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Honeywell BENDIX/KING KCS55 Installation Manual

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RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION
INSTALLATION MANUAL
KCS 55/55A
PICTORIAL NAVIGATION
SYSTEM
MANUAL NUMBER 006-00111-0011
REVISION 11 April 2007

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  Summary of Contents for Honeywell BENDIX/KING KCS55

  • Page 1 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION INSTALLATION MANUAL KCS 55/55A PICTORIAL NAVIGATION SYSTEM MANUAL NUMBER 006-00111-0011 REVISION 11 April 2007...
  • Page 2 ©1997-2002, 2007 Honeywell International Inc. Reproduction of this publication or any portion thereof by any means without the express written permission of Honeywell is prohibited. For further information contact the manager, Technical Publications, Honeywell, One Technology Center, 23500 West 105th Street Olathe KS 66061...
  • Page 3 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.
  • Page 4 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.
  • Page 5 REVISION HIGHLIGHTS KCS 55/55A Part Number Date Description 006-00111-0008 Jun/2001 006-00111-0009 Jan/2002 006-00111-0010 Feb/2002 006-00111-0011 Apr/2007 Updated to remove NVG versions of the unit Rev. 11, Apr/2007 Page RH-1 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 6 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION KCS 55/55A REVISION HIGHLIGHTS Part Number Date Description Rev. 11, Apr/2007 Page RH-2 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 7: Table Of Contents

    INSTRUCTIONS FOR CONTINUED AIRWORTHINESS 1-13 SECTION II INSTALLATION PARAGRAPH PAGE UNPACKING AND INSPECTING EQUIPMENT PREINSTALLATION CHECK KI 525/525A INDICATOR INSTALLATION 2.3.1 GENERAL 2.3.2 MOUNTING Rev 11, Apr/2007 Page i ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 8 AVAILABILITY OF 400 HZ. POWER FROM THE KG 102/102A SECTION III OPERATION PARAGRAPH PAGE DISPLAY DESCRIPTION 3.1.1 KI 525/525A INDICATOR AND CONTROLS OPERATING PROCEDURES EMERGENCY OPERATION Page ii Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 9 KG 102/102A 400 Hz. SUPPLY INTERCONNECT DIAGRAM 2-57 KI 525/525A INDICATOR AND CONTROLS KA 51/51A SLAVING ACCESSORY AND CONTROLS KA 51B SLAVING ACCESSORY AND CONTROLS Rev 11, Apr/2007 Page iii ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 10 KCS 55/55A LIST OF TABLES TABLE PAGE KI 525A VERSION CHART KI 525 VERSION CHART KA 51A VERSION CHART KA 51B VERSION CHART 1-10 Page iv Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 11: General Information

    "slave in" button on the KA 51A (toggle switch- es on the KA 51B), the "fast slave" will automatically be repeated. Rev 11, Apr/2007 Page 1-1 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 12: Technical Characteristics

    Hx = 0.18 gauss Hz = 0.54 gauss. WARM-UP TIME: Varies from 1 min. at +55 C to 5 min. at -46 1.3.2 KI 525/525A Page 1-2 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 13: Ki 525/525A

    400Hz. Electrically equivalent to Clifton TSH- 11-F-08. (066-3046-02/03/06/07/11/12 indicators only) Drive signal for the heading loop drive motor from the KG 102/102A. 1.3.2 KI 525/525A (cont). Rev 11, Apr/2007 Page 1-3 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 14: Kg 102/102A

    Slaving meter drive signal for the KA 51/51A/51B. (KG 102A Only) Pin a supplies a ground when compass system is valid. 1.3.4 KMT 112 Page 1-4 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 15: Ka 51/51A

    North/South and East/West correction to the KI 525/525A. Clockwise and counterclockwise manual slave signals to the KG 102/102A Slaved/free gyro mode logic signal to the KG 102/102A 1.3.6 KA 51B Rev 11, Apr/2007 Page 1-5 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 16 Course datum AC output transformer isolated and phase locked to the reference input from the autopilot. 1.3.8 KA 57 Page 1-6 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 17: Units And Accessories Supplied

    All part numbers are capable of operating at 30Hz. However, 066-03046-02/03/06/07/11/12 are capable of operating at either 30Hz or 400Hz. Serial number 43434 and above have glideslope damping for helicopters in all versions. Rev 11, Apr/2007 Page 1-7 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 18: Kg 102/102A Directional Gyro

