPROM . . . . .3. . . . . . . . . . . MULTIPLEX AND DISPLAY CIRCUITRY . . . . . . . . . . . . .3. . . . . . . . .3. . . . .3. . . . . .2. HIGH VOLTAGE CURRENT LIMITER . . .3 4.2. . . . . . . . . . .2. . . . . . . . . . . . . . . . . . . . . . . . . . . . REPLY INPUT . . . . . . . . . . FINAL TEST . . . .2 4. . .1 4. . . . . . . .3. . . . . . . . . . . . . . . .4. . .3. . . . . . . . . . . . . .2. . . . . . . . . . . . . . . . ANODE AND CATHODE DRIVERS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .5 GENERAL INFORMATION . . . . . . . . . . . . . . . . . . DISPLAY . . . . . . . . . . 429 BUS.2 5. . . . . . . . . . . . . . .2. . . . . . . . . . . . . . . . . . . . CLOCK. . . . . . . . . . . . . . . . . . . . . . . . . .8 4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2 4. . . . . . . . . . . . . . . . . . . . .2. . . . . . . . . . . . . . . . . . . . . . . . . . . . AUTOMATIC DIMMING . . . . . . . . . . . . . . . .2. . . .4 4. . . CONTROL UNIT INPUTS . . . .3.2 5. . . . .2. . . . . . . . . . . . . . . . . . . . . . . . . . .3. . . . . . . . . . . .9 4. . . . FLIGHT LEVEL (FL) . . . . .1 4. . . . .1. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . IDENT . DESCRIPTION OF KFS 576A TEST PROGRAM .2. . . . . . . . . . . . . . .3. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . +5 VOLT REGULATOR . . . . MICROPROCESSOR RESET . . . . . . . . . . . . . . . . . . . . . . . . . .4. . . Apr/2007 ©Honeywell International Inc. .2. ON/OFF . . . . . . . . CODE SELECTOR SWITCH . . . . .4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . STROBE AND SERIAL DATA OUTPUTS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3. . . . . . . . . . . . . .3. . . . . . . . . . . . . . . . . . . .4 5. . . . . . . . . . . . .2. . . . . .2 4. 5-1 5-1 5-1 5-2 5-3 5-3 5-5 5-5 5-5 5-6 5-6 TOC-1 . . . . . CLOCK. . . TEST AND ALIGNMENT . . . . . . . . . . . . . . . . . . . . . . . . . . . . OPERATING VOLTAGES . . . . . . . 4-1 4-1 4-1 4-1 4-2 4-2 4-2 4-2 4-2 4-3 4-3 4-3 4-3 4-3 4-3 4-4 4-4 4-4 4-4 4-4 4-5 4-5 4-6 4-6 4-6 4-7 4-7 4-8 SECTION 5 MAINTENANCE 5. . . . . . . . . . .2. . . . .2 4. . . . . . . . . . . . . . . . TRANSPONDER SELECT SWITCH . . . . . . . . . .KFS 576A TABLE OF CONTENTS SECTION 4 THEORY OF OPERATION 4. . . . . . . . .6 4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2. . . . TEST EQUIPMENT REQUIRED . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .8 4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2 4. .1 4. . . .2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .7 4. . FUNCTION SWITCH . . . . .3 4. . . . . . . .3. . . . .3 5.2.2. . . . . . . . . .3. . . . . . . . . . . . . . . . . . . . .2.4. . . . . . .3 4. . . . . . . . . . . . . . . . . . . . . . . . . . . . .1 5. . . . . . .1 4. . . . . . . . . . . . . . . . . . . POWER SUPPLY. . . . . . . . .2. . . . . . .4. . . . .3. . . . . . . .2. . . . . . . . . . . . . . . . . . . . . SWITCH INPUTS. . . . . . .2. . . . . . . .4 5. . . . . . . . . . . . . . . .1 4. . . . . . . . . . . . . . . . . . . . . . . .2 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2. . . . . . . . . . . . . . . . . . . . . . . Rev 0. ALIGNMENT . . . . . . . . . . . .4 4. . . . .3 5. . . . . . .2 5. . . . . . . . . . . . . . . . 429 BUS . . . . . . . . IDENT SWITCH . . . . . . . . . . . . . . . . . . . . . . . .1. . DETAILED CIRCUIT THEORY . . .2. . . . . . . MODE A/B SELECT . . . . . . . . . . . . . . . .1 5. . .2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .5 4. . . .2. . . MICROPROCESSORS . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3. . . . . . . . . . . . . . . . . . . . . . . . . CODE SELECTOR SWITCH .3. . . . . . . . . . . . . .10 CONTROL DISABLE . . . . 6-1 BILL OF MATERIAL DESCRIPTION . . . . . . Apr/2007 ©Honeywell International Inc. . . . . . . . . . . . . . . . . . . . . . . .4. . . .2. 5-9 5. . .2. . .6 EMERGENCY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3. . . . . . . . . . . . . . .4.4. . . . . . . . . . . .15 UNIT STATUS . . . . . . . . . . . . . . . . .2. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4. . . .3 OVERHAUL . . . . . . . . . . . . . . . . . . . . . . . . . . .2 INTRODUCTION . . . . . . . . . . . . . . . . . . . . . . .2. . .4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . .3. . . . .4. . . . . . . . . 5-12 5.14 VFR CODE . . . . . . . . . . 5-7 5. . 6-1 Rev 0. . . . . .9 EXTERNAL STANDBY . . . . . . . . . . . . . . . . . . . . . . . . . . .1 COVER REMOVAL (047-5021-02) . . . . . . . 5-15 5. . . . . . . . . 5-7 5. . . . . . . .4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .12 CHANNELING . . . . . . . .3. . . . . . . . . . . . . .4 TROUBLESHOOTING .4. . . . . . . . . . . . . . . . . . . . . . . . . . .4. . . . . . . . . . 5-7 5. . . . . . . . . .5 ASSEMBLY . . . . .3 FRONT COVER/SWITCH BOARD REMOVAL (088-1166-XX/200-6589-XX) . . . .2. .11 NON VOLATILE MEMORY . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .KFS 576A TABLE OF CONTENTS 5. . . . . . . . . . 5-7 5.2. . .13 429 I/O . . . . . . 5-8 5. . . . . . 5-12 5. . . . . 5-16 5. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .2. . . . . . . . . . . . . . .16 FINAL TEST DATA SHEET . . . . . . . . . . . . . . . . . . . . . . . . . 5-14 5. . . . . . . . . . . . . . . . 5-16 SECTION 6 ILLUSTRATED PARTS LIST 6.4. 5-7 5. . . . . . . . . . . . . . . . . . .3.8 DIMMING . . . . . . . . . . . . . . . . . . . . . . 5-8 5. . .2. .4 DRIVER BOARD REMOVAL (200-6626-XX) . . . . . . 5-15 5. . . . . . .4. . . . . . .3. . . .7 REPLY . . . . . . . . . . . . . . . . . . . . . . .1 VISUAL INSPECTION . . . . . . . . . . . . . . . . . . . . . . . . . . . .2. . . . . . .4. . . . 5-15 5. . . . . . . . . . . . . . . . . . 5-15 5. . .4. . . . . . . . . . . . . . . .3. . . . . . . . . . . . . .1 6. 5-9 5. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-7 5. . . . . . . . . . . . . . . . . . . . . . TOC-2 . . . . . . . . . . . . . . . . . . . . . .4. . . . . . . . . . 5-16 5. . . .4. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .4 DISASSEMBLY . .4. . . . . . . . . . . . . . . . . . . . . . . . . . . .3. . . . . . . . . . .2. . . .2 MICROPROCESSOR BOARD REMOVAL (200-6580-XX) . . . . . .3. . . . . . . .3 REPAIR . . 5-10 5.2. . . . . . Do not print without express permission of Honeywell. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-43 Microprocessor Board Schematic . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-29 I/O Board . . . . . . . . . . . . 6-69 ©Honeywell International Inc. . . . . . . . . . . . . 6-31 I/O Board Schematic . . . . . . . . . . . 6-59 Driver Board . . . . . . . . . . . . . . . . . . . . . 6-67 Driver Board Schematic. . . . . . . . . . . 5-19 Typical Bill of Material . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-11 Waveform and Timing Diagram. . . . . . . . . . . . . . . . . . . . . . . . . 6-35 Microprocessor Board . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-65 Driver Board . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-15 Test Setup . . . . . . . . . . . . . . . 6-5 Final Assembly . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .KFS 576A LIST OF FIGURES Figure 4-1 Figure 4-2 Figure 4-3 Figure 4-4 Figure 5-1 Figure 5-2 Figure 5-2 Figure 6-1 Figure 6-2 Figure 6-3 Figure 6-4 Figure 6-5 Figure 6-6 Figure 6-6 Figure 6-7 Figure 6-8 Figure 6-9 Figure 6-10 Figure 6-11 Figure 6-12 Figure 6-13 Figure 6-14 Figure 6-15 Figure 6-16 Rev 0. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-55 Switch Board . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 4-14 Display Timing Diagram . . . . . 6-33 I/O Board Schematic . . . . . . . . . . . . . . . . . . . . 6-57 Switch Board Schematic . . . . . . . . . . . Do not print without express permission of Honeywell. . . . . . . . . 6-19 I/O Board . . 4-13 Serial Data. . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 6-45 Microprocessor Board Schematic . . . . . . . . . . . . . . 6-41 Microprocessor Board . . . 6-17 Final Assembly . 6-47 Switch Board . . . . . . . . . . . . . . . . . . . . . 5-17 KFS 576A Troubleshooting Flowchart. . . . . LOF-1 . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . 5-4 KFS 576A Troubleshooting Flowchart. . . . . . . . . . . . . . . . . Apr/2007 KFS 576A Block Diagram . . . . . . . . . . . . . . . . . Do not print without express permission of Honeywell. LOF-2 . Apr/2007 ©Honeywell International Inc.KFS 576A This Page Intentionally Left Blank Rev 0. When the transponder is replying. 4-1 . When the unit is designated a Master it initiates communications on the 429 bus. communicating status with an external unit via the 429 bus. Master/Slave select. Do not print without express permission of Honeywell. When it is a Slave it responds to interrogation on the 429 bus. Control Disable.1 INTRODUCTION The KFS 576A is the cockpit-mounted Control Unit for the KXP 756 Transponder.2. it sends a signal to the Control Unit causing an “R” to be illuminated on the display. The External Ident input permits a remotely mounted switch to perform the same function as the Ident Button on the Control Unit. Activating Control Disable disables all the switch functions except the VFR Code recall.2. External Standby and Reply input from the transponder. Mode A/Mode B select. Nomenclature on the display indicates the position of the Function Switch. These inputs are serialized and transmitted to the transponder. Apr/2007 ©Honeywell International Inc. Rev 0. 1/2 select. 4. Third. displaying the selected transponder code and mode of the transponder for the pilot via the gas-discharge display. When the External Standby input is active the unit keeps the transponder in Standby mode. First. The altitude inputs are provided by an encoding altimeter.1 CONTROL UNIT INPUTS The Control Unit signal inputs consist of the External Ident. ten altitude (Mode C) inputs. The 1/2 select input determines the unit designation in a dual unit system. Second. 4. Emergency.KFS 576A SECTION 4 THEORY OF OPERATION 4.2 GENERAL CIRCUIT THEORY 4.2 FUNCTION SWITCH The switch is continuously rotatable in both directions and is used to select the desired mode of operation of the transponder. When the Emergency input is active the code is replaced by 7700 when the cursor switch is held in for over 3 seconds. The Mode A/Mode B select input changes a bit in the serial data informing the transponder whether to reply to Mode A or Mode B interrogations. that of converting switch inputs and information from the optional encoding altimeter into a serial data format and sending it to the transponder. It performs three main functions. The same action results when the External Ident input is activated. To provide this feature an EEPROM is used. The data to be displayed on the cathodes is outputted synchronously with the clocking of the anodes. 4. Momentarily depressing the switch knob changes the position of the cursor.2. 4. Each anode is energized for approximately 1 out of every 8msec.3 CODE SELECTOR SWITCH This switch is continuously rotatable in both directions and is used to change the transponder reply code. The anodes of the display are energized sequentially. The Electrically Erasable Programmable Read Only Memory (EEPROM) “remembers” the transponder code when power is removed from the Control Unit. The KFS 576A is supplied in either a +5V or +28V bezel lighting version. -26. The +190V is used to drive the gas discharge display.3 and +190V for the KFS 576A are externally supplied by the KXP 756 transponder. The cursor moves from left to right only. +9.2. The IDT nomenclature on the display.2. A photodetector activates the automatic dimming circuit and is used to adjust the display brightness in response to variations in ambient light levels. lights for approximately 23 seconds to indicate the transmission to the SPI pulse. the transponder code will change to the VFR code and the cursor will return to the leftmost position.2.7 MULTIPLEX AND DISPLAY CIRCUITRY The KFS 576A uses a multiplexed gas-discharge display. The +9. regulator. This causes the transponder to transmit the SPI (Special Position Identification) pulse for approximately 23 seconds. 4-2 .4 IDENT SWITCH Pressing the Ident Switch results in an ident pulse being sent to the transponder via the serial data line. Rev 0. 4. The cursor points to the digit that will change when the Code Selector Switch is rotated.2.KFS 576A 4. Do not print without express permission of Honeywell. The code is automatically recalled from the EEPROM when power is applied to the Control Unit.3V input is used to generate the +5V source by means of an I. The -26V is regulated to -10V for the 429 circuitry.5 OPERATING VOLTAGES All operating voltages. If the Code Selector Switch is held in continuously for approximately 3 seconds. 4.C. Apr/2007 ©Honeywell International Inc.6 EEPROM An indicator without mechanical code selector switches is unable to “remember” its selected code when power is removed. The following table lists component designators and the schematics on which they are found: Component Designations Schematic 101-199 201-299 301-399 401-499 I/O Board Processor Board Driver Board Switch Board 4.1.9 TRANSPONDER SELECT SWITCH A Transponder Select Switch is installed on some versions of the KFS 576A and permits a single Control Unit to select one of two remote mounted transponders. The referenced schematics and timing diagrams should be used as an aid in understanding the theory. The Serial Data output contains all the information needed by the transponder to reply properly to an interrogation. 