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BENDIXKing KA 310 Installation Manual

Autopilot adapter
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RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS
Honeywell International, Inc.
9201-B San Mateo Blvd N.E.
Albuquerque, New Mexico 87113 U.S.A.
Telephone: 855-250-7027 (Toll Free U.S.A./Canada)
Telephone: 602-365-7027 (International Direct)
KA 310 AUTOPILOT ADAPTER
STC INSTALLATION MANUAL
Document P/N 89000004-200 Rev 0
JULY 2019
Export Control
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.
ECCN: 7E994
© Honeywell International Inc. Do not copy without express permission of Honeywell.
REF:

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  • Page 1 Honeywell International, Inc. 9201-B San Mateo Blvd N.E. Albuquerque, New Mexico 87113 U.S.A. Telephone: 855-250-7027 (Toll Free U.S.A./Canada) Telephone: 602-365-7027 (International Direct) KA 310 AUTOPILOT ADAPTER STC INSTALLATION MANUAL Document P/N 89000004-200 Rev 0 JULY 2019 Export Control 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.
  • Page 2 RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS Blank Page REF:...
  • Page 3 No license to use any Honeywell trademarks or patents is granted under this License Agreement. 89000004-200 KA 310 STC Installation Manual Rev 0 Page T-1 ©...
  • Page 4 Honeywell and may only be modified by a writing duly executed by the duly authorized representatives of the parties. 89000004-200 KA 310 STC Installation Manual Rev 0 Page T-2 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 5 OF THE COMPONENTS. INCORRECTLY FABRICATED SPECIAL TOOLING OR TEST EQUIPMENT CAN RESULT IN DAMAGE TO THE PRODUCT COMPONENTS OR GIVE UNSATISFACTORY RESULTS. 89000004-200 KA 310 STC Installation Manual Rev 0 Page T-3 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 6 Changes to this manual are provided to users who have registered via the website to receive updates. BendixKing Customer Support If you need to speak to personnel about Technical matters, the BendixKing Customer Support team provides 24/7 customer service. ...
  • Page 7 NOTE: The revision level for every page of this document will be updated during the revision process. A list of effective pages is, therefore, not required. Revision Revision Date Description 07/16/2019 Initial release 89000004-200 KA 310 STC Installation Manual Rev 0 Page T-5 © Honeywell International Inc. Do not copy without express permission of Honeywell. REF:...

  • Page 8: Table Of Contents

    3.5.2 KA310 Installation Considerations with BendixKing Flight Control Systems ....3-3 3.5.2.1 Compatible BendixKing Flight Control Systems ............. 3-3 3.5.2.2 KA 310 Installation Considerations in KAP 150/KAP 200/KFC 150/KFC 200 Flight Control System 3-4 3.5.2.3 KA 310 Installation Considerations in KFC 225 Flight Control System ......3-5 3.5.2.4 KA310 Installation Considerations in KAP 100 Flight Control System ......
  • Page 9 Electrical Bonding Considerations ................... 3-8 INSTALLATION PROCEDURES .....................4-1 KA 310 Location and Mounting ....................4-1 4.1.1 KA 310 Installation with KAP 100/KAP 150/KAP 200/KFC 150/KFC 200/KFC 225 .... 4-1 Weight and Balance ......................... 4-1 Cable and Wiring ........................4-2 Wiring, and Power Checks ....................... 4-2 Aircraft Electrical Load Analysis (ELA) ..................
  • Page 10 Figure B - 3 KA 310 Installation Notes ......................B-2 Figure B - 4 KA 310 Installation in KAP 100/KAP 150/KFC 150 Flight Control System ....... B-3 Figure B - 5 KA 310 Installation in KAP 100/KAP 150/KFC 150 Flight Control System ....... B-4 Figure B - 6 KA 310 Installation in KAP 200/KFC 200 Flight Control System ..........
  • Page 11 RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS Table 5-2. KA 310 DB-9 Pin Descriptions ....................5-2 Table 7-1. KAP 100/KAP 150/KAP 200/KFC 150/KFC 200 Flight Control System Maintenance Action ..7-5 Table 8-1. Power-Up Failures Troubleshooting Chart................8-1 Table 8-2.

  • Page 12: Introduction

    (3) The signal names followed by an “*” show an active low signal. (4) The symbols in Figure 1-1 show ESDS and moisture sensitive devices. 89000004-200 KA 310 STC Installation Manual Rev 0 Page 1-1 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 13: Units Of Measure

    Document Number Description IM, KAP 100/KAP 150/KFC 150 Flight Control System for Piper Models PA-46-310P and PA- 006-00287-0000 46-350P 89000004-201 KI 300/KA 310 Pilot's Guide 89800004-098 KA 310 Approved Model List 89000004-210 KI 300 TSO Installation Manual 89000004-101 KI 300 Electronic Attitude Indicator Installation Manual 1.2.2 Other Publications...