    The KMT 112 (PN 071-1052-00) senses the direction of the earth’s magnetic field and transmits this information to the KI 525/525A. 1.4.4 KA 51/51A/51B SLAVING ACCESSORY Page 1-8 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 19 BLACK 5 V RED 071-1053-07 GRAY 5 V RED 071-1053-08 GRAY 14 V 071-1053-09 BLACK 28 V RED Table 1-3 KA 51/51A Version Chart Rev 11, Apr/2007 Page 1-9 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 20: Ka 52 Autopilot Adapter

    DC heading and course datum signals from the KI 525/525A Indicator into a single, swit- chable AC output signal compatible with certain autopilot systems. INSTALLATION KITS See figure 1-1 for crimping, insertion, and extraction tools. Page 1-10 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 21 Shock Mount Hole Temp 071-04025-0001 Assy Vibration Mount 089-05909-0009 Scr. #8-32 X 9/16 PHP 155-02001-0000 GND Strap The shock mount assembly (P/N 071-04025-0001) contains the following: Rev 11, Apr/2007 Page 1-11 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 22 Scr. PHP #4-40 x 7/16 KA 57 Installation Kit (050-01421-0000) includes the following: Description Qty. 030-00107-0016 Conn, 20 Pin 088-00438-0000 Conn, Hood 089-05903-0006 Scr. PHP #4-40 x 3/8 Page 1-12 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 23: Compensator Kit (Optional)

    The instructions for continued airworthiness given in the TC or STC approvals for this product sup- plements or supersedes the instructions for continued airworthiness in this manual. Most Honeywell products are designed and manufactured to allow "on condition maintenance." On condition maintenance is described as follows; There are no periodic service requirements necessary to maintain continued airworthiness.
  • Page 24 HONEYWELL P/N 005-02012-0015 POSITRONICS P/N 9099 EXTRACTION TOOL (NOT PICTURED) HONEYWELL P/N 005-02012-0012 POSITRONICS P/N 9081 FIGURE 1-1 KCS 55/55A CRIMPING, INSERTION, AND EXTRACTION TOOLS Page 1-14 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 25: Installation

    DC POSITION ON THE KG 102/102A. NOTE: FOR THE CENTURY 21/31/41 AUTOPILOT INTER- FACES, AN IC 930 ADAPTER IS AVAILABLE FROM CENTURY FLIGHT SYSTEMS. CONTACT AT TEL: (817) 325-2517. Rev 11, Apr/2007 Page 2-1 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 26: Ki 525/525A Indicator Installation

    2-2 with four #6-32 screws that are provided with the unit. Using the connectors provided connect the system wiring and the navigation and lighting wiring per Figures 2-10, 2-11, 2-12 and 2-13. Page 2-2 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 27: Kg 102/102A Gyro Installation

    Figure 2-1 with two #4-40 screws provided in the installation kit. Using the connector provided, connect the wiring to the unit as shown in Figure 2-2. Rev 11, Apr/2007 Page 2-3 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 28: Adapter Installation

    With the complete KCS 55/55A system operating and the KA 51/51A in the "free gyro" mode; po- sition the aircraft on a compass rose and adjust the compensator as follows: Page 2-4 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 29: Ka 51B

    All readings should be within of those on the compass rose. The KA 51B can now be re- secured to the aircraft panel. The alignment is complete. Rev 11, Apr/2007 Page 2-5 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 30: Alternate Method Of Compensation Adjustments For Kmt 112 And Ka 51/Ka 51A

    Place a non-magnetic blade screwdriver in the N/ S potentiometer on the KA 51/KA 51A and adjust the exter- nal millivolt meter for 1/2 of the existing meter readout. Page 2-6 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 31: Ka 52 And Ka 57