4. This switch does not affect the operation of the indicator in any way other than determining which transponder is operational. 4-3 . 4.10 429 BUS The 429 Bus is used to communicate Control Unit status with external units. Apr/2007 ©Honeywell International Inc. C311 provides filtering for the +5 volt line.3.8 CLOCK.KFS 576A 4. 4. Do not print without express permission of Honeywell. STROBE AND SERIAL DATA OUTPUTS As previously stated. 4.3 DETAILED CIRCUIT THEORY The following is a detailed description of the KFS 576A circuit operation. all information inputted to the Control Unit is sent to the transponder in a serial data format.1 +5 VOLT REGULATOR I307 uses the +9. Rev 0.2.2.1 POWER SUPPLY All operating voltages for the KFS 576A are externally provided (by the KXP 756 Transponder).3 volt input to provide a +5 volt regulated output that is used to power the logic devices in the Control Unit. The Strobe output indicates to the transponder the end of a valid sequence of serial data.2. The clock occurs only after a particular bit of data has stabilized on the Serial Data output causing the transponder to accept that particular bit of data.3. the IDENT bit of serial data is low. This provides protection for the anode and cathode drivers (I301.1. Rev 0.2 MICROPROCESSORS I202 and I203 are 8-bit. if the IDENT switch is pushed.5 volts it caused pin 1 of I204 to go low. Do not print without express permission of Honeywell. if the IDENT switch is not being pushed. I302 and I303) and the gas discharge display in the event of a momentary short inside the display. 4. The level of a particular bit. I203 subsequently causes the "R" nomenclature on the gas discharge to light indicating a transponder reply.3. 4-4 . each bit approximately 1 msec wide. The multiplexed output from I101 and I102 is sent to microprocessor I202 pin 39 via J102 pin 16.2.3 CLOCK. strobe and serial data waveforms. 4.2 REPLY INPUT When the transponder replies to an interrogation.3. Apr/2007 ©Honeywell International Inc.KFS 576A 4. Serial data is outputted from board 1 via board 2 to J5761-23.2. 4. A detailed description of the internal operation of the microprocessors or their interaction is not required for maintenance and is beyond the scope of this manual. Figure 4-3 Serial Data shows the serial data and the information associated with each bit. Proper microprocessor operation is best determined by inputting of specific information and checking to see that the proper output is present. STROBE AND SERIAL DATA Figure 4-2 Waveform and Timing Diagram shows typical clock. The ten lines are multiplexed by I101 and I102. the IDENT bit in the serial data is high. For example.2 HIGH VOLTAGE CURRENT LIMITER Q303 limits the current drawn from the +190 volt line to approximately 25mA. A time delay in I203 causes the "R" to remain lit for about 250 msec after the Reply input returns to the high state. either high or low. it sends a signal to the KFS 576A.3.2.3. Conversely. which pulls pin 1 of I203 low. This data consists of 32 continuously repeating bits of information. 4. The clock and strobe lines are used by the transponder to decode the serial data information.1 ALTITUDE INPUTS Ten input lines from an encoding altimeter supply altitude information to the Control Unit. represents some bit of information that must be sent from the KFS 576A to the transponder. This data is then serialized and outputted to the transponder. As this signal falls below 2. single chip microprocessors that control most of the operations in the Control Unit.3. The data bit level during the rising edge determines what value of data will be "seen" by the transponder.4 MODE A/B SELECT Grounding pin 9 of J5761 causes the A/B bit of the serial data to go low.5 429 BUS When 429 data is received on J5762-1 and 2 it is buffered by I103A. strobe and serial data signals. The 429 bus drivers are composed of Q107 thru Q110 and associated components which supply +5. This results in the transponder replying only to Mode B and Mode C interrogations. Do not print without express permission of Honeywell.2. and +9. When I202-33 is low and I202-34 is high J5762-1 is +5 volts and J5762-2 is -5 volts. When I202-33 is high and I202-34 is low J5762-1 is -5 volts and J5762-2 is +5 volts. 4-5 . If the signal level is less than 3 volts I207A pulls TP207 low. Q201. and DATA BUS lines from I203 respectively. The clock signal occurs only after the data bit has stabilized at which time the clock goes high. These two signals are differentially amplified by I104A and I105A. CLOCK BUS. 34. and Q203 invert and level shift the DATA STROBE. After 32 bits of serial data have been transmitted. and Q203 is P202 pin 19. -10.3 volts to drive the 429 data bus components. When the microprocessor is finished transmitting a 32 bit word it turns off the 429 bus drivers by pulling I202-38 high.2.6 volts I206B pulls TP207 low interrupting the microprocessor I202. When TP207 goes low TP208 reflects the state of the 429 data bit received so the microprocessor can read it on I202-1. The output of I105A is the inverse of I104A. J5762-1 and 2 are both 0 volts. These two data lines are inverted by Q105 and Q106. this bit can be checked by observing the serial data while pin 9 of J5761 is grounded and opened. the strobe occurs which indicates the end of a 32 bit segment of data and the beginning of a new 32 bit segment.3. Q202. Data is outputted on I202-33. 4. When the microprocessor I202 transmits data on the 429 bus it first turns on the 429 bus drivers by pulling I202-38 low. Q202 is P201 pin 13.KFS 576A Refer again to Figure 4-2 Waveform and Timing Diagram and notice the time relationship between the clock.3. When pin 9 of J5761 is open to the A/B bit is high and the transponder replies only to Mode A and Mode C interrogations. Apr/2007 ©Honeywell International Inc. Without a transponder. 4. The output from Q201 is P201 pin 6. Rev 0. When I202-33 and 34 are both high. The output of I103A is level shifted by R141 and R213. If the signal level is greater than 7. to check the status of the FUNCTION and IDENT SWITCH to high.2. Pin 9 of the EEPROM is the store line. When power is applied to the control unit R212 and C201 hold I201-10 low for a short time after the 5 volt line is valid. I201 has a RAM space that is bit for bit mapped over the EEPROM. 22. Ident.3. to check the status of the CODE and CURSOR switches. I204B senses a drop in the 9. The Code selector switch is connected to E401 DATA SEL and the Function Switch to E402 DATA SEL. When a power interruption occurs.8 SWITCH INPUTS Pins 21. I203 alternately changes pin 17 from low. 23.2.7 MICROPROCESSOR RESET Pin 4 of both I202 and I203 are the reset inputs for the microprocessors and are used when power to I202 and I203 are interrupted. To prevent the EEPROM from being needlessly updated. I204B pulls I202-4 and I203-4 low and then allows them to slowly rise to +5 volts through an external capacitor C208. 23. This enables the use of only four pins of I203 to input eight different sources of information through a multiplexing scheme. Apr/2007 ©Honeywell International Inc. This results in a power on recall from EEPROM to RAM of the last code that was programmed so the microprocessor can read it. The DATA SEL and DATA SEL signals are complements of each other. 22. Rev 0. Only one of the two signals can be low at a time. 4. Pin 4 must then slowly rise to +5V. 23 or 24 of I203 during the time DATA SEL is low will be interpreted as an input from the Code Selector and Cursor Switches. and Cursor switch. Pin 4 of I202 and I203 are held at +5V during normal operation. or 24 during the time DATA SEL is low as an input from the Function and Ident Switches. it updates the EEPROM with the new code.KFS 576A 4.3.2. 23 and 24 of I203 are the inputs to the microprocessor from the Function selector. Code selector. the microprocessors wait approximately 3 seconds after a digit has changed and if another digit does not change within that time.3. When I201-9 goes low the contents of the RAM are stored in EEPROM. Data stored in memory I201 can only be erased electrically and remains stored even when power is removed. 4. A low on pins 21. 4-6 . Pin 11 controls reading and writing to the device RAM. The status of each switch is read by setting the appropriate DATA SEL line to low and checking the status of pins 21. and 24. I203 Pins 21 thru 23 are connected to the FUNCTION/CODE switches and I203 Pin 24 is the IDENT/CURSOR line. 22.6 EEPROM I201 is an Electrically Erasable Programmable Read Only Memory (EEPROM). When power is reapplied. I203 interprets a low input to pin 21. Do not print without express permission of Honeywell. I202-4 and I203-4 must be brought to ground before power is reapplied.3 volt supply and pulls pin 4 of I202 and I203 low. 22. two keep-alive anodes inside the gas discharge display (DS103) are continuously ionized. This circuit sequentially fires the eight anodes and energizes the proper cathodes. the "a" cathode bus (pin 11 of DS103) is connected to the top segment of all four digits. Apr/2007 ©Honeywell International Inc.KFS 576A 4. 7. Do not print without express permission of Honeywell. 8. Four of the anodes are associated with the 7-segment digits and their cursors. Cathode buses "i”. There is approximately +100 volts on the anodes of the display when they are not being fired. This +30 volt differential is not enough to ionize the gas and illuminate a display cathode segment. a cursor. The keep-alive anodes connect to +190 volts through R401 and R402 and the keep-alive cathodes connect to ground through R323 and R324. "k". The corresponding segments of each digit are wired together to form the "a". In addition. "l" and "m" are associated with letters in the nomenclature and they are formed in a similar manner.1 ANODE AND CATHODE DRIVERS The gas discharge display consists of 8 anodes and 13 cathode buses. while the cathodes are approximately +70 volts. The anodes of the display are driven by I302 and fired sequentially in the following order: 2.3. All of the cursors are wired together to form the "h" cathode bus. 4. an eight bit Johnson (ring) counter. "b". Each cathode bus is connected to the particular segment of a digit.3 DISPLAY CIRCUITRY The KFS 576A display circuitry consists of a gas discharge display and associated multiplexing and driving circuitry. 1. 4-7 . The corresponding anode must be pulled high (about +190 volts) by I302 and the cathode must be pulled low (about +15 volts) by I301 or I303. "e". Refer to Figure 4-4 Display Timing Diagram for display timing information. 3. A high on an input of I302 raises the corresponding output from about +100 volts to about +190 volts. For example. To insure proper display functioning under all ambient light and temperature conditions. 5. Once the segment is ionized the cathode voltage increases to about +35 volts and the resulting +155 volts between the anode and cathode is sufficient to sustain the ionization and illuminate a cathode segment. "f" and "g" buses. The remaining four anodes are used with the nomenclature. "j".3. a programming current proportional to the ambient light level is supplied to the cathode drivers to provide automatic dimming of the gas discharge display. or one letter in the nomenclature. "d".3. 6. Rev 0. "c". 4. Anode driver I302 is driven by I304. 3. If anode #2 is energized a three will illuminate as the leftmost digit. which is applied to I302-10. A high on the input of I303 pulls the corresponding output from about +70 volts to about +10 volts. The current output of I306B decreases as the increasing ambient light level lowers the resistance of V401. is turned on and off with the cathode by Q304 and Q305. 2. Do not print without express permission of Honeywell. "b". 4 and 8 of the Binary Coded Decimal digit that is to be displayed. if a segment is to be energized. The minimum time constant is approximately 80 usec and can be adjusted by R327. "d" and "g" low. Apr/2007 ©Honeywell International Inc. I303 drives the nomenclature cathode buses while I301 drives the digit cathode buses. I301 functions similar to I303 except that it contains a BCD to 7-segment decoder. if the digit "3" (binary 0011) is to be displayed as the leftmost digit. The decoder determines which cathode buses should be pulled low to display the digit. For example. the anode and cathode voltages are switched on and off together. The time constant of I305 is determined by the rate of charge of this capacitor. D3. This variable current varies the rate of charge of C308. Q304 and Q305 form a voltage divider that supplies approximately +95 volts to the driving circuitry. synchronizes the output of I304 with the data present on the cathode buses. Note that this input is different from all the others since a low signal pulls the cathode bus low. As a result. a constant current source (I306B) and a photodetector (V401). Some inputs and outputs of I303 are paralleled to provide increased driving current for the larger cathode segments in the nomenclature. D2. The cursors in the display are energized by a low on I301-10 which pulls the "h" cathode bus low. Like the cathode voltage. A Multiplex SYNC signal. An output of I304 goes high on the rising edge of the clock bus line and remains high until the next rising edge at which time the next anode in the sequence is energized.KFS 576A Only one output of I304 is high at a time which results in only one anode being energized at a time.2 AUTOMATIC DIMMING The brightness of the gas discharge changes in response to varying ambient light as sensed by photodetector V401. pins 4 and 5 of I301 are low while pins 2 and 3 of I301 are high. This signal forces anode #2 to go high in the event I304 is falsely triggered and anode #2 is not already high.3. This will cause ionization of the gas if the associated anode is energized at the same time. Rev 0. The decoder interprets this input as a three and pulls cathodes "a". 4. "c". 4-8 . the amount of time the anode voltage remains is dependent on the ambient light level. A square wave present at TP302 varies its duty cycle as a function of ambient light. P301-6. thus keeping the anode synchronous with the cathode data. This is accomplished by means of a one-shot (I305). Inputs D1. D4 and D8 contain bits 1. The cathode firing sequence is such that a cathode associated with a digit is energized followed by an anode associated with a nomenclature in a continuous manner. The anode voltage. Dimming is accomplished by varying both the duty cycle and the amplitude of the cathode driving current. R310 limits this current to the value required by cathode drivers I301 and I306. Rev 0. Each output of I301 and I303 acts as a constant current source. This is because a low on I305-2 and 4 forces I305 to reset causing the output of I305 pin 3 change from high to low.'s varies in amplitude and duration the cathode current is also varied and the brightness of the gas discharge display changes in response to ambient light level. DIM 1 switches Q301 on allowing I301 to source current while DIM 2 switches Q302 off so I303 cannot source current. DIM 2 is the inverse of the DIM 1. This pulse begins when the clock bus line on I305-2 and 4 goes high and triggers the one-shot and ends at the time determined by the rate of charge of C308. Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. approximately 1msec. The maximum pulse width can be no longer than the time between the rising and falling edge of the clock bus line. This DC voltage is applied to I306A which is used as a voltage-to-current converter.KFS 576A As ambient light increases the pulse width at TP302 continues to increase. The output of I306A is a current that is proportional to the voltage on C301. 4-9 . CR302 shunts this current to ground when the signal at TP302 is low resulting in a cathode driving current that varies in amplitude and duty cycle. The output of I305 is filtered by R314 and C301 to form a DC voltage proportional to the duty cycle of the square wave. This source current is proportional to the current applied to pin 1 of I301 and I303.C. On the next falling edge of DATA SEL line I203 pin 17 the signals are inverted and I303 sources current and I301 does not. Since the programming current at pin 1 of the I. A line from I203 microprocessor pin 17 is outputted to I205A inverter which is sent to P301 pin 7 “DIM 1” and I205A which inverts the signal and outputs it to P301 pin 11 “DIM 2”. Do not print without express permission of Honeywell.KFS 576A Rev 0. 4-10 . Apr/2007 ©Honeywell International Inc. 4-11 . Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc.KFS 576A Figure 4-1 KFS 576A Block Diagram (Dwg No 696-06837-0000 Rev 0) Rev 0. Do not print without express permission of Honeywell. 4-12 . Apr/2007 ©Honeywell International Inc.KFS 576A Rev 0. 4-13 .KFS 576A Figure 4-2 Waveform and Timing Diagram Rev 0. Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc.KFS 576A Figure 4-3 Serial Data (Dwg No 696-06838-0000 Rev 0) Rev 0. 4-14 . Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.KFS 576A Figure 4-4 Display Timing Diagram (Dwg No 696-06828-0001 Rev 0) Rev 0. 4-15 . KFS 576A Rev 0. Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 4-16 . 2. Digital voltmeter: Fluke 8000A or equivalent D. KFS 586/A Test disk. KFS 579/A Test disk. Apple Disk ][ and controller card. Apple //e or Apple ][ plus with 48 K memory or equivalent. KFS 598/A Test disk. Oscilloscope: Tektronics 465 or equivalent C. PN 222-00004-0000. Power supply: +28 VDC @ 5A Sorensen PTM 28-6. 5 1/4 inch or equivalent.1 TEST EQUIPMENT REQUIRED A. PN 071-05084-0000. alignment. KFS 564/A Test disk. 5. Apple test system: 1. 6. KCT 110 Test Set. 4. KCA 110 Test set Adapter.2 TEST AND ALIGNMENT The preferred method of testing the KFS 576A Transponder Control Unit is using either an APPLE //e or an APPLE ][ PLUS or equivalent personal computer with a disk drive. PN 222-00002-0000. The following procedure describes how to prepare the KFS 576A for testing. which contains: 1. Rev 0. cleaning. PN 222-00006-0000. 3.0 or equivalent B. 5. disassembly/assembly and troubleshooting procedures for the KFS 576A Transponder Control Unit. Refer to the test setup illustration in Figure 5-1 Test Setup. PN 222-00005-0000.1 GENERAL INFORMATION This section contains test. E.KFS 576A SECTION 5 MAINTENANCE 5. PN 222-00003-0000. 2. KFS 576/A Test disk. Do not print without express permission of Honeywell. Video monitor. 5-1 . 3. Apr/2007 ©Honeywell International Inc. 2. 48K or memory and a monitor. inspection. 5. PN 050-02260-0010. The last step on the menu. It is also necessary to send a selected. 2. as well as display a received. 2. PN 155-05664-0012. 5.1. Sync cable P2. The KFS 576A test program is set up to follow the test procedures and test data sheet in section 5. and a floppy disk containing the test program. unit status. 4. or go directly to a specific test in an attempt to verify a complaint or performance of a unit function.4. The ARINC 429 serial data message is used to communicate between master and slave KFS 576A’s in a tandem installation or a KFS 576A and a KNS 660 system for frequency management. PN 155-05664-0016. Sync cable P3. The KCA 110 interface box contains break out of necessary test points. as described in section 5. 3. 5-2 .2.2 DESCRIPTION OF KFS 576A TEST PROGRAM Testing of the KFS 576A requires the ability to receive and display the King serial data messages which are used to set up the mode of the KXP 756 transponder.KFS 576A F. which contains: 1. PN 050-02606-0000. of this manual.2. The unit status will be valuable for trouble-shooting the commonly used functions of a KFS 576A. Rev 0. filling out a test data sheet and completing a final test data sheet. four cables which connect the KFS 576A and the KCA 110 interface box to the computer. so that a menu of tests can be displayed on the screen. The KCA 110 will supply power to the control unit. The unit status portion of the program displays all functions except auto dim override and ARINC 429.2. The KCT 110 consists of two PC boards which will be inserted in the appropriate card slots of the computer. Async cable P3. Async cable P2. which contains: 1. Once the menu is displayed you may choose to step through in sequence. will provide all of the necessary serial interface and control function interface to the KFS 576A . PN 200-07164-0000. Sync Card Kit. The test program will ask for the specific part number of the control unit to be tested. PN 200-07157-0000. PN 155-05664-0006. PN 155-05664-0007. PN 050-02605-0000. Async Card Kit. 3. Sync card. ARINC 429 serial data message. Apr/2007 ©Honeywell International Inc. is not part of the final test procedure. Do not print without express permission of Honeywell. Async card. Async cable P1. The KCT 110 computer test system used in conjunction with an Apple or Apple equivalent computer system. G. PN 155-05664-0017. 8. A finger is not opaque and will not block sufficient light to correctly set the brightness. B. Cover the photodetector with an opaque material. Connect the KFS 576A interface harness to the Interface Box and the KFS 576A. 5. 3. The bench test setup should be connected as shown in Figure 5-1 Test Setup. Make sure power is turned off to both the KFS 576A and the APPLE computer. Remove opaque material from detector. To adjust the brightness. and the async card in any slot except 0 (7 is preferred). Apply +28 VDC to the interface box. The test program requires about 30 seconds to load. Remove the cover on the APPLE computer and insert the sync card in any slot except 0 (5 is preferred). Apr/2007 ©Honeywell International Inc. The top menu will then appear on the monitor. Connect the monitor and disk drive to the computer per the instructions in the owners manual. Rev 0. At this time the KFS 576A should have all voltages necessary to operate and should come on. Follow the instructions displayed on the monitor and any supplemental instructions in the corresponding paragraphs in this section. refer to the alignment and troubleshooting sections of this manual for guidance in locating the problem. Insert the diskette containing the KFS 576A Test Program into the disk drive and turn on computer.2. 6. Select the KFS 576A Test Program. 9. connect an oscilloscope to TP 302. 5-3 . Display dimming is the only adjustment necessary for the KFS 576A.3 ALIGNMENT A.KFS 576A 5. Adjust R 327 until the pulse width is 80us wide. Refer to owners manual. TEST SETUP 1. If it is not. then turn on the control unit (if equipped with an ON/OFF switch). 2.2. 7. Do not print without express permission of Honeywell. Connect the ribbon cables from the King sync card to the KCA 110 interface box and the ribbon cable from the King async card to the KCA 110 interface box and put the cover back on computer. Confirm that the computer system is operating properly. 4.4 FINAL TEST The following tests (in the KFS 576A Test Program) should be run to determine if the KFS 576A is operating properly. 5. 10. Unless otherwise indicated. 3. If the key is held down the function may be repeated. Connect to test points and test connectors on the front of the KCA 110 during testing per the final test procedures. Rev 0. The KCA 110 cable #4 connects the KFS control unit to the KCA 110 via P1014. 2. Do not print without express permission of Honeywell. however 7 is preferred. Do not connect more than one control unit at a time. 4. Cable 4 has connectors for all of the control units. The async card is inserted into any slot except 0. Observe the connector markings and connect the appropriate connector to the unit to be tested. when instructions are given on the Apple screen or in the Maintenance manual to press a key it is implied that the key stroke is momentary.The sync card is inserted into any slot except 0. The KCA 110 cables reach through the rear of the computer to the cards.DVM. Apr/2007 ©Honeywell International Inc. 5-4 .and audio gen.The scope. NOTE The slot 0 applies only to the Apple ][ plus.KFS 576A Figure 5-1 Test Setup NOTE:1. During alignment the scope is used to monitor a test point inside the control unit. however 5 is preferred. C. Verify that the display is illuminated and that TP11 ON 1 is high. Apr/2007 ©Honeywell International Inc. 071-1276-19/20/21/22: If unit is not equipped with an ON/OFF switch.2 DISPLAY A. Verify that the display is illuminated and that TP11 ON 1 is high. Turn the function switch clockwise to view Flight Level. Verify that the display of the unit is illuminated. B. Turn the 1/OFF/2 knob to the 2 position. D. 071-1276-08/09/10/11/18: Turn the On/Off knob from the OFF position to the ON position and verify that the display of the unit is illuminated when power is applied to the KCA 110. Rev 0.1 ON/OFF A. Verify that the Flight Level on the control head display is the same as the Flight Level selected on the Apple screen. Verify that the display of the unit is illuminated in the 1 position and not illuminated in the OFF position. Use the selector switch (S1) on the KCA 110 to verify that the lighting is working correctly. Use the <. All segments shall be of uniform brightness with no arcing between segments.and -> cursor keys to increment/decrement the Flight Levels on Apple. C.2.KFS 576A 5. Verify that the display does not flicker in a dark environment.4. 071-1276-13/14/15/16: Turn the 1/OFF/2 knob from the OFF position to the 1 position. 5-5 .2. 5.4. 071-1276-23/24/25/26: Turn the 1/2 knob to the 1 position.3 FLIGHT LEVEL (FL) To test Flight Level (FL) ground External Standby (J5761 pin 17). This should place the unit in SBY mode.2. B. Turn the 1/2 knob to the 2 position. Do not print without express permission of Honeywell. 5.4. verify that the display of the unit is illuminated when power is applied to the KCA 110. C. A zero indicates that the corresponding pin of J5761 is open.4.4. unless otherwise desired leave External Ident in the non-active state. When the cursor switch is pushed the control head display cursor should move from left to right. A. Verify that counter-clockwise rotation decrements the digit above the cursor in the control head display. Altitude is displayed only in TEST mode and Flight Level mode. 5. Do not print without express permission of Honeywell. D. Digits should rollover from 7 to 0 and roll under from 0 to 7.5 CODE SELECTOR SWITCH NOTE: There should be a change in code for every increment or decrement. Apr/2007 ©Honeywell International Inc.4 IDENT Verify that when the IDT button is pushed or the external ident line (J 5761 pin 21) is grounded IDT should light in the lower right corner of the control head display and stay lit for 23 ±4 seconds. Rev 0. 2.2. NOTE: IDT will not light in standby mode. If the cursor is pointing to the right most digit when the switch is pushed the cursor should move to the left most digit. a one indicates that the pin is shorted to ground. 5. The cursor will remain under a digit for approximately 5 seconds and if the code selector switch is not rotated during that 5 second period the cursor will return to the leftmost digit and the new code is transmitted from the RT. Verify that clockwise rotation increments the digit above the cursor in the control head display. 5-6 . NOTE: There should be a change in cursor position each time the cursor switch is pushed.KFS 576A 1. B.2. 7 REPLY Verify that when Reply (J5761 pin 11) is grounded the “R” in the upper left corner should light.2.4. 5. Rev 0.6 EMERGENCY Verify that when Emergency (J5762 pin 4) is grounded the channeling code should change to 7700 when the cursor is held in for at least 3 seconds. Apr/2007 ©Honeywell International Inc.4. Verify that grounding automatic dimmer override (J5761 pin 25) disables dimming from the photo-cell and the display goes to maximum brightness.2. B.9 EXTERNAL STANDBY When the External Standby (J5761 pin 17) is grounded the unit should go to standby mode.2.2. Verify that the display dims evenly in a dark environment.4. Change Transponder Code. 5-7 . the cursor is extinguished. 5. NOTE: Before going on to another step leave control disable not active. 5. 5.KFS 576A 5.4. B. NOTE: Unless otherwise desired leave emergency in the non-active state. NOTE: Unless otherwise desired leave reply in the non-active state. Wait at least 5 seconds.11 NON VOLATILE MEMORY A.8 DIMMING A. C. Remove power from the unit.4. NOTE: Unless otherwise desired leave external standby in the non-active state.2. Do not print without express permission of Honeywell. When the line is ungrounded the unit should return to the mode it was in prior to activating the line. D. 5. Observe display.4.2.10 CONTROL DISABLE Verify that the when Control Disable (J5762 pin 5) is grounded. Verify that there is no data present on TP 1 (data A) and TP 2 (data B). Place control head in Unit No. Place TP 2 on channel 2 of the Oscilloscope. TP 1 and B. 5. F. and Master modes. Reapply power to the unit.12 CHANNELING NOTE: The information on the Apple screen is a display of what is on the serial synthesizer bus. (Note: 429 data will appear in this test) B.2. Xpond Data TP 4.4. UNIT ONE 1. Verify that display is the same as observed in step B. Rev 0.0V MAX NOTE: Place TP 1 on channel 1 of the Oscilloscope. 1 and Slave modes. Place control head in Unit No. TP 2 are.4.5V max 5. Verify that the control head display duplicates the key board.13 429 I/O A.0V MIN 11. Verify that the voltages between the data line A.2. XPOND CLK TP3 XPOND DATA TP 4 XPOND TP 5 VOLTAGE HIGH 8.0V max VOLTAGE LOW 0. Refer to the table below for appropriate voltage levels for the Xpond Clock TP 3.0V MAX VOLTAGE NULL -0. Send a frequency from the apple key board to the control head.KFS 576A E.0V min 10.0V MIN -9. VOLTAGE HIGH 9. Verify that the Xpond data bus transmits the serial data from the control head display to the Apple screen. Do not print without express permission of Honeywell. Invert channel 2 and add the two channels.5V MAX VOLTAGE LOW -11. 2. 2. A. 5-8 . Xpond Strobe TP 5 lines. UNIT TWO 1. Apr/2007 ©Honeywell International Inc.5V MIN 0.0V min 0. 5-9 .15 UNIT STATUS This test is only intended to be used as a troubleshooting aid.KFS 576A 5.2. select the VFR code as required. the display code should be replaced with the last VFR code programmed.4.14 VFR CODE To program the VFR code: Rotate the function selector knob to standby.2. Apr/2007 ©Honeywell International Inc. 5. Rev 0. Do not print without express permission of Honeywell. The displayed code should be stored as the VFR code. press the IDT and Cursor buttons simultaneously.4. To select the VFR code: When the cursor switch is held in for at least 3 seconds. Cursor switch OK 6.16 FINAL TEST DATA SHEET NOTE: The term "OK" indicates that particular function is operating properly.3 alignment c.4. Display goes to max bright OK d. Lighting OK Flight Level Display matches Apple screen OK a. 5-10 . Display 3. Pulse width 80us OK see para.2. IDENT button OK b. 5. 4. On/Off 2. Emergency (7700)OK 7.2. Apr/2007 OK ©Honeywell International Inc.KFS 576A 5. 5. 1. Reply “R” lit OK 8. External IDENT OK Ident Code selector switch a. Rollover OK d. Photo-cell is disabled OK External Standby Rev 0. Clockwise rotation OK b. Display OK b. a. Dimming 9. Do not print without express permission of Honeywell. OK a. Counter-clockwise rotation OK c. Display dims evenly OK b. 2. 5-11 .5v Xpond Data TP 4 OK logic high greater than 8v Xpond Data TP 4 OK logic low less than . 13. Apr/2007 ©Honeywell International Inc. 14. Channeling a. Xpond clock TP 3 OK logic high greater than 8v Xpond clock TP 3 OK logic low less than . OK Control head matches Apple OK 1.5V OK Voltage between A and B logic low less than -9V OK Apple screen matches control head OK VFR code a. No data on A and B OK Apple keyboard changes display OK UNIT TWO 1.5v Xpond strobe TP 5 OK logic high greater than 8v Xpond strobe TP 5 OK logic low less than . OK Unit 2. 3. Stores VFR code OK b.KFS 576A 10. 2. Selects VFR code OK Rev 0. Unit 1. Master OK Voltage between A and B OK logic high greater than +9V Voltage between A and B logic null less than +. Control disable a. 429 I/O a. Slave. Cursor not lit 11 Memory 12. Do not print without express permission of Honeywell. b. UNIT ONE 1.5v 2. component corrosion. D. and other irregularities. deformed shells or clamps. Fuse and Clips Inspect for blown fuse and check clips for loose or corroded connections. Capacitors. Chassis Inspect the chassis for deformation. 5-12 . A. punctures. or corroded terminal studs. improperly soldered. Apr/2007 ©Honeywell International Inc. and badly worn surfaces. detailed procedures are arranged in alphabetical order. damaged connectors. Also. broken. corrosion and damage to finish. Do not print without express permission of Honeywell.1 VISUAL INSPECTION This section contains instructions to assist in determining. and cracked. Inspect for cracked or broken insulation and for contacts that are broken. broken. damaged fastener devices. deep dents. Inspect for loose. E. Variable Inspect trimmers for chipped and cracked bodies. check for damaged fastener devices. broken. or charred insulation. Check for loose. lugs. or leads. broken. badly worn surfaces. deterioration or other causes can be found by these inspection procedures. deformed or out of alignment. To aid inspection. by inspection. Defects resulting from wear. check for corroded or damaged plating on contacts and for loose.3. Covers and Shields Inspect covers and shields for punctures. or improperly soldered connections. the condition of the KFS 576A assemblies. F. loose or missing hardware. body damage. Rev 0. and damage to the finish. Capacitors. Also. C.KFS 576A 5. physical damage.3 OVERHAUL 5. damaged dielectrics and damaged contacts. B. or corroded terminal connections. Connectors Inspect connectors for broken parts. Fixed Inspect capacitors for case damage. dents. Check for insulation that is stripped back too far from the terminal. or other irregularities. improperly soldered. Inspect for corrosion at the terminal. deformations. or improperly soldered connections. 5-13 . Insulators Inspect insulators for evidence of damage. Potentiometers Inspect all potentiometers for evidence of damage or loose terminals. K. 4. Apr/2007 ©Honeywell International Inc. Inspect the windings. cracked insulation or other irregularities. or charred bodies and loose. Inspect for cold-soldered or rosin joints. or broken terminal connections.KFS 576A G. H. loose or broken parts. rough appearance. These joints present a porous or dull. 2. cracked insulation. Resistors. protrusions from a joint. leads. broken. L. Examine the terminals for excess solder. Jacks Inspect all jacks for corrosion. J. cut or charred windings. such as broken or chipped edges. Do not print without express permission of Honeywell. burned areas. terminals and connections for corrosion or physical damage. Inspect for insufficient solder and unsoldered strands of wire protruding from the conductor at terminal. Check for crushed. pieces adhering to adjacent insulation. broken. and particles lodged between joints. scratched. or other components. bad contacts. loose mountings. blistered. Check for physical damage to forms and tuning slug adjustment screws. Fixed Inspect the fixed resistors for cracked. conductors. I. RF Coils Inspect all RF coils for broken leads. Terminal Connections Soldered 1. 3. and loose. rust. Check for strength of bond using the points of a tool. and presence of foreign matter. Rev 0. dry. Using a clean. C. Transformers 1. Inspect for signs of excessive heating. lint-free cloth lightly moistened with a regular cleaning detergent. B. refer to the appropriate PC board assembly drawing and follow notes to insure correct mounting and mating of each connector. cracked or broken insulation. Rev 0. and other abnormal conditions. C. poorly soldered. physical damage to case.KFS 576A M. Connectors When replacing a connector. Apr/2007 ©Honeywell International Inc. Care should be taken to prevent damage by the airblast.3. Clean the receptacles and plugs with a hand controlled dry air jet (not more than 25psi). use long nose pliers as a heat sink under normal soldering conditions. Using a hand controlled dry air jet (not more than 15psi). or loose connecting leads or terminals. lint-free cloth lightly moistened with an approved cleaning solvent. cut or broken lacing and improper dress in relation to adjacent wiring or chassis. blow the dust from inaccessible areas. Do not print without express permission of Honeywell. subassembly chassis and parts of equipment for breaks in insulation. Wiring/Coaxial Cable Inspect open and laced wiring of the chassis. Wipe dry with a clean.3.3 CLEANING A.3 REPAIR This section describes the procedure along with any special techniques for replacing damaged or defective components. Crystal The use of other than a King approved crystal is considered an unauthorized modification. and a clean. 5. B. Diodes Diodes used are silicon and germanium. Note the diode polarity before removal. conductor breaks. dry. 5-14 . A. lint-free cloth. Inspect for corroded. 2. 5. remove the foreign matter from the equipment case and unit front panels. N. Wipe dry using a clean. lint-free cloth. The switch board can then be removed by sliding the board forward till the driver board pins and the switch board connector are disconnected from each other.3 FRONT COVER/SWITCH BOARD REMOVAL (088-01166-XXXX/ 200-06589-XXXX) A. B.3. Remove the three screws holding the Display board to the unit.3. Remove unit cover. Remove the two screws at the back of the unit cover. Do not print without express permission of Honeywell. Remove the two screws at the rear and front of the Microprocessor board. size and length. 5. board harness connector from the I/O board E.4.4. C. 5. Disconnect switch (200-06579-XXXX).3. B. Remove the four screws that hold the front cover to the unit.4. and the two screws which are located on the top and bottom of the unit. F. 5. Wiring/Coaxial Cables When repairing a wire that has broken from its terminal. 5.2 MICROPROCESSOR BOARD REMOVAL (200-6580-XX) A. Replace the damaged wire or coax with one of the same type. remove front cover. Apr/2007 ©Honeywell International Inc. Carefully remove the Board by sliding the board outward from the connector pins till the board is disconnected from the I/O board (200-06579-XXXX) connector pins. restrip the wire to the necessary length and resolder the wire to the terminal.4 DISASSEMBLY Refer to Figure 6-1.KFS 576A D. Remove display (037-00083-0000) from board.1 COVER REMOVAL (047-05021-0002) A. Rev 0.3. remove all old solder and pieces of wire from the terminal. Remove front knobs from unit. 5-15 . D. 5. Do not print without express permission of Honeywell.3V C. A.4. 5. J103-7 Lighting +28VDC or +5VDC as appropriate Rev 0.3. Apr/2007 ©Honeywell International Inc. and refer to the troubleshooting flowchart in Figure 5-2 KFS 576A Troubleshooting Flowchart for troubleshooting information. I106-3 -26V D. To reassemble the unit.3. reverse disassembly procedures. B.4 TROUBLESHOOTING To troubleshoot the KFS 576A consult the schematics for waveform and voltage data.4 DRIVER BOARD REMOVAL (200-06626-XXXX) A. J5761-7 +190V B. 5-16 . The board can now be pulled away from the center mounted I/O board (200-06579-XXXX).4. J5761-10 +9. being careful not to damage the I/O board (200-06579-XXXX) connector pins or the connector on the driver board.KFS 576A 5.5 ASSEMBLY A. Remove the rear two screws and the front three screws. The following voltages should be checked before troubleshooting is attempted. Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.KFS 576A Figure 5-2 KFS 576A Troubleshooting Flowchart (Dwg No 696-02376-0000 Rev 0) (Sheet 1 of 2) Rev 0. 5-17 . Do not print without express permission of Honeywell. 5-18 .KFS 576A Rev 0. Apr/2007 ©Honeywell International Inc. 5-19 . Apr/2007 ©Honeywell International Inc.KFS 576A Figure 5-2 KFS 576A Troubleshooting Flowchart (Dwg No 696-02376-0000 Rev 0) (Sheet 2 of 2) Rev 0. Do not print without express permission of Honeywell. 5-20 .KFS 576A Rev 0. Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 6-1 . the existing 9-digit numbering system is being expanded to 12 digits by the addition of 3 zeros. Symbol Column This column contains the Reference Designators of the electrical components of the assembly.KFS 576A SECTION 6 ILLUSTRATED PARTS LIST 6. The Reference Designator consists of a letter abbreviation which indicates the type of component followed by the number assigned to that part (C101. Apr/2007 ©Honeywell International Inc. Parts or documents represented either by the existing 9-digit or expanded 12-digit part number are identical and interchangeable. B. NOTE: To facilitate a common Part Number System between ATAD and GAAD. Add one zero to the center set and two zeros to the dash number (XXX-0XXX-00XX). A sample BOM is included in this section as Figure 6-1 Typical Bill of Material. 6. Common Reference Designator abbreviations are listed below. etc). Individual Bills of Material (BOM) within this IPL are arranged in numerical order by BOM number. Each BOM is followed by the Assembly Drawing and Schematic Diagram for that assembly. Q101. Rev 0. BOM Number The Bill of Material Number appears at the top of the BOM as a 9-digit number which is also the Honeywell Part Number for the assembly.1 INTRODUCTION This Illustrated Parts List (IPL) provides for the proper identification of replacement parts. Warranty information concerning Honeywell replacement parts are contained in Service Memo #1. P/N 600-08001-XXXX. Mechanical parts are not assigned Reference Designators. Parts identified in this IPL by Honeywell Part Number meet design specifications for this equipment and are the recommended replacement parts.2 BILL OF MATERIAL DESCRIPTION This section describes the various items that appear on the Bills of Material. A. The BOM Number is followed by the assembly description and the revision level of the BOM. Do not print without express permission of Honeywell. Do not print without express permission of Honeywell. CR401 999-9999-99 DO NOT USE The component designator CR401 has been previously used on the assembly and then deleted. Apr/2007 ©Honeywell International Inc. CR401 999-9999-96 RESERVED The component designator CR 401 is reserved for future usage. 3. CR401 999-9999-97 SEE NEXT ASSEMBLY The component designator CR401 is used as part of the electrical circuit assembly but because of assembly or testing requirements may be part of another assembly. 6-2 . 1. Part Number Column This column contains the King Part Number for each part.KFS 576A C Capacitor P Plug CJ Circuit Jumper R Resistor CR Diode S Switch DS Lamp T Transformer F Fuse TP Test Point FL Filter U Resistor/Capacitor Network I Integrated Circuit V Photocell/tube J Fixed Connector WG Waveguide L Inductor Y Crystal Q Transistor C. Rev 0. 4. 2. CR401 999-9999-98 NOT USED The component designator CR401 is available for future assignment and is not presently a part of the PC board/Final assembly. therefore it cannot be reassigned. Special purpose 999-9999-XX series part numbers may appear in the BOM and are described below. Apr/2007 ©Honeywell International Inc. If the PN and description reads "200-XXXXX-0099 COMMON BOM" the parts for that assembly are included in the same BOM. Description Column This column contains the description of each part in the assembly. 6-3 . Common abbreviations which may appear in this column are listed below. Do not print without express permission of Honeywell. AL Aluminum PC Polycarbonate BIFLR Bifilar PF Precision Film BOM Bill of Material PP Paper CC Carbon Composite PS Polystrene CF Carbon Film QW Quarter Watt CH Choke RES Resistor CAP Capacitor S Silicon CAP CR Ceramic SCR Screw DC Disk Ceramic SM Silver Mica DIO Diode STDF Standoff EL Electrolytic SW Switch FC Fixed Composition TERM Terminal FERR Ferrite TN Tantalum FLTR Filter TST PT Test Point FT Feedthru TW Tenth Watt HV High Voltage VA Variable HW Half Watt WW Wire Wound IC Integrated Circuit XFMR Transformer MC Monolithic Ceramic XSTR Transistor MY Mylar XTAL Crystal E. The parts breakdown for an assembly with any other PN will be found in the BOM with the same number.KFS 576A D. Rev 0. Assembly (A) Column An "A" in this column indicates that the part indicated is an assembly. KFS 576A F. EA Each FT Foot AR As Required G. Rev 0. Do not print without express permission of Honeywell. Quantity and Version Columns Individual versions of an assembly are identified by the last two digits of the PN. The parts indicated in the 0099 Column are common to all other versions of the assembly and are considered the Common Bill of Material for the assembly. Common abbreviations found in this column are listed below. Apr/2007 ©Honeywell International Inc. 6-4 . Unit of Measure (UM) Column This column indicates the Unit of Measure for each part. Part quantities for each version will be indicated under headings numbered 0000 through 0099 as required. KFS 576A Figure 6-1 Typical Bill of Material Rev 0, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 6-5 KFS 576A Rev 0, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 6-6 KFS 576A PN DESCRIPTION REV ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------071-1276-08 XPDR CTRL BK 28V 2 071-1276-09 XPDR CTRL BK 5V 2 071-1276-10 XPDR CTRL GY 28V 2 071-1276-99 COMMON DFSD AD ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0008 -0009 -0010 -0099 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------REF1 300-03119-0000 FINAL ASSEMBLY RF .00 .00 .00 . REF100 000-00388-0000 FLOW CHT KFS0576A RF .00 .00 .00 . REF4 004-00448-0000 MPS KFS0576A RF .00 .00 .00 . 012-01005-0002 TAPE MYLAR .500 W IN . . . 4.80 012-01127-0000 TAG COVER EA . . . 1.00 016-01412-0000 LOCTITE 425 AR . . . 1.00 035-01909-0001 PROTECTIVE COVER EA . . . 1.00 037-00083-0000 KFS 576A DISPLAY EA . . . 1.00 047-05021-0002 COVER W/FINISH EA . . . 1.00 057-01540-0000 WARNING HV TAG EA . . . 1.00 057-01764-0000 WRN TAG 5V LGT EA . 1.00 . . 057-01764-0002 WRN TAG 28V LGT EA 1.00 . 1.00 . 057-02203-0008 FLAVOR STCKR EA 1.00 . . . 057-02203-0009 FLAVOR STCKR EA . 1.00 . . 057-02203-0010 FLAVOR STICKER EA . . 1.00 . 057-02337-0000 PRTCTV CVR DECAL EA . . . 1.00 057-02742-0000 S/N TAG, KFS 576A EA . . . 1.00 057-02831-0001 KFS DUP S/N TAG EA . . . 1.00 057-02834-0000 ESD TAG EA . . . 1.00 057-02888-0000 DECAL D.O.C. EA . . . 1.00 057-02890-0027 SCT KFS576A EA . . . 1.00 071-01276-0099 COMMON DFSD EA 1.00 1.00 1.00 . 073-00504-0003 BEZEL BLK EA 1.00 1.00 . . 073-00504-0004 BEZEL GRAY EA . . 1.00 . 073-00551-0004 KNOB W/H EA . . . 1.00 073-00553-0006 KNOB W/H EA 1.00 1.00 1.00 . 073-00554-0008 KNOB W/H EA . . . 1.00 076-00111-0001 STAND-OFF .605 EA . . . 1.00 088-01166-0002 INSERT -00 W/LENS EA 1.00 1.00 . . 088-01166-0004 INSERT -03 W/LENS EA . . 1.00 . 089-05874-0003 SCR PHP 2-56X3/16 EA . . . 2.00 089-05874-0004 SCR PHP 2-56X1/4 EA . . . 9.00 089-05874-0005 SCR PHP 2-56X5/16 EA . . . 3.00 089-05874-0006 SCR PHP 2-56X3/8 EA . . . 1.00 089-06000-0003 SCR FHP 0-80X3/16 EA . . . 4.00 089-06004-0003 SCR FHP 2-56X3/16 EA . . . 2.00 089-06584-0000 SCR PHP 6-32X 1/2 EA . . . 2.00 090-00990-0001 PROTECTIVE CAP, SUB-D, 9P EA . . . 1.00 090-00990-0003 PROTECTIVE CAP, SUB-D, 15P EA . . . 1.00 091-00637-0002 INSULATOR, MYLAR EA . . . 1.00 150-00018-0010 TUBING SHRINK WHT IN . . . 2.00 150-00020-0010 TUBING SHRINK 18G IN . . . .40 200-06579-0000 I/O BOARD ASSY EA 1.00 . 1.00 . 200-06579-0001 I/O BOARD ASSY EA . 1.00 . . 200-06580-0000 MICROPROCESSOR BD EA . . . 1.00 200-06589-0000 SW BD 28V W/SW EA 1.00 . 1.00 . 200-06589-0001 SW BD 5V W/SW EA . 1.00 . . 200-06626-0000 DRIVER BD EA . . . 1.00 Rev 0, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 6-7 00 . 012-01005-0002 TAPE MYLAR .O. . .00 076-00111-0001 STAND-OFF . 1. 089-05874-0003 SCR PHP 2-56X3/16 EA . REF4 004-00448-0000 MPS KFS0576A RF . 1. 9P EA . .00 . . . 4.00 . 1. .00 . 1. 1. 1. 200-06626-0000 DRIVER BD EA . . . . EA . .00 . .00 057-02888-0000 DECAL D. 200-06579-0001 I/O BOARD ASSY EA 1. . 1.00 . . 1. 9.00 . . KFS 576A EA . 1.00 090-00990-0001 PROTECTIVE CAP.00 . 1. .00 . 3. . 057-02337-0000 PRTCTV CVR DECAL EA . 1. .00 Rev 0.00 089-05874-0005 SCR PHP 2-56X5/16 EA . . . . . 200-06589-0003 SW BD 5V SW 1/2 EA .00 . 073-00504-0003 BEZEL BLK EA . .00 . . . 057-02203-0013 FLAVOR STCKR EA .00 . . . .00 089-05874-0006 SCR PHP 2-56X3/8 EA . .00 . 2. . 1. 088-01166-0006 INSERT -05 W/LENS EA . 1.80 012-01127-0000 TAG COVER EA . . 1. 073-00551-0004 KNOB W/H EA . 073-00504-0004 BEZEL GRAY EA 1. . 200-06580-0000 MICROPROCESSOR BD EA .500 W IN . . 1. .00 . .00 1.00 . .00 057-02742-0000 S/N TAG. .40 200-06579-0000 I/O BOARD ASSY EA .C.00 . .00 089-06000-0003 SCR FHP 0-80X3/16 EA . 1. .00 057-02890-0027 SCT KFS576A EA . .00 057-01540-0000 WARNING HV TAG EA . . 6-8 .00 150-00020-0010 TUBING SHRINK 18G IN . 15P EA .00 089-06584-0000 SCR PHP 6-32X 1/2 EA . 2. .00 1. 1. 1.00 . . . . 057-01764-0002 WRN TAG 28V LGT EA . 4. . 1. . 1. . . . 1. 073-00554-0008 KNOB W/H EA .00 035-01909-0001 PROTECTIVE COVER EA . SUB-D. 1.00 090-00990-0003 PROTECTIVE CAP. . .00 . Apr/2007 ©Honeywell International Inc. .00 016-01412-0000 LOCTITE 425 AR .00 . 2. Do not print without express permission of Honeywell. MYLAR EA .00 200-06589-0001 SW BD 5V W/SW EA 1. 1. 1.00 . . . .00 057-01764-0000 WRN TAG 5V LGT EA 1. .00 1.00 089-06004-0003 SCR FHP 2-56X3/16 EA . .00 . 1. .00 047-05021-0002 COVER W/FINISH EA . . . 1. . .00 1.00 1. 2. . 1.605 EA . .KFS 576A PN DESCRIPTION REV ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------071-1276-11 XPDR CTRL GY 5V 2 071-1276-13 XPDR CTRL BK 28V 2 071-1276-14 XPDR CTRL BK 5V 2 071-1276-99 COMMON DFSD AD ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0011 -0013 -0014 -0099 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------REF1 300-03119-0000 FINAL ASSEMBLY RF . 1. 200-06589-0002 SW BD 28V SW 1/2 EA .00 057-02831-0001 KFS DUP S/N TAG EA . 1.00 071-01276-0099 COMMON DFSD EA 1. 1.00 037-00083-0000 KFS 576A DISPLAY EA .00 .00 1.00 057-02834-0000 ESD TAG EA . REF100 000-00388-0000 FLOW CHT KFS0576A RF .00 073-00553-0006 KNOB W/H EA 1. . 057-02203-0014 FLAVOR STCKR EA . 1.00 091-00637-0002 INSULATOR. 057-02203-0011 FLAVOR STICKER EA 1. SUB-D.00 . . . .00 150-00018-0010 TUBING SHRINK WHT IN .00 . .00 088-01166-0004 INSERT -03 W/LENS EA 1. .00 089-05874-0004 SCR PHP 2-56X1/4 EA . . . .00 . . .00 .00 . Apr/2007 ©Honeywell International Inc. EA .00 200-06589-0000 SW BD 28V W/SW EA .00 071-01276-0099 COMMON DFSD EA 1.80 012-01127-0000 TAG COVER EA . . 200-06589-0003 SW BD 5V SW 1/2 EA . 057-02203-0015 FLAVOR STCKR EA 1.00 . 2. 073-00504-0003 BEZEL BLK EA .00 .00 Rev 0.40 200-06579-0000 I/O BOARD ASSY EA 1.00 . . 1. . . .00 . .00 076-00111-0001 STAND-OFF . .00 . 057-02203-0016 FLAVOR STCKR EA . . 1.00 .00 088-01166-0001 INSERT -00 W/LENS EA .00 016-01412-0000 LOCTITE 425 AR .O. 1. .00 089-06584-0000 SCR PHP 6-32X 1/2 EA . . KFS 576A EA . 1. 9. . 1. 1. 4. 012-01005-0002 TAPE MYLAR . . . . . . 073-00504-0004 BEZEL GRAY EA 1.00 . 1. . 1. .00 1. . .00 1. 1. . 1. .00 091-00637-0002 INSULATOR.00 057-02890-0027 SCT KFS576A EA . Do not print without express permission of Honeywell. . . .00 . . REF4 004-00448-0000 MPS KFS0576A RF .00 047-05021-0002 COVER W/FINISH EA .00 .00 . . .00 .00 1.00 089-06000-0003 SCR FHP 0-80X3/16 EA . 6-9 .00 089-05874-0006 SCR PHP 2-56X3/8 EA .00 .605 EA . 1. . 089-05874-0003 SCR PHP 2-56X3/16 EA .00 073-00553-0006 KNOB W/H EA 1. . 1.00 . 1. .00 057-02834-0000 ESD TAG EA . . . .00 057-02742-0000 S/N TAG. 4.00 090-00990-0001 PROTECTIVE CAP. . 1. 073-00554-0008 KNOB W/H EA .00 057-01764-0000 WRN TAG 5V LGT EA .00 . . .00 .00 . 057-02337-0000 PRTCTV CVR DECAL EA . . .00 . 1.00 .00 . .00 057-02831-0001 KFS DUP S/N TAG EA . .00 089-05874-0005 SCR PHP 2-56X5/16 EA . 1. . 1. SUB-D. .00 . .00 089-06004-0003 SCR FHP 2-56X3/16 EA .00 . 1.00 090-00990-0003 PROTECTIVE CAP. . . 057-02203-0018 FLAVOR STCKR EA .00 .C. . 1. SUB-D.00 1.00 . . . . 200-06589-0002 SW BD 28V SW 1/2 EA 1. .500 W IN . 1. 1. . .00 .00 150-00020-0010 TUBING SHRINK 18G IN .00 150-00018-0010 TUBING SHRINK WHT IN . 088-01166-0008 INSERT -07 W/LENS EA 1. . 3. 9P EA . . . . 2. . 15P EA .00 037-00083-0000 KFS 576A DISPLAY EA .00 035-01909-0001 PROTECTIVE COVER EA . 1.00 089-05874-0004 SCR PHP 2-56X1/4 EA . 200-06626-0000 DRIVER BD EA . 1. . 2.00 . 2. .00 1. . 200-06579-0001 I/O BOARD ASSY EA . 073-00551-0004 KNOB W/H EA . 1.00 057-02888-0000 DECAL D. .00 1. . 1. . 1. . .00 . . . 200-06580-0000 MICROPROCESSOR BD EA . REF100 000-00388-0000 FLOW CHT KFS0576A RF . . 1. 057-01764-0002 WRN TAG 28V LGT EA 1. . . .00 . 1. . . 1. . MYLAR EA .00 057-01540-0000 WARNING HV TAG EA . 1. 1.KFS 576A PN DESCRIPTION REV ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------071-1276-15 XPDR CTRL GY 28V 2 071-1276-16 XPDR CTRL GY 5V 2 071-1276-18 XPDR CTRL BK 28V 2 071-1276-99 COMMON DFSD AD ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0015 -0016 -0018 -0099 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------REF1 300-03119-0000 FINAL ASSEMBLY RF . 00 . 1. 1. .00 016-01412-0000 LOCTITE 425 AR . . . . 1. . 1. 1. 1. . .00 . 1.00 073-00554-0008 KNOB W/H EA . . . .00 1. . EA . .500 W IN . 057-02203-0020 FLAVOR STCKR EA . .00 057-02888-0000 DECAL D. 1. . . . 200-06589-0005 SW BD 5V NO SW EA . . .00 1. . 1. . 1. 1.00 .00 057-02831-0001 KFS DUP S/N TAG EA . 2. . .00 057-02834-0000 ESD TAG EA . 1. 1.00 090-00990-0003 PROTECTIVE CAP.00 . . 012-01005-0002 TAPE MYLAR . 1. .00 . 089-05874-0003 SCR PHP 2-56X3/16 EA . .00 089-06000-0003 SCR FHP 0-80X3/16 EA .00 071-01276-0099 COMMON DFSD EA 1. . . REF4 004-00448-0000 MPS KFS0576A RF .00 . .00 . . .00 .00 . . SUB-D.C. . 057-01764-0002 WRN TAG 28V LGT EA 1.00 . . 200-06580-0000 MICROPROCESSOR BD EA . . 1. 1.00 091-00637-0002 INSULATOR.00 076-00111-0001 STAND-OFF . 057-02203-0019 FLAVOR STCKR EA 1. . .00 057-01764-0000 WRN TAG 5V LGT EA .00 089-06584-0000 SCR PHP 6-32X 1/2 EA . 2. 088-01166-0012 INSERT -11 W/LENS EA . 1. . 1.00 035-01909-0001 PROTECTIVE COVER EA . .00 . .00 .00 . 4. 073-00551-0004 KNOB W/H EA .00 047-05021-0002 COVER W/FINISH EA . 9P EA .00 1. 2. SUB-D. . . . .80 012-01127-0000 TAG COVER EA .40 200-06579-0000 I/O BOARD ASSY EA 1.00 . . 1. 200-06626-0000 DRIVER BD EA . 1.00 089-05874-0005 SCR PHP 2-56X5/16 EA . .00 . 1. 1. . . .O.00 150-00020-0010 TUBING SHRINK 18G IN . . 1. . .00 . .00 . . . MYLAR EA . . . 073-00504-0003 BEZEL BLK EA 1.00 089-05874-0004 SCR PHP 2-56X1/4 EA . 200-06579-0001 I/O BOARD ASSY EA . 1.00 200-06589-0004 SW BD 28V NO SW EA 1.00 088-01166-0010 INSERT -09 W/LENS EA 1.00 Rev 0.00 057-02890-0027 SCT KFS576A EA .00 . . 057-02203-0021 FLAVOR STCKR EA . 15P EA . . . 9. . .00 057-02742-0000 S/N TAG. . . 1. . 1. 3. . .00 090-00990-0001 PROTECTIVE CAP.00 . 4. . 073-00504-0004 BEZEL GRAY EA . 1. REF100 000-00388-0000 FLOW CHT KFS0576A RF . 057-02337-0000 PRTCTV CVR DECAL EA . . . 2. 1. 1. 1. 6-10 . KFS 576A EA .00 150-00018-0010 TUBING SHRINK WHT IN . . .00 .00 .00 1.00 037-00083-0000 KFS 576A DISPLAY EA .605 EA . Apr/2007 ©Honeywell International Inc.00 .00 .00 .00 . Do not print without express permission of Honeywell.KFS 576A PN DESCRIPTION REV ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------071-1276-19 XPDR CTRL BK 28V 2 071-1276-20 XPDR CTRL BK 5V 2 071-1276-21 XPDR CTRL GY 28V 2 071-1276-99 COMMON DFSD AD ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0019 -0020 -0021 -0099 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------REF1 300-03119-0000 FINAL ASSEMBLY RF . .00 057-01540-0000 WARNING HV TAG EA .00 089-05874-0006 SCR PHP 2-56X3/8 EA . 1.00 .00 089-06004-0003 SCR FHP 2-56X3/16 EA . 00 . 1. .00 . 1.00 091-00637-0002 INSULATOR. .00 . . .00 . . 1. . . 1.00 089-06004-0003 SCR FHP 2-56X3/16 EA . . 2. Do not print without express permission of Honeywell. . .C.00 057-01764-0000 WRN TAG 5V LGT EA 1. 200-06589-0006 SW BD 28V 1/2 EA .00 090-00990-0003 PROTECTIVE CAP. 1. SUB-D. 1. .O. . 057-02337-0000 PRTCTV CVR DECAL EA . .00 .00 150-00018-0010 TUBING SHRINK WHT IN . . 1. .00 057-02831-0001 KFS DUP S/N TAG EA . . . 1. . 1. . . .00 . .00 016-01412-0000 LOCTITE 425 AR .00 150-00020-0010 TUBING SHRINK 18G IN . 088-01166-0014 INSERT -13 W/LENS EA . 200-06580-0000 MICROPROCESSOR BD EA . .00 . 15P EA . 057-02203-0024 FLAVOR STCKR EA . 1. 1.00 . 073-00504-0003 BEZEL BLK EA . . 073-00554-0008 KNOB W/H EA . REF100 000-00388-0000 FLOW CHT KFS0576A RF . .00 . . 1.00 200-06589-0005 SW BD 5V NO SW EA 1. . . . . 1.00 089-05874-0005 SCR PHP 2-56X5/16 EA .00 057-02890-0027 SCT KFS576A EA . REF4 004-00448-0000 MPS KFS0576A RF . 3. 1. Apr/2007 ©Honeywell International Inc. . . 057-01764-0002 WRN TAG 28V LGT EA . 073-00504-0004 BEZEL GRAY EA 1.00 057-02888-0000 DECAL D.00 . .00 071-01276-0099 COMMON DFSD EA 1. . 1. 1. . 1. 1. 1. 1. . 4. . 1. 1.00 089-06584-0000 SCR PHP 6-32X 1/2 EA .00 057-02834-0000 ESD TAG EA . .00 . . .605 EA . .00 1. 1. . . 073-00551-0004 KNOB W/H EA .00 .80 012-01127-0000 TAG COVER EA . . 1. EA .00 Rev 0.00 089-06000-0003 SCR FHP 0-80X3/16 EA .500 W IN . .00 . .00 035-01909-0001 PROTECTIVE COVER EA . 1. 057-02203-0022 FLAVOR STCKR EA 1.00 1. .KFS 576A PN DESCRIPTION REV ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------071-1276-22 XPDR CTRL GY 5V 2 071-1276-23 XPDR CTRL BK 28V 2 071-1276-24 XPDR CTRL BK 5V 2 071-1276-99 COMMON DFSD AD ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0022 -0023 -0024 -0099 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------REF1 300-03119-0000 FINAL ASSEMBLY RF .00 . SUB-D.00 037-00083-0000 KFS 576A DISPLAY EA . 089-05874-0003 SCR PHP 2-56X3/16 EA . KFS 576A EA . 2. 4. . . . . 2.00 1.00 . . . 9.00 090-00990-0001 PROTECTIVE CAP.00 . . . .00 057-02742-0000 S/N TAG.00 . 1.00 .00 .00 . 1. . . 1. . . . .00 073-00553-0006 KNOB W/H EA .00 . . 200-06626-0000 DRIVER BD EA .00 089-05874-0004 SCR PHP 2-56X1/4 EA . 9P EA . 1. .40 200-06579-0000 I/O BOARD ASSY EA . 012-01005-0002 TAPE MYLAR .00 088-01166-0012 INSERT -11 W/LENS EA 1. . . 1.00 047-05021-0002 COVER W/FINISH EA . .00 .00 1.00 .00 057-01540-0000 WARNING HV TAG EA . 2. MYLAR EA . . . . .00 076-00111-0001 STAND-OFF . 200-06589-0007 SW BD 5V 1/2 EA . . 1.00 . .00 1. .00 089-05874-0006 SCR PHP 2-56X3/8 EA . 1. 200-06579-0001 I/O BOARD ASSY EA 1. 6-11 . .00 .00 . 057-02203-0023 FLAVOR STCKR EA .00 . 00 Rev 0.00 . Apr/2007 ©Honeywell International Inc. .00 .00 . . 1. .00 089-06000-0003 SCR FHP 0-80X3/16 EA .00 089-05874-0006 SCR PHP 2-56X3/8 EA . 1. 057-01764-0002 WRN TAG 28V LGT EA 1. 4. 1.00 091-00637-0002 INSULATOR.00 .00 . .00 090-00990-0001 PROTECTIVE CAP. 1. 200-06589-0007 SW BD 5V 1/2 EA .00 .00 016-01412-0000 LOCTITE 425 AR . .00 089-05874-0004 SCR PHP 2-56X1/4 EA . 9P EA . . . 9. . 073-00551-0004 KNOB W/H EA . 2.00 1. 1.KFS 576A PN DESCRIPTION REV ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------071-1276-25 XPDR CTRL BY 28V 2 071-1276-26 XPDR CTRL GY 5V 2 071-1276-99 COMMON DFSD AD ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0025 -0026 -0099 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------REF1 300-03119-0000 FINAL ASSEMBLY RF . . 1. 1. . 1. Do not print without express permission of Honeywell. 1.00 073-00553-0006 KNOB W/H EA 1. 057-02203-0025 FLAVOR STCKR EA 1. . .00 .00 057-02834-0000 ESD TAG EA .00 047-05021-0002 COVER W/FINISH EA . KFS 576A EA . . 1. 1. 1. .00 . . 073-00554-0008 KNOB W/H EA .500 W IN . 1. .00 037-00083-0000 KFS 576A DISPLAY EA .00 .00 .00 057-02888-0000 DECAL D. .00 035-01909-0001 PROTECTIVE COVER EA . .00 076-00111-0001 STAND-OFF . 012-01005-0002 TAPE MYLAR .00 089-05874-0005 SCR PHP 2-56X5/16 EA .605 EA .40 200-06579-0000 I/O BOARD ASSY EA 1.00 057-02831-0001 KFS DUP S/N TAG EA . 1.00 . .00 089-06584-0000 SCR PHP 6-32X 1/2 EA .00 200-06589-0006 SW BD 28V 1/2 EA 1.00 . .00 150-00020-0010 TUBING SHRINK 18G IN .00 .00 .80 012-01127-0000 TAG COVER EA . 1. 1. 2.00 . .00 071-01276-0099 COMMON DFSD EA 1.00 090-00990-0003 PROTECTIVE CAP. .00 088-01166-0016 INSERT -15 W/LENS EA 1. . 1. . . . . 1. 6-12 . 3. 1. 2.00 . 200-06579-0001 I/O BOARD ASSY EA . 200-06580-0000 MICROPROCESSOR BD EA . 057-02203-0026 FLAVOR STCKR EA .O. 089-05874-0003 SCR PHP 2-56X3/16 EA . MYLAR EA . 15P EA . . 1. SUB-D. . REF4 004-00448-0000 MPS KFS0576A RF .00 089-06004-0003 SCR FHP 2-56X3/16 EA . .00 057-01540-0000 WARNING HV TAG EA .00 . 200-06626-0000 DRIVER BD EA . . 073-00504-0004 BEZEL GRAY EA 1. 1.00 150-00018-0010 TUBING SHRINK WHT IN . 1. 1. EA .00 1. REF100 000-00388-0000 FLOW CHT KFS0576A RF . .00 1. 057-02337-0000 PRTCTV CVR DECAL EA .00 1.C.00 057-02742-0000 S/N TAG. .00 057-01764-0000 WRN TAG 5V LGT EA . . 2. 1.00 057-02890-0027 SCT KFS576A EA . . SUB-D. 1.00 . 4. 6-13 . Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. Rev 0.KFS 576A THE FOLLOWING IS THE PARTS LIST FROM THE PREVIOUS REVISION AND IS PROVIDED FOR REFERENCE ONLY. KFS 576A Rev 0. Do not print without express permission of Honeywell. 6-14 . Apr/2007 ©Honeywell International Inc. KFS 576A Rev 0. Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. 6-15 . KFS 576A Rev 0. 6-16 . Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. Apr/2007 ©Honeywell International Inc. 6-17 . Do not print without express permission of Honeywell.KFS 576A Figure 6-2 Final Assembly (Dwg No 300-03119-0000 Rev AD) Rev 0. 6-18 . Apr/2007 ©Honeywell International Inc.KFS 576A Rev 0. Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. 6-19 .KFS 576A Figure 6-3 Final Assembly (Dwg No 300-03119-0000 Rev 7) (For Reference Only) Rev 0. Do not print without express permission of Honeywell. KFS 576A Rev 0. Do not print without express permission of Honeywell. 6-20 . Apr/2007 ©Honeywell International Inc. .00 L105 013-00006-0003 FERR BEAD EA .00 CJ101 026-00018-0001 WIRE CKTJMPR 24AWG EA . .00 CR116 007-06016-0000 DIO S 1N4154 EA . . 1.00 CR103 007-06016-0000 DIO S 1N4154 EA . . . . . 1. C104 999-09999-0098 PLACE HOLDER RF . 1. 1.1UF 50V EA . 1. 1. 1.00 . 1. . .00 L101 013-00006-0003 FERR BEAD EA . 1. 1. 1. .00 I106 120-03116-0003 IC LM137H EA . 1. 1. 1. . 1.00 CR104 007-06016-0000 DIO S 1N4154 EA . 1.00 CR123 007-06025-0000 DIO S 1N4003 EA .00 CR110 007-06016-0000 DIO S 1N4154 EA .00 CR106 007-06016-0000 DIO S 1N4154 EA . .00 C103 999-09999-0098 PLACE HOLDER RF . CR101 007-06016-0000 DIO S 1N4154 EA . 1. 1. . . 1. 1.00 I103 120-03174-0001 IC TDB0082FP EA .00 CR113 007-06016-0000 DIO S 1N4154 EA . 1.00 .00 C111 111-00001-0066 CAP CR 33PF 50V EA .00 . 6-21 .00 CR119 007-06016-0000 DIO S 1N4154 EA 1.1UF 50V EA .00 I105 120-03174-0001 IC TDB0082FP EA . 1.00 CR112 007-06016-0000 DIO S 1N4154 EA . . .00 L103 013-00006-0003 FERR BEAD EA . 1. . . . CR120 007-06025-0000 DIO S 1N4003 EA . . .00 C114 111-00001-0017 CAP CR 180PF 50V EA . 1.00 C112 111-00001-0066 CAP CR 33PF 50V EA . . 1.00 J102 030-02322-0019 HEADER 19P EA . 1.00 CR111 007-06016-0000 DIO S 1N4154 EA .00 C110 111-00001-0017 CAP CR 180PF 50V EA . . 1. .00 L102 013-00006-0003 FERR BEAD EA . Do not print without express permission of Honeywell. . 1. 1.00 CR102 007-06016-0000 DIO S 1N4154 EA . 1. 1.00 CR122 007-06025-0000 DIO S 1N4003 EA . . . 1.00 1. . . . 1. . .00 . C108 111-00001-0001 CAP CR .KFS 576A PN DESCRIPTION REV ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------200-06579-0000 I/O BOARD ASSY AA 200-06579-0001 I/O BOARD ASSY 3 200-06579-0099 COMMON I/O BD ASSY AA ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0000 -0001 -0099 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------C101 111-00001-0017 CAP CR 180PF 50V EA .00 I101 120-06116-0000 IC HEF4512BTD EA . 1. 1.00 CR117 007-06016-0000 DIO S 1N4154 EA .00 . 1. 1. CJ102 026-00018-0001 WIRE CKTJMPR 24AWG EA 1. Apr/2007 ©Honeywell International Inc.00 I104 120-03174-0001 IC TDB0082FP EA .00 C106 096-01082-0005 CAP TN 10UF 20V EA .00 C113 111-00001-0017 CAP CR 180PF 50V EA . 1. 1.00 C115 111-00001-0017 CAP CR 180PF 50V EA . . . .00 C109 111-00001-0001 CAP CR .00 CR118 007-06016-0000 DIO S 1N4154 EA . . .00 J101 030-02458-0014 CONN STRGT 14P EA .00 CR121 007-06025-0000 DIO S 1N4003 EA . 1.00 CR114 007-06016-0000 DIO S 1N4154 EA .00 . 11.00 L104 013-00006-0003 FERR BEAD EA . . .00 CR105 007-06016-0000 DIO S 1N4154 EA . 1.00 . 1. 1.00 C102 111-00001-0017 CAP CR 180PF 50V EA .00 CR115 007-06016-0000 DIO S 1N4154 EA .00 J5762 030-02346-0008 CONN SUB-D CA 9P EA . 1.00 CR107 007-06016-0000 DIO S 1N4154 EA .00 . .00 CR108 007-06016-0000 DIO S 1N4154 EA . . C105 096-01082-0010 CAP TN 10UF 35V EA .00 Rev 0. .00 J5761 030-02358-0007 CONN SUB-D PC 29P EA . 1.00 C107 999-09999-0098 PLACE HOLDER RF . 1. . . 1. 1. . .00 .00 J103 030-02174-0004 PIN CONTACT EA .00 CR109 007-06016-0000 DIO S 1N4154 EA . . .00 I102 120-06116-0000 IC HEF4512BTD EA . . . 1. 1. . 1. 1. 1. 1. 1.00 R111 131-00223-0013 RES CF 22K EW 5% EA .00 R125 131-00273-0013 RES CF 27K EW 5% EA . .00 R124 131-00273-0013 RES CF 27K EW 5% EA . 1. . . 1. .00 L123 013-00006-0003 FERR BEAD EA .00 Q109 007-00467-0000 XSTR S NPN MMBTA06 EA .00 R116 131-00223-0013 RES CF 22K EW 5% EA . 1.00 L121 013-00006-0003 FERR BEAD EA .00 L113 013-00006-0003 FERR BEAD EA . . 1.00 Q101 007-00467-0000 XSTR S NPN MMBTA06 EA .00 R128 131-00102-0013 RES CF 1K EW 5% EA . . 1.00 R120 131-00223-0013 RES CF 22K EW 5% EA . 1. . 1.00 L107 013-00006-0003 FERR BEAD EA . 1.00 L128 013-00006-0003 FERR BEAD EA . 6-22 . 1. Do not print without express permission of Honeywell.00 R113 131-00223-0013 RES CF 22K EW 5% EA .00 L122 999-09999-0098 PLACE HOLDER RF .00 R123 131-00102-0013 RES CF 1K EW 5% EA . 1. . . 1.00 Q105 007-00467-0000 XSTR S NPN MMBTA06 EA . 1. .00 R106 131-00223-0013 RES CF 22K EW 5% EA . 1. . 1. .00 Q102 007-00466-0000 XSTR S PNP MMBTA56 EA .00 L129 013-00006-0003 FERR BEAD EA . . 1.00 R115 131-00223-0013 RES CF 22K EW 5% EA .00 R105 131-00223-0013 RES CF 22K EW 5% EA . 1. 1. 1.00 Rev 0. . . . 1.00 L119 013-00006-0003 FERR BEAD EA . . . 1.00 L110 013-00006-0003 FERR BEAD EA . 1. 1. 1. 1.00 L114 013-00006-0003 FERR BEAD EA . . 1.KFS 576A ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0000 -0001 -0099 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------L106 013-00006-0003 FERR BEAD EA . .00 Q108 007-00467-0000 XSTR S NPN MMBTA06 EA . 1. 1. . . 1. 1. . 1. . . . .00 L124 013-00006-0003 FERR BEAD EA .00 Q106 007-00467-0000 XSTR S NPN MMBTA06 EA .00 R119 131-00223-0013 RES CF 22K EW 5% EA .00 L120 013-00006-0003 FERR BEAD EA . 1. . 1. 1. .00 R127 131-00203-0013 RES CF 20K EW 5% EA . 1.00 Q103 007-00467-0000 XSTR S NPN MMBTA06 EA .00 R118 131-00103-0013 RES CF 10K EW 5% EA .00 R117 131-00103-0013 RES CF 10K EW 5% EA .00 R109 131-00223-0013 RES CF 22K EW 5% EA . 1. .00 R126 131-00203-0013 RES CF 20K EW 5% EA . .00 Q107 007-00466-0000 XSTR S PNP MMBTA56 EA .00 R104 131-00223-0013 RES CF 22K EW 5% EA . .00 R107 131-00223-0013 RES CF 22K EW 5% EA . 1. 1.00 L116 013-00006-0003 FERR BEAD EA . 1. . .00 R103 131-00223-0013 RES CF 22K EW 5% EA . 1. 1. .00 Q110 007-00466-0000 XSTR S PNP MMBTA56 EA . . 1. 1. .00 R112 131-00223-0013 RES CF 22K EW 5% EA . .00 R110 131-00223-0013 RES CF 22K EW 5% EA . . .00 L117 013-00006-0003 FERR BEAD EA . . . .00 L111 013-00006-0003 FERR BEAD EA . 1. . . 1.00 L108 013-00006-0003 FERR BEAD EA . . 1. 1. .00 L109 013-00006-0003 FERR BEAD EA . 1.00 L112 013-00006-0003 FERR BEAD EA .00 L126 013-00006-0003 FERR BEAD EA .00 R122 131-00330-0023 RES CF 33 QW 5% EA . 1. .00 L127 013-00006-0003 FERR BEAD EA . 1. .00 L118 013-00006-0003 FERR BEAD EA . 1.00 L125 013-00006-0003 FERR BEAD EA . . 1. . . Apr/2007 ©Honeywell International Inc.00 Q104 007-00466-0000 XSTR S PNP MMBTA56 EA . . . .00 R114 131-00223-0013 RES CF 22K EW 5% EA . .00 R102 131-00223-0013 RES CF 22K EW 5% EA . 1. . . 1. .00 R121 131-00360-0023 RES CF 36 QW 5% EA .00 L115 013-00006-0003 FERR BEAD EA . .00 R101 131-00223-0013 RES CF 22K EW 5% EA . 1. . 1. .00 R108 131-00223-0013 RES CF 22K EW 5% EA . . 1. 1. .00 TP105 008-00096-0001 TERMINAL TEST PNT EA . 1. .00 025-00018-0022 WIRE 26 RED IN .00 R137 131-00104-0013 RES CF 100K EW 5% EA .00 . 6-23 .00 R160 131-00241-0013 RES CF 240 EW 5% EA . 1. 1.00 R136 131-00330-0023 RES CF 33 QW 5% EA . . 1. R143 999-09999-0098 PLACE HOLDER RF .00 R139 131-00104-0013 RES CF 100K EW 5% EA . .00 .00 R158 131-00103-0013 RES CF 10K EW 5% EA . .00 . 1.00 009-06579-0000 PC BD I/O EA .00 . R148 999-09999-0098 PLACE HOLDER RF .00 .00 .00 025-00018-0044 WIRE 26 YEL IN . 1. R151 131-00103-0013 RES CF 10K EW 5% EA . . . .00 073-00454-0004 CAST MOD W/F EA . .00 U102 015-00039-0000 RES MOD 10K150V2% EA . . 6.00 R161 131-00162-0013 RES CF 1. 1. 008-00038-0001 TERM BIFUR . 6. .00 . . 1. 6.00 R157 131-00102-0013 RES CF 1K EW 5% EA . 1. 1.00 R132 131-00273-0013 RES CF 27K EW 5% EA .00 TP104 008-00096-0001 TERMINAL TEST PNT EA . . 1.6K EW 5% EA .00 Rev 0. 6.00 . 1.00 R164 131-00104-0013 RES CF 100K EW 5% EA . . 1. .084L EA . R144 999-09999-0098 PLACE HOLDER RF .00 R138 131-00104-0013 RES CF 100K EW 5% EA . 1.00 R140 131-00104-0013 RES CF 100K EW 5% EA . 1. 1. . 1.00 . .00 R159 131-00102-0013 RES CF 1K EW 5% EA . 1.00 089-05874-0004 SCR PHP 2-56X1/4 EA .00 . R150 999-09999-0098 PLACE HOLDER RF . 1. 1.00 R153 131-00103-0013 RES CF 10K EW 5% EA .00 REF1 300-06579-0000 I/O BOARD RF . 1. R149 999-09999-0098 PLACE HOLDER RF . 1.00 R163 131-00103-0013 RES CF 10K EW 5% EA . . . . 1. .00 R141 131-00822-0013 RES CF 8. .00 . .2K EW 5% EA . .00 R134 131-00102-0013 RES CF 1K EW 5% EA . . 6.00 .00 076-00741-0011 STANDOFF .00 TP101 008-00096-0001 TERMINAL TEST PNT EA . .00 025-00018-0033 WIRE 26 ORG IN .00 U101 015-00039-0000 RES MOD 10K150V2% EA .00 TP102 008-00096-0001 TERMINAL TEST PNT EA . 6. .00 R156 131-00102-0013 RES CF 1K EW 5% EA .00 . . Apr/2007 ©Honeywell International Inc. 6. .00 R130 131-00203-0013 RES CF 20K EW 5% EA . R145 999-09999-0098 PLACE HOLDER RF .00 U104 015-00064-0013 8P CAP 220PF 10% EA . 3. . .00 R131 131-00203-0013 RES CF 20K EW 5% EA . 1.00 .00 016-01040-0000 COATING TYPE AR AR . .120 EA .00 076-00741-0009 STANDOFF . . 1.00 R155 131-00433-0013 RES CF 43K EW 5% EA . 1. 1.00 U105 015-00064-0013 8P CAP 220PF 10% EA .00 R133 131-00273-0013 RES CF 27K EW 5% EA . . 1. . . .00 030-02352-0000 LOCK TAB EA . . 1.00 .00 R135 131-00360-0023 RES CF 36 QW 5% EA . 1.00 R162 131-00103-0013 RES CF 10K EW 5% EA . . 1. . 2. . .00 025-00018-0055 WIRE 26 GRN IN . 1. Do not print without express permission of Honeywell.00 . . .00 R154 131-00103-0013 RES CF 10K EW 5% EA . .00 . 1.00 . .00 025-00018-0011 WIRE 26 BRN IN . 1.00 .00 R142 999-09999-0098 PLACE HOLDER RF . . 1.120 EA .00 TP103 008-00096-0001 TERMINAL TEST PNT EA . R146 999-09999-0098 PLACE HOLDER RF . 1.00 R152 131-00103-0013 RES CF 10K EW 5% EA .00 . .00 002-06579-0000 SCH I/O BD KFS 576A RF . 1. 1.KFS 576A ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0000 -0001 -0099 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------R129 131-00102-0013 RES CF 1K EW 5% EA . .00 025-00018-0066 WIRE 26 BLU IN . . . R147 999-09999-0098 PLACE HOLDER RF . 1. 6. .00 . .00 U103 015-00064-0013 8P CAP 220PF 10% EA . Rev 0.00 1.00 150-00018-0010 TUBING SHRINK WHT AR .00 091-00109-0000 CABLE TIE EA . .KFS 576A ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0000 -0001 -0099 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------091-00025-0000 WSHR XSTR INSUL EA .00 200-06579-0099 COMMON I/O BD ASSY EA 1. . 1. . . 6-24 .00 . Do not print without express permission of Honeywell. 1. 2. Apr/2007 ©Honeywell International Inc.00 .00 192-06579-0000 KFS 576A I/O BOARD ASSY RF . Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.KFS 576A THE FOLLOWING IS THE PARTS LIST FROM THE PREVIOUS REVISION AND IS PROVIDED FOR REFERENCE ONLY. 6-25 . Rev 0. Apr/2007 ©Honeywell International Inc.KFS 576A Rev 0. 6-26 . Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.KFS 576A Rev 0. 6-27 . KFS 576A Rev 0. 6-28 . Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. KFS 576A Figure 6-4 I/O Board (Dwg No 300-06570-0000 Rev 1) Rev 0. Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. 6-29 . 6-30 .KFS 576A Rev 0. Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 6-31 . Apr/2007 ©Honeywell International Inc.KFS 576A Figure 6-5 I/O Board (Dwg No 300-06579-0000 Rev 0) (For Reference Only) Rev 0. Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.KFS 576A Rev 0. 6-32 . KFS 576A Figure 6-6 I/O Board Schematic (Dwg No 002-06579-0000 Rev 3) (Sheet 1 of 2) Rev 0. Apr/2007 ©Honeywell International Inc. 6-33 . Do not print without express permission of Honeywell. 6-34 .KFS 576A Rev 0. Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. 6-35 . Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.KFS 576A Figure 6-6 I/O Board Schematic (Dwg No 002-06579-0000 Rev 3) (Sheet 2 of 2) Rev 0. KFS 576A Rev 0. 6-36 . Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 00 R225 131-00472-0013 RES CF 4. INDUSTRIAL EA 1.00 R210 131-00302-0013 RES CF 3K EW 5% EA 1. Do not print without express permission of Honeywell.00 C203 111-00001-0013 CAP CR .00 I203 125-00035-0001 576A DSPLY MICRO EA 1.00 R217 131-00912-0013 RES CF 9.1UF 50V EA 1.00 I205 120-06025-0001 IC SCL4049ABC+ EA 1.00 R212 131-00102-0013 RES CF 1K EW 5% EA 1.00 R203 131-00153-0013 RES CF 15K EW 5% EA 1.00 R208 131-00102-0013 RES CF 1K EW 5% EA 1.00 TP208 008-00096-0001 TERMINAL TEST PNT EA 1.1UF 50V EA 1. INDUSTRIAL EA 1.00 I207 120-03127-0008 IC LM2903N DIP.00 R204 131-00103-0013 RES CF 10K EW 5% EA 1.00 R220 131-00823-0013 RES CF 82K EW 5% EA 1.00 C208 096-01082-0015 CAP TN 2. Apr/2007 ©Honeywell International Inc.00 002-06580-0000 SCH UPROCESSOR BD RF .00 TP206 008-00096-0001 TERMINAL TEST PNT EA 1.00 R202 131-00752-0013 RES CF 7.5K EW 5% EA 1.00 R223 131-00223-0013 RES CF 22K EW 5% EA 1.00 R213 131-00752-0013 RES CF 7.00 I206 120-03127-0008 IC LM2903N DIP.00 R221 131-00204-0013 RES CF 200K EW 5% EA 1.00 TP204 008-00096-0001 TERMINAL TEST PNT EA 1.00 R214 131-00622-0013 RES CF 6.00 R218 131-00682-0013 RES CF 6.00 TP202 008-00096-0001 TERMINAL TEST PNT EA 1.00 C202 111-00001-0013 CAP CR .00 R224 131-00473-0013 RES CF 47K EW 5% EA 1.00 R201 131-00103-0013 RES CF 10K EW 5% EA 1.00 Y201 044-00128-0000 CR RSNR 11.00 C204 111-00001-0077 CAP CR 12PF 100V EA 1.00 I204 120-03127-0008 IC LM2903N DIP.00 R211 131-00302-0013 RES CF 3K EW 5% EA 1.00 TP207 008-00096-0001 TERMINAL TEST PNT EA 1.00 TP205 008-00096-0001 TERMINAL TEST PNT EA 1.00 TP203 008-00096-0001 TERMINAL TEST PNT EA 1.00 R209 131-00102-0013 RES CF 1K EW 5% EA 1.2K EW 5% EA 1.8K EW 5% EA 1.00 R206 131-00103-0013 RES CF 10K EW 5% EA 1.0MHZ EA 1.00 I202 125-00036-0000 429 I/O MICRO EA 1.00 R222 131-00223-0013 RES CF 22K EW 5% EA 1.5K EW 5% EA 1.00 I201 120-02119-0000 NONVOLATILE RAM EA 1.00 R205 131-00103-0013 RES CF 10K EW 5% EA 1.2UF 15V EA 1.00 R216 131-00105-0013 RES CF 1M EW 5% EA 1.00 C206 111-00001-0077 CAP CR 12PF 100V EA 1.00 TP201 008-00096-0001 TERMINAL TEST PNT EA 1.00 R215 131-00105-0013 RES CF 1M EW 5% EA 1. INDUSTRIAL EA 1.00 Q202 007-00180-0000 XSTR S NPN 2N4401 EA 1.00 R219 131-00822-0013 RES CF 8.7K EW 5% EA 1.0MHZ EA 1. RF .KFS 576A PN DESCRIPTION REV ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------200-06580-0000 MICROPROCESSOR BD AA ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------C201 111-00001-0032 CAP CR 1UF 50V EA 1.00 KFS 576A Rev 0.1K EW 5% EA 1.00 Q203 007-00180-0000 XSTR S NPN 2N4401 EA 1.00 P201 030-01117-0000 RECEPTACLE EA 13.00 C205 111-00001-0077 CAP CR 12PF 100V EA 1.00 R207 131-00102-0013 RES CF 1K EW 5% EA 1.00 C207 111-00001-0077 CAP CR 12PF 100V EA 1.2K EW 5% EA 1.00 Y202 044-00128-0000 CR RSNR 11. 6-37 .00 P202 030-01117-0000 RECEPTACLE EA 19.00 Q201 007-00180-0000 XSTR S NPN 2N4401 EA 1.00 REF1 300-06580-0000 MICROPROCESSOR BD. 00 192-06580-0000 KFS 576A MICROPROCESSOR RF . Do not print without express permission of Honeywell.00 033-00092-0012 IC DIP SCKT 18C EA 1. Apr/2007 ©Honeywell International Inc.00 033-00114-0017 SCKT IC DIP 40C EA 2.00 016-01040-0000 COATING TYPE AR AR .KFS 576A ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------009-06580-0000 PC BD UPROCESSOR EA 1.00 BD ASSY Rev 0. 6-38 . 6-39 . Apr/2007 ©Honeywell International Inc.KFS 576A THE FOLLOWING IS THE PARTS LIST FROM THE PREVIOUS REVISION AND IS PROVIDED FOR REFERENCE ONLY. Do not print without express permission of Honeywell. Rev 0. 6-40 . Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc.KFS 576A Rev 0. KFS 576A Figure 6-7 Microprocessor Board (Dwg No 300-06580-0000 Rev 4) Rev 0. Apr/2007 ©Honeywell International Inc. 6-41 . Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc.KFS 576A Rev 0. Do not print without express permission of Honeywell. 6-42 . Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. 6-43 .KFS 576A Figure 6-8 Microprocessor Board (Dwg No 300-06580-0000 Rev 1) (For Reference Only) Rev 0. KFS 576A Rev 0. Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. 6-44 . KFS 576A Figure 6-9 Microprocessor Board Schematic (Dwg No 002-06580-0000 Rev 7) Rev 0. Apr/2007 ©Honeywell International Inc. 6-45 . Do not print without express permission of Honeywell. 6-46 . Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.KFS 576A Rev 0. KFS 576A Figure 6-10 Microprocessor Board Schematic (Dwg No 002-06580-0000 Rev 6) (For Reference Only) Rev 0. 6-47 . Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. Do not print without express permission of Honeywell.KFS 576A Rev 0. Apr/2007 ©Honeywell International Inc. 6-48 . . 1. . S401 031-00443-0001 SW ROTARY AJ-20 EA .20 030-01185-0000 CONNECTOR SOCKET EA .00 S403 031-00399-0002 SWITCH ASSY IDT EA . 1. .025 EA . .00 012-01299-0000 INSULATING WASHER EA . . .00 . S402 031-00372-0001 SWITCH SLIDE SPDT EA . DS402 037-00034-0000 LMP 7715 T1 5V EA . 6-49 . 1.00 073-00550-0002 SHAFT W/F EA . .00 REF1 300-06589-0000 SWITCH BD KFS 576A RF .00 . . 7. 2. 1. . . . . 1. . .00 CR403 007-06016-0000 DIO S 1N4154 EA .00 R402 131-00334-0013 RES CF 330K EW 5% EA . . . 1. . 1.00 DS401 037-00034-0000 LMP 7715 T1 5V EA . 1.00 088-01053-0000 SWITCH HOUSING EA . . .125 EA .00 088-00971-0000 SPCR PHOTODETECTOR EA . . 1. . .00 . 1. 25. 1. 1.00 . . 1.00 078-00116-0000 SPRING COMPRESSION EA . . . .KFS 576A PN DESCRIPTION REV ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------200-06589-0000 SW BD 28V W/SW 3 200-06589-0001 SW BD 5V W/SW 3 200-06589-0002 SW BD 28V SW 1/2 3 200-06589-0099 COMMON BM AB ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0000 -0001 -0002 -0099 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------CR401 007-06016-0000 DIO S 1N4154 EA .00 . 1.00 CR406 007-06016-0000 DIO S 1N4154 EA .00 088-01084-0000 SWITCH HOUSING EA . . Apr/2007 ©Honeywell International Inc. 1. . 1. 1. .00 089-08023-0030 WSHR FLT STD #2 EA . P402 030-02200-0008 VERT CRD CONN 8P EA . 1. DS402 037-00034-0001 LMP 7839 T1 28V EA 1. . 1. .00 047-05798-0001 DETENT SPRING . .00 092-05009-0004 RVT BH 1/16X. . 1. . 1.00 R401 131-00334-0013 RES CF 330K EW 5% EA .00 .00 CR408 007-06016-0000 DIO S 1N4154 EA .00 1.00 089-02136-0000 NUT LOCK 2-56 EA . 2. .00 088-00769-0000 SLEEVE LOCKING EA .00 047-05798-0000 DETENT SPRING . . . . .00 047-06689-0002 BRACKET ASSEMBLED EA . . 2. 1.051 EA .00 1. 1.00 090-00019-0005 RING RTNR . . . . . . S401 031-00443-0003 SWITCH 2P EA 1. . .00 155-02169-0000 CABLE ASSY SW BD EA . . 1. . DS401 037-00034-0001 LMP 7839 T1 28V EA 1. . 1. .00 V401 134-05005-0000 PHOTODETECTOR EA . . . 1. . 2. 1. .00 . . .00 CR402 007-06016-0000 DIO S 1N4154 EA .00 088-01022-0001 CONTACT ASSY EA . 1.00 R404 131-00334-0013 RES CF 330K EW 5% EA .00 CR407 007-06016-0000 DIO S 1N4154 EA . . .00 009-06589-0000 PC BD SWITCH EA . 1. . 1. 1. . . . 2.00 1. . 1. . . . 1. Rev 0.00 . .00 016-01040-0000 COATING TYPE AR AR . 3.030 EA . 1.00 073-00505-0002 BRACKET EA . 1.00 CR404 007-06016-0000 DIO S 1N4154 EA .00 R403 131-00334-0013 RES CF 330K EW 5% EA . . . . . . Do not print without express permission of Honeywell. 1. . .00 P404 030-02200-0008 VERT CRD CONN 8P EA .00 .00 .00 089-06004-0003 SCR FHP 2-56X3/16 EA .00 CR405 007-06016-0000 DIO S 1N4154 EA .00 200-06589-0099 COMMON BM EA 1. . .00 076-01232-0003 SHAFT W/F EA . . . . 1. 2. . .00 . . . . . .00 . .00 025-00018-0099 WIRE 26 WHT IN .00 090-00036-0004 RING RTNR . .00 076-01433-0001 SPOOL W/F EA .00 089-05899-0011 SCR PHP 2-56X11/16 EA . . . 1. .00 016-01013-0000 VAC GREASE DC 976 AR . .188 EA . . 1.00 DS401 037-00034-0000 LMP 7715 T1 5V EA 1.00 R402 131-00334-0013 RES CF 330K EW 5% EA . 25. 1. 1.00 073-00505-0002 BRACKET EA . 24AWG. 1.00 . .00 088-00769-0000 SLEEVE LOCKING EA . .00 090-00019-0005 RING RTNR . 1.00 078-00116-0000 SPRING COMPRESSION EA . 1. . . 1. 1. CU. . . . . 1. 1. .00 047-05798-0001 DETENT SPRING . 1. . . . . . 1. .00 088-01084-0000 SWITCH HOUSING EA .00 090-00036-0004 RING RTNR . .00 092-05009-0004 RVT BH 1/16X. . .00 089-08023-0030 WSHR FLT STD #2 EA . . S402 031-00372-0001 SWITCH SLIDE SPDT EA . . Do not print without express permission of Honeywell. 24AWG.00 CR405 007-06016-0000 DIO S 1N4154 EA . . .00 . . 1. . . DS402 037-00034-0001 LMP 7839 T1 28V EA . .00 . 1.00 076-01232-0003 SHAFT W/F EA . . .00 073-00550-0002 SHAFT W/F EA . . . . . . 2. 1. 2.00 025-00018-0099 WIRE 26 WHT IN . . . . 1. . 1.00 . Apr/2007 ©Honeywell International Inc. 1. 2. 1. . 2. . .00 . CU. . . 1.00 088-01022-0001 CONTACT ASSY EA .00 R403 131-00334-0013 RES CF 330K EW 5% EA .00 200-06589-0099 COMMON BM EA 1. . .00 .00 V401 134-05005-0000 PHOTODETECTOR EA . .00 089-02136-0000 NUT LOCK 2-56 EA . . 1. 1. .00 012-01299-0000 INSULATING WASHER EA . . 1. . .051 EA . . .00 016-01013-0000 VAC GREASE DC 976 AR . 1.00 088-00971-0000 SPCR PHOTODETECTOR EA . .00 CR403 007-06016-0000 DIO S 1N4154 EA . 1. 2. . DS402 037-00034-0000 LMP 7715 T1 5V EA 1. . . .00 S403 031-00399-0002 SWITCH ASSY IDT EA . . 3. DS401 037-00034-0001 LMP 7839 T1 28V EA . 7. . 2. .00 R401 131-00334-0013 RES CF 330K EW 5% EA .00 P404 030-02200-0008 VERT CRD CONN 8P EA . . . 1.00 . . . . . .00 089-06004-0003 SCR FHP 2-56X3/16 EA . .00 CR402 007-06016-0000 DIO S 1N4154 EA . TINNED IN . . .025 EA .00 CR407 007-06016-0000 DIO S 1N4154 EA .00 .00 . . .00 088-01053-0000 SWITCH HOUSING EA . TINNED IN .00 CR408 007-06016-0000 DIO S 1N4154 EA . .00 CR404 007-06016-0000 DIO S 1N4154 EA . . . 1. 1. 1. 1.00 047-05798-0000 DETENT SPRING . .00 009-06589-0000 PC BD SWITCH EA . . .00 CR406 007-06016-0000 DIO S 1N4154 EA . 1. 1.125 EA . 030-01185-0000 CONNECTOR SOCKET EA .188 EA . 1. . . . . .030 EA .00 089-05899-0011 SCR PHP 2-56X11/16 EA .00 076-01433-0001 SPOOL W/F EA . . P402 030-02200-0008 VERT CRD CONN 8P EA .20 026-00030-0000 WIRE.00 REF1 300-06589-0000 SWITCH BD KFS 576A RF . . . . S401 031-00443-0001 SW ROTARY AJ-20 EA 1.KFS 576A PN DESCRIPTION REV ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------200-06589-0003 SW BD 5V SW 1/2 3 200-06589-0004 SW BD 28V NO SW 4 200-06589-0005 SW BD 5V NO SW AA 200-06589-0099 COMMON BM AB ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0003 -0004 -0005 -0099 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------CJ1 026-00030-0000 WIRE. 1. . 1.00 . . .00 016-01040-0000 COATING TYPE AR AR . 1. 1.00 . CR401 007-06016-0000 DIO S 1N4154 EA . . .00 . Rev 0. .00 1.00 1. . .00 . .00 155-02169-0000 CABLE ASSY SW BD EA .00 047-06689-0002 BRACKET ASSEMBLED EA . 6-50 .00 R404 131-00334-0013 RES CF 330K EW 5% EA . 1. 1. 00 R404 131-00334-0013 RES CF 330K EW 5% EA . S402 031-00372-0001 SWITCH SLIDE SPDT EA .00 073-00550-0002 SHAFT W/F EA . . . . P402 030-02200-0008 VERT CRD CONN 8P EA .00 CR405 007-06016-0000 DIO S 1N4154 EA . . .188 EA . 1.20 030-01185-0000 CONNECTOR SOCKET EA . . 1. .00 R403 131-00334-0013 RES CF 330K EW 5% EA .125 EA . 3.00 016-01040-0000 COATING TYPE AR AR .051 EA . 1. 2. 1. . . . . 1.00 1. 1. 1. 6-51 .00 047-05798-0001 DETENT SPRING . 1.KFS 576A PN DESCRIPTION REV ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------200-06589-0006 SW BD 28V 1/2 3 200-06589-0007 SW BD 5V 1/2 1 200-06589-0099 COMMON BM AB ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0006 -0007 -0099 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------CR401 007-06016-0000 DIO S 1N4154 EA . 1.00 089-06004-0003 SCR FHP 2-56X3/16 EA .00 155-02169-0000 CABLE ASSY SW BD EA . . . Apr/2007 ©Honeywell International Inc. 1.00 DS401 037-00034-0000 LMP 7715 T1 5V EA . 1.00 CR404 007-06016-0000 DIO S 1N4154 EA . 1.00 CR403 007-06016-0000 DIO S 1N4154 EA .025 EA . 1. .00 088-01053-0000 SWITCH HOUSING EA . . . 7.00 CR407 007-06016-0000 DIO S 1N4154 EA . 1.00 047-05798-0000 DETENT SPRING .00 R401 131-00334-0013 RES CF 330K EW 5% EA . . 1.00 .00 089-08023-0030 WSHR FLT STD #2 EA .00 047-06689-0002 BRACKET ASSEMBLED EA . Rev 0. . 1. . . . DS402 037-00034-0001 LMP 7839 T1 28V EA 1. 1. .00 .00 016-01013-0000 VAC GREASE DC 976 AR . .00 090-00036-0004 RING RTNR . .00 090-00019-0005 RING RTNR . . . . 2.00 1. 1. . .00 088-01022-0001 CONTACT ASSY EA .00 P404 030-02200-0008 VERT CRD CONN 8P EA . 1. 1.00 089-05899-0011 SCR PHP 2-56X11/16 EA .00 . .00 S403 031-00399-0002 SWITCH ASSY IDT EA . 2. 1.00 . 1.00 012-01299-0000 INSULATING WASHER EA .00 . DS402 037-00034-0000 LMP 7715 T1 5V EA . . 2.00 088-00971-0000 SPCR PHOTODETECTOR EA . 25.00 009-06589-0000 PC BD SWITCH EA . 1. 1. 1. . 1.00 088-00769-0000 SLEEVE LOCKING EA .00 CR408 007-06016-0000 DIO S 1N4154 EA . . . Do not print without express permission of Honeywell.00 088-01084-0000 SWITCH HOUSING EA . .00 CR402 007-06016-0000 DIO S 1N4154 EA .00 092-05009-0004 RVT BH 1/16X. 1. . 2. .00 REF1 300-06589-0000 SWITCH BD KFS 576A RF .00 .030 EA .00 076-01232-0003 SHAFT W/F EA . . 1.00 076-01433-0001 SPOOL W/F EA . .00 200-06589-0099 COMMON BM EA 1. .00 089-02136-0000 NUT LOCK 2-56 EA . 2. DS401 037-00034-0001 LMP 7839 T1 28V EA 1.00 078-00116-0000 SPRING COMPRESSION EA . S401 031-00443-0002 SW ROTARY AJ-7 EA 1. . . 1. . .00 025-00018-0099 WIRE 26 WHT IN . .00 R402 131-00334-0013 RES CF 330K EW 5% EA . .00 . .00 073-00505-0002 BRACKET EA . 1. 1.00 V401 134-05005-0000 PHOTODETECTOR EA .00 . 1.00 CR406 007-06016-0000 DIO S 1N4154 EA . 1. 1. 1. . 6-52 . Apr/2007 ©Honeywell International Inc.KFS 576A Rev 0. Do not print without express permission of Honeywell. 6-53 .KFS 576A THE FOLLOWING IS THE PARTS LIST FROM THE PREVIOUS REVISION AND IS PROVIDED FOR REFERENCE ONLY. Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. Rev 0. 6-54 .KFS 576A Rev 0. Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. KFS 576A Figure 6-11 Switch Board (Dwg No 300-06589-0000 Rev AC) Rev 0. Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. 6-55 . Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.KFS 576A Rev 0. 6-56 . Do not print without express permission of Honeywell.KFS 576A Figure 6-12 Switch Board (Dwg No 300-06589-0000 Rev 5) (For Reference Only) Rev 0. Apr/2007 ©Honeywell International Inc. 6-57 . 6-58 .KFS 576A Rev 0. Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 6-59 . Apr/2007 ©Honeywell International Inc.KFS 576A Figure 6-13 Switch Board Schematic (Dwg No 002-06589-0000 Rev 1) Rev 0. KFS 576A Rev 0. 6-60 . Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 00 C305 097-00103-0020 CAP AL 1. Do not print without express permission of Honeywell.00 C307 096-01006-0000 CAP TN 1.00 C310 096-01082-0009 CAP TN 15UF 20V EA 1.00 R310 131-00240-0013 RES CF 24 EW 5% EA 1.00 R320 131-00204-0013 RES CF 200K EW 5% EA 1.00 R316 131-00204-0013 RES CF 200K EW 5% EA 1.00 I306 120-03053-0000 IC LM358N EA 1.00 Q301 007-00383-0001 XSTR S NPN 2N2222A EA 1.00 CR302 007-06016-0000 DIO S 1N4154 EA 1.00 R314 131-00683-0013 RES CF 68K EW 5% EA 1.00 J304 030-02424-0002 HDR RTANG DBL 16P EA 1.00 I304 120-06045-0001 IC SCL4022ABC+ EA 1.00 I303 120-03138-0000 IC DI 240A EA 1.00 R309 131-00823-0013 RES CF 82K EW 5% EA 1.00 R324 131-00154-0013 RES CF 150K EW 5% EA 1.00 C308 111-02103-0041 CAP MC 10KPF50V10% EA 1.00 R306 999-09999-0098 PLACE HOLDER RF .00 C306 111-00001-0063 CAP CR .00 (TO-18 PACKAGE) R301 131-00103-0013 RES CF 10K EW 5% EA 1.00 CR305 007-06059-0000 DIO S FDH400 EA 1.00 I307 120-03025-0004 IC LM209H EA 1.00 Q306 007-00383-0001 XSTR S NPN 2N2222A EA 1.00 Q305 007-00409-0003 XSTR S MM5416 EA 1.00 C303 113-05331-0000 CAP DC 330PF 500V EA 1.00 R313 131-00753-0013 RES CF 75K EW 5% EA 1.0UF 350V EA 1.00 C309 999-09999-0098 PLACE HOLDER RF .00 R303 131-00105-0013 RES CF 1M EW 5% EA 1.1K EW 5% EA 1.00 Rev 0.00 C304 111-02104-0041 CAP MC 100KPF50V10 EA 1.00 R307 999-09999-0098 PLACE HOLDER RF . Apr/2007 ©Honeywell International Inc.00 R319 131-00683-0013 RES CF 68K EW 5% EA 1.00 R315 131-00333-0013 RES CF 33K EW 5% EA 1.022UF 200V EA 1.00 C311 096-01009-0000 CAP TN 22UF 15V EA 1.00 R312 131-00104-0013 RES CF 100K EW 5% EA 1.3K EW 5% EA 1.00 R318 131-00432-0013 RES CF 4.00 R308 131-00912-0013 RES CF 9.00 P301 030-01117-0000 RECEPTACLE EA 14.00 I301 120-00163-0000 IC DI8884A EA 1.00 R302 131-00103-0013 RES CF 10K EW 5% EA 1.00 R322 131-00394-0013 RES CF 390K EW 5% EA 1. 6-61 .00 R304 131-00105-0013 RES CF 1M EW 5% EA 1.KFS 576A PN DESCRIPTION REV ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------200-06626-0000 DRIVER BD AA ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------C302 113-05331-0000 CAP DC 330PF 500V EA 1.00 Q304 007-00409-0000 XSTR S 2N3439 EA 1.00 (TO-18 PACKAGE) Q303 007-00409-0003 XSTR S MM5416 EA 1.00 R311 131-00334-0013 RES CF 330K EW 5% EA 1.00 R321 131-00154-0013 RES CF 150K EW 5% EA 1.00 R305 131-00822-0013 RES CF 8.00 (TO-18 PACKAGE) Q302 007-00383-0001 XSTR S NPN 2N2222A EA 1.00 J302 030-02217-0005 HEADER RTANG 8P EA 1.00 R323 131-00202-0013 RES CF 2K EW 5% EA 1.00 I302 120-00161-0000 HIGH VOLT DSPLY DR EA 1.0UF 50V EA 1.00 I305 120-03040-0000 IC SE555CN EA 1.2K EW 5% EA 1.00 CR301 007-06111-0000 DIO S IN4157 EA 1.00 CR304 007-06059-0000 DIO S FDH400 EA 1.00 R317 131-00683-0013 RES CF 68K EW 5% EA 1.00 CR303 007-06111-0000 DIO S IN4157 EA 1. 00 REF1 300-06626-0000 DRIVER BD ASSY RF . Apr/2007 ©Honeywell International Inc.00 REF2 002-06626-0000 SCH DRIVER BOARD KFS 576 RF .00 TP302 008-00096-0001 TERMINAL TEST PNT EA 1.00 091-00025-0000 WSHR XSTR INSUL EA 2. 6-62 .00 R326 131-00512-0013 RES CF 5.00 TP304 008-00096-0001 TERMINAL TEST PNT EA 1.1K EW 5% EA 1.00 R328 131-00105-0013 RES CF 1M EW 5% EA 1.125 EA 1.00 033-00092-0011 IC DIP SCKT 16C EA 1.00 091-00182-0000 CAP SEMICN TO-5 EA 2.00 R329 131-00105-0013 RES CF 1M EW 5% EA 1.00 TP301 008-00096-0001 TERMINAL TEST PNT EA 1.00 192-06626-0000 KFS 576A DRIVER BOARD RF .00 TP303 008-00096-0001 TERMINAL TEST PNT EA 1.KFS 576A ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------SYMBOL PART NUMBER FIND NO DESCRIPTION UM -0000 ------------------------------------------------------------------------------------------------------------------------------------------------------------------------------R325 131-00394-0013 RES CF 390K EW 5% EA 1.00 009-06626-0000 PC BD DRIVER EA 1.00 R327 133-00122-0001 RES VA 2K HW 20% EA 1.00 R331 131-00103-0013 RES CF 10K EW 5% EA 1.00 016-01040-0000 COATING TYPE AR AR .00 U301 015-00055-0001 NTWK RES 1M10%. Do not print without express permission of Honeywell.00 033-00092-0012 IC DIP SCKT 18C EA 3.00 R330 131-00823-0013 RES CF 82K EW 5% EA 1.00 ASSY Rev 0.00 090-00307-0000 HEAT SINK FOR TO-5 EA 1. 6-63 . Rev 0. Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.KFS 576A THE FOLLOWING IS THE PARTS LIST FROM THE PREVIOUS REVISION AND IS PROVIDED FOR REFERENCE ONLY. 6-64 . Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell.KFS 576A Rev 0. KFS 576A Figure 6-14 Driver Board (Dwg No 300-06626-0000 Rev 4) Rev 0. Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc. 6-65 . KFS 576A Rev 0. Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 6-66 . Do not print without express permission of Honeywell. Apr/2007 ©Honeywell International Inc.KFS 576A Figure 6-15 Driver Board (Dwg No 300-06626-0000 Rev 2) (For Reference Only) Rev 0. 6-67 . 6-68 . Apr/2007 ©Honeywell International Inc.KFS 576A Rev 0. Do not print without express permission of Honeywell. 6-69 .KFS 576A Figure 6-16 Driver Board Schematic (Dwg No 002-06626-0000 Rev 1) Rev 0. Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell. 6-70 . Apr/2007 ©Honeywell International Inc.KFS 576A Rev 0. Do not print without express permission of Honeywell. THE END . BACK .
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