  • Page 14: Acronyms And Abbreviations

    American Society for Testing and Materials American Wire Gauge Binary Number Celsius CAGE Commercial and Government Entity Category 89000004-200 KA 310 STC Installation Manual Rev 0 Page 1-3 © Honeywell International Inc. Do not copy without express permission of Honeywell. REF:...
  • Page 15 RTCA Radio Technical Commission for Aeronautics Receive Society of Automotive Engineers International System of Units Serial Number 89000004-200 KA 310 STC Installation Manual Rev 0 Page 1-4 © Honeywell International Inc. Do not copy without express permission of Honeywell. REF:...

  • Page 16: Definition

    Flight Director Indicator KG 258 Attitude Horizon Indicator KRG 331 Yaw Rate Gyro KRG 332 Yaw Rate Gyro 89000004-200 KA 310 STC Installation Manual Rev 0 Page 1-5 © Honeywell International Inc. Do not copy without express permission of Honeywell. REF:...

  • Page 17: General Information

    2.2.1 Part 23 Aircraft Not Identified on the STC Aircraft which are not included on the KA 310 STC and are identified via AC 23.1309-1E Class I - II airplanes may be valid candidates for installation of the KA 310. Data provided in this manual may be used to perform the alteration, but additional FAA approval is required.

  • Page 18: Regulatory Compliance

    Regulatory Compliance This article meets the minimum performance and quality control standards required by the TSO listed in the tables below. The KA 310 can only function as a TSO Incomplete article when installed with a KI 300 (PN 89000004-100-00).

  • Page 19: Pre-Installation Checklist

    Before beginning a KA 310 installation, it is important to ensure the aircraft meets the pre-requisites for the installation of the KA 310 under this STC. The following checklist is provided to help the installer determine the necessary requirements that must be met before beginning installation of the KA 310 in a specific aircraft.

  • Page 20: Installation Limitations

    This section summarizes installation limitations applicable for the KA 310.  The KA 310 is designed to support 14 CFR Part 23 Class I, and II installations. It is not designed to meet installations in 14 CFR Part 27 rotorcraft.

  • Page 21: Environmental Qualification Form (Eqf)

    Note 1 – Testing not required. The enclosure is constructed of metal on all sides and has no vent holes. Note 2 – Section 20 testing completed for CS and RS at a system level with a KI 300 and a KA 310 interconnected, for Level A system. (Cat MD) Note 3 –...

  • Page 22: Stc Permission

    Refer to the troubleshooting instructions in Section 8 - Troubleshooting. If repair is necessary, the unit must be sent to a properly certificated repair facility. The KA 310 is not field repairable. For information on returning the unit, contact BendixKing support.

  • Page 23: Installation Overview

    89400004-102 KA 310 Installation Connector Kit 89400004-114 Note – The table only lists components from the kit that are associated with the KA 310 installation. 3.3.2 Materials Required but Not Supplied The KA 310 is intended for use with standard aviation accessories. The following items are required for...

  • Page 24: Tools Required But Not Supplied

    The KA 310 is not authorized to be installed in flammable fluid zones. There are no clearance requirements for the KA 310. The KA 310 unit may be mounted in any orientation. The KA 310 may be installed in pressurized or unpressurized, temperature controlled locations in fixed wing aircraft with service ceilings not exceeding 35,000 ft.

  • Page 25: Ka310 Installation Considerations With Bendixking Flight Control Systems

    KI300 provides the intended function of KI 255/KI 256/KG 258 and KRG 331/332 in flight control systems. The KA 310 can also provide flight director command bars data to the KI 300 (if flight director functionality is available in the flight control system).

  • Page 26: Ka 310 Installation Considerations In Kap 150/Kap 200/Kfc 150/Kfc 200 Flight Control

    RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS 3.5.2.2 KA 310 Installation Considerations in KAP 150/KAP 200/KFC 150/KFC 200 Flight Control System When installing the KA310 with the KI 300 to provide intended functions of the KI 255/KI 256/KG 258 and KRG 331 (yaw rate gyro) in KAP 150/KAP 200/KFC 150/KFC 200 autopilot system, refer to Figure 3-1 for a system depiction of the wiring that will be required.