    0 position). Turn on the autopilot and slew the Heading Select Marker to -10 (Marker 10 counterclock- wise from the lubber line). Rev 11, Apr/2007 Page 2-7 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 32 Radio Coupler with an ILS frequency on the ra- dio, the KA 57 Course Datum output will be 180 de- grees out of phase. Page 2-8 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 33 NAV1/NAV2 autopilot transfer), will be connected to the KG 102/102A 26 VAC out- put (P1021, pins p and t). Some Honeywell Flight Control Systems incorporate a KRG 331 Rate Gyro. These units are typically shown powered off of the KG 102A. The KG 102A will not simul- taneously supply a KRG 331 and a KI 229 or KNI 582.
  • Page 34 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 2-1 PIN LOCATIONS (Viewed From REAR of Mating Connectors Except Where Noted) Page 2-10 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 35 BENDIX/KING KCS 55/55A FIGURE 2-2 KI 525/525A INSTALLATION DRAWING (Dwg. No. 155-05117-0000, R-AA) Page 2-11 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 36 BENDIX/KING KCS 55/55A Page 2-12 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 37 BENDIX/KING KCS 55/55A FIGURE 2-3 KG 102/102A INSTALLATION DRAWING (Dwg. No. 155-05118-0000, R-AA) Page 2-13 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 38 BENDIX/KING KCS 55/55A Page 2-14 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 39 BENDIX/KING KCS 55/55A FIGURE 2-4 KMT 112 INSTALLATION DRAWING (Dwg. No. 155-05130-0000, R-1) Page 2-15 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 40 BENDIX/KING KCS 55/55A Page 2-16 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 41 BENDIX/KING KCS 55/55A FIGURE 2-5 KA 51 INSTALLATION DRAWING (Dwg. No. 155-05144-0000, R-1) Page 2-17 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 42 BENDIX/KING KCS 55/55A Page 2-18 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 43 BENDIX/KING KCS 55/55A FIGURE 2-6 KA 51A INSTALLATION DRAWING (Dwg. No. 155-05144-0001, R-3) Page 2-19 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 44 BENDIX/KING KCS 55/55A Page 2-20 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 45 BENDIX/KING KCS 55/55A FIGURE 2-7 KA 51B INSTALLATION DRAWING (Dwg. No. 155-05371-0000, R-4) Page 2-21 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 46 BENDIX/KING KCS 55/55A Page 2-22 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 47 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 2-8 KA 52 INSTALLATION DRAWING (Dwg. No. 155-05143-0000, R-2) Rev 11, Apr/2007 Page 2-23 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 48 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 2-9 KA 57 INSTALLATION DRAWING (Dwg. No. 155-05165-0000, R-1) Page 2-24 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 49 BENDIX/KING KCS 55/55A FIGURE 2-10 KCS 55 SILVER CROWN COMPASS SYSTEM INTERCONNECT DIAGRAM (Dwg. No. 155-01147-0000, R-8) Page 2-25 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 50 BENDIX/KING KCS 55/55A Page 2-26 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 51 BENDIX/KING KCS 55/55A FIGURE 2-11 KCS 55A SILVER CROWN COMPASS SYSTEM (30Hz OBS RESOLVER) INTERCONNECT DIAGRAM (Dwg. No. 155-01147-0001, R-AB) Page 2-27 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 52 BENDIX/KING KCS 55/55A Page 2-28 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 53 BENDIX/KING KCS 55/55A FIGURE 2-12 KCS 55A SILVER CROWN COMPASS SYSTEM (400HZ OBS RESOLVER) INTERCONNECT DIAGRAM (Dwg. No. 155-01147-0002, R-AB) Page 2-29 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 54 BENDIX/KING KCS 55/55A Page 2-30 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 55 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 2-13 KX 175/KN 73/KN 77/KI 525/525A INTERCONNECT DIAGRAM (Dwg. No. 155-01148-0000, R-3) Rev 11, Apr/2007 Page 2-31 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 56 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A THIS PAGE IS RESERVED Page 2-32 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 57 BENDIX/KING KCS 55/55A FIGURE 2-14 COMPLETE SILVER CROWN SYSTEM INTERCONNECT DIAGRAM (Dwg. No. 155-01149-0000, R-0, Sheet 1 of 2) Page 2-33 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 58 BENDIX/KING KCS 55/55A Page 2-34 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 59 BENDIX/KING KCS 55/55A FIGURE 2-14 COMPLETE SILVER CROWN SYSTEM INTERCONNECT DIAGRAM (Dwg. No. 155-01149-0000, R-0, Sheet 2 of 2) Page 2-35 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 60 BENDIX/KING KCS 55/55A Page 2-36 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 61 BENDIX/KING KCS 55/55A FIGURE 2-15 KN 72/KN 75/KI 525A INTERCONNECT DIAGRAM (Dwg. No. 155-01340-0000, R-1) Page 2-37 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 62 BENDIX/KING KCS 55/55A Page 2-38 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 63 BENDIX/KING KCS 55/55A FIGURE 2-16 KNS 80 - KI 525A INTERCONNECT DIAGRAM (Dwg. No. 155-01316-0000, R-7) Page 2-39 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 64 BENDIX/KING KCS 55/55A Page 2-40 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 65 HONEYWELL SUGGESTS THAT NO ATTEMPT BE MADE TO INTERFACE THE KCS 55/55A SYS- TEM WITH THE ALTIMATIC II OR ANY OTHER "RF SENSING DESIGN" AUTOPILOT SYSTEM. Rev 11, Apr/2007 Page 2-41 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 66 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 2-17 KCS 55/55A/BENDIX FCS-810 AUTOPILOT INTERFACE INTERCONNECT Page 2-42 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 67 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 2-18 KCS 55/55A/CESSNA 300 NAVOMATIC INTERFACE INTERCONNECT (Dwg. No. 155-01190-0000, R-2) Rev 11, Apr/2007 Page 2-43 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 68 LECT/NAV COURSE DATUM SWITCHING OPERATION WITH THE EXTERNAL SWITCH, THE INTERCONNECT MUST BE WIRED IN ACCORDANCE TO THIS NOTE. FIGURE 2-19 KCS 55A/KA 57 CESSNA 300A/CA395A INTERCONNECT Page 2-44 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 69 KCS 55/55A FIGURE 2-20 KCS 55/55A CESSNA NAVOMATIC 400 INTERFACE INTERCONNECT (Dwg. No. 155-01182-0000, R-3) NOTE: THIS INTERCONNECT IS FOR 400A AUTOPILOT WITH FLIGHT DIRECTOR. Rev 11, Apr/2007 Page 2-45 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 70 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 2-21 KCS 55/55A CESSNA NAVOMATIC 400A AUTOPILOT INTERFACE INTER- CONNECT (Dwg. Nos. 155-01180-0000, R-2; 155-01193-0000, R-1) Page 2-46 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 71 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 2-22 KCS 55/55A/CESSNA 400B AUTOPILOT INTERFACE INTERCONNECT (Dwg. No. 155-01254-0000, R-3) Rev 11, Apr/2007 Page 2-47 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 72 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 2-23 KCS 55/55A MITCHELL COUPLER IC-388, 388C, 388M, 388MC INTERFACE INTERCONNECT (Dwg. No. 155-01181-0000, R-6) Page 2-48 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 73 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 2-24 KCS 55/55A MITCHELL III AUTOPILOT w/IC 388-3 COUPLER INTERFACE INTERCONNECT (Dwg. No. 155-01192-0000, R-0) Rev 11, Apr/2007 Page 2-49 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 74 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 2-25 KCS 55/55A MITCHELL CENTURY IV AUTOPILOT INTERFACE INTERCONNECT (Dwg. No. 155-01191-0000, R-1) Page 2-50 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 75 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 2-26 KCS 55/55A - AP106/AP107/913K-1 COMPUTER AMPLIFIER AUTOPILOT INTERFACE INTERCONNECT (Dwg. No. 155-01255-0000, R-0) Rev 11, Apr/2007 Page 2-51 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 76 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A THIS PAGE IS RESERVED Page 2-52 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 77 BENDIX/KING KCS 55/55A FIGURE 2-27 KLN 90B - KI 525A INTERCONNECT DIAGRAM (Dwg. No. 155-06021-0000, R-AB, Sheet 1 of 2) Page 2-53 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 78 BENDIX/KING KCS 55/55A Page 2-54 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 79 BENDIX/KING KCS 55/55A FIGURE 2-27 KLN 90B - KI 525A INTERCONNECT DIAGRAM (Dwg. No. 155-06021-0000, R-AB, Sheet 2 of 2) Page 2-55 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 80 BENDIX/KING KCS 55/55A Page 2-56 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 81 The 2.7K resistor provides a pull up for the compass valid to the KNI 582. Pin D pulls the compass valid low in an invalid condition. FIGURE 2-28 KG 102/102A 400 Hz. Supply Interconnection Diagrams Rev 11, Apr/2007 Page 2-57 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 82 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A THIS PAGE IS RESERVED Page 2-58 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 83 360 de- Heading Drive Pushbutton: grees per minute. Rev 11, Apr/2007 Page 3-1 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 84 The deviation bar position relative to the symbolic aircraft then represents the position of the backcourse with respect to the aircraft. Page 3-2 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 85 If possible switch to another glideslope receiver. The localizer and heading displays will continue to function normally. Rev 11, Apr/2007 Page 3-3 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 86 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 3-1 KI 525/525A INDICATOR AND CONTROLS Page 3-4 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 87 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 3-2 KA 51/51A SLAVING ACCESSORY AND CONTROLS Rev 11, Apr/2007 Page 3-5 ©Honeywell International Inc. Do not print without express permission of Honeywell...
  • Page 88 RELEASED FOR THE EXCLUSIVE USE BY: AIRCRAFT ELECTRONICS ASSOCIATION BENDIX/KING KCS 55/55A FIGURE 3-3 KA 51B SLAVING ACCESSORY AND CONTROLS Page 3-6 Rev 11, Apr/2007 ©Honeywell International Inc. Do not print without express permission of Honeywell...

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