  • Page 27: Ka 310 Installation Considerations In Kfc 225 Flight Control System

    RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS 3.5.2.3 KA 310 Installation Considerations in KFC 225 Flight Control System When installing the KA310 with the KI 300 to provide intended functions of the KI 256 and KRG 331/332 (yaw rate gyro) in KFC 225 autopilot system, refer to Figure 3-2 for a system depiction of the wiring that will be required.

  • Page 28: Ka310 Installation Considerations In Kap 100 Flight Control System

    ALERT (OPTIONAL FOR INSTALLATION WITH RADAR ALTIMETER) Figure 3-3 Installation of KA310 in KAP 100 Flight Control System ARINC 429 Interface The KA 310 provides the following ARINC 429 interfaces:  Attitude output  Airdata output  Flight director input The interface speed is a common setting for all interfaces and is set to high (100 kbps).

  • Page 29: Placards And Labels

    Power Distribution The KA 310 can operate on either 14 or 28 VDC. The KA 310 is powered from the aircraft’s avionics bus through a circuit breaker. The KA 310 requires a 2 AMP circuit breaker for both 14 and 28 VDC installations.

  • Page 30: Cable And Wiring Considerations

    RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS Cable and Wiring Considerations KA 310 wiring will be installed in accordance with AC 43.13-1B Chapter 11, (Section 8 – Wiring Installation Inspection Requirements, Section 10 – Service Loop Harnesses, Section 11 – Clamping, Section 15 –...

  • Page 31: Installation Procedures

    KA 310 Location and Mounting The KA 310 does not require forced cooling. The unit must be mounted to a metal surface per the drawing listed in the STC Approved Model List (P/N 89800004-098) to allow proper heat dissipation and electrical bonding of the unit.

  • Page 32: Cable And Wiring

    4.5.1 Aircraft with Existing ELA If the aircraft has an existing ELA, update the ELA to reflect the addition of the KA 310 LRU. The updated ELA must show the alternator(s)/generator(s) have adequate capacity to supply power to the modified systems in all anticipated conditions.

  • Page 33: Aircraft Without Existing Ela

    Verify the electrical load including the KA 310 does not exceed 80% or maximum load published in the AFM/AMM of the rated capacity of the installed generator(s)/alternator(s). If the additional load of the KA 310 exceeds the rated capacity, alternate FAA approval is required for the installation of the KA 310 in the aircraft.

  • Page 34: Connector Pinout Information

    RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS 5 CONNECTOR PINOUT INFORMATION KA 310 Table 5-1. KA 310 DB-44 Pin Descriptions KA310 Pin (J3101) Description Power 1 Input Interlock High Yaw Rate Output Yaw Rate Pseudo Valid + Analog Pitch Angle...

  • Page 35: Table 5-2. Ka 310 Db-9 Pin Descriptions

    RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS Ground Ground Ground Table 5-2. KA 310 DB-9 Pin Descriptions KA 310 Pin (P3102) Description Serial 1 TX Serial 1 RX Reserved Reserved Reserved Reserved Reserved Serial Ground Reserved 89000004-200 KA 310 STC Installation Manual Rev 0 ©...

  • Page 36: System Configuration

    Autopilot Configuration If the KA 310 is connected to an autopilot, the type of autopilot must be configured on the KI 300. In the setup menu, cycle through the setup pages to the “AP Type” setup page. Turn the rotary knob to select the correct autopilot interface: ...

  • Page 37: Application Software Part Number Confirmation

    “Software Part Numbers” setup menu both the KI 300 and KA 310 software numbers are displayed. The first software part number is for KI 300, and the second software part number is for KA 310. Figure 6-3 Software Part Number Display Page Note: This figure is for illustration purposes only.

  • Page 38: System Checkout

    7.1.1 KAP 100/KAP 150/KFC 150/KAP 200/KFC 200/KFC225 Flight Control System Alignment When the KA 310 is installed in the KAP 100/KAP 150/KFC 150/KAP 200/KFC 200/KFC225 Flight Control System, the system alignment procedures (Gyro Alignment Procedure and FD/AP Checks) as described in the appropriate STC Installation Manual and supplemented with the KI 300 alignment instructions, must be performed by the installer.

  • Page 39: Figure 7-2 Ap Alignment Pitch Setup Page

    Figure 7-2 AP Alignment Pitch Setup Page Figure 7-3 AP Alignment Roll Setup Page Figure 7-4 AP Alignment Yaw Rate Setup Page 89000004-200 KA 310 STC Installation Manual Rev 0 © Honeywell International Inc. Do not copy without express permission of Honeywell. REF:...

  • Page 40: Yaw Damper Checkout

    RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS NOTE IF COMMUNICATION BETWEEN THE KI 300 AND KA 310 IS LOST, “AP OUTPUT FAIL” ANNUNCIATION WILL BE DISPLAYED ON THE KI 300. DISCONTINUE AUTOPILOT ALIGNMENT AND DETERMINE CAUSE OF COMMUNICATION FAILURE.

  • Page 41: Figure 7-5 Rudder Deflection Orientation

    “Yes”. Press the rotary knob to exit the setup menus. Figure 7-5 Rudder Deflection Orientation 89000004-200 KA 310 STC Installation Manual Rev 0 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 42: Emc Interaction Checkout

    KA 310. Use the KI 300/KA 310 AP Alignment feature in the setup menu of the KI 300 to manipulate the analog output of the KA 310. Refer to Section 6.1 and Section 7.1.2.

  • Page 43: Troubleshooting

    Return the unit to the manufacturer. (caution) KA 310 Analog Output to Autopilot Failure The KA 310 must be properly configured to output analog signals to the autopilot. If the autopilot is not responding to the KA 310 inputs, verify the following: ...

  • Page 44: Outline And Installation Drawings

    RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS OUTLINE AND INSTALLATION DRAWINGS Figure A - 1 KA 310 Base Unit Figure A - 2 KA 310 Mounting Hole Location 89000004-200 KA 310 STC Installation Manual Rev 0 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 45: Figure A - 3 Ka 310 Center Of Gravity

    RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS TOP VIEW FRONT VIEW Figure A - 3 KA 310 Center of Gravity 89000004-200 KA 310 STC Installation Manual Rev 0 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 46: Interconnect Diagrams

    POWER 1 INPUT POWER 1 RETURN POWER 1 RETURN AIRCRAFT GROUND Figure B - 2 KA 310 – Power and (optional) Radar Altimeter Sheet 2 of 3 89000004-200 KA 310 STC Installation Manual Rev 0 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 47: Figure B - 3 Ka 310 Installation Notes

    REFER TO THE KI 300 INSTALLATION MANUAL (PN 89000004-101) FOR POWER AND GROUND CONNECTIONS. POWER AND GROUND WIRES MAXIMUM LENGTH NOT TO EXCEED 15 FEET. Figure B - 3 KA 310 Installation Notes Sheet 3 of 3 89000004-200 KA 310 STC Installation Manual Rev 0 ©...

  • Page 48: Figure B - 4 Ka 310 Installation In Kap 100/Kap 150/Kfc 150 Flight Control System

    P2962 YAW INTERLOCK HI YAW INTERLOCK HI YAW ANNUNCIATE YAW ANNUNCIATE Figure B - 4 KA 310 Installation in KAP 100/KAP 150/KFC 150 Flight Control System Sheet 1 of 2 89000004-200 KA 310 STC Installation Manual Rev 0 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 49: Figure B - 5 Ka 310 Installation In Kap 100/Kap 150/Kfc 150 Flight Control System

    REPLACEMENT FOR THE KG 257 YAW RATE GYRO. CONNECTION 16, E and C are NO CONNECTION (NC) FOR INSTALLS WITH KAP 100 and KAP 150. Figure B - 5 KA 310 Installation in KAP 100/KAP 150/KFC 150 Flight Control System Sheet 2 of 2 89000004-200...

  • Page 50: Figure B - 6 Ka 310 Installation In Kap 200/Kfc 200 Flight Control System

    YAW RATE OUTPUT REFERENCE YAW RATE OUTPUT REFERENCE YAW RATE IN REFERENCE YAW RATE IN REFERENCE BACKSHELL Figure B - 6 KA 310 Installation in KAP 200/KFC 200 Flight Control System Sheet 1 of 2 89000004-200 KA 310 STC Installation Manual Rev 0 ©...

  • Page 51: Figure B - 7 Ka 310 Installation In Kap 200/Kfc 200 Flight Control System

    LOWER CASE LETTER 10. CONNECTIONS BB, EE, AND p ARE NO CONNECTION (NC) FOR KAP 200. Figure B - 7 KA 310 Installation in KAP 200/KFC 200 Flight Control System Sheet 2 of 2 89000004-200 KA 310 STC Installation Manual Rev 0 ©...

  • Page 52: Figure B - 8 Ka 310 Installation In Kfc 225 Flight Control System

    YAW RATE PSUEDO VALID + YAW RATE PSUEDO VALID + YAW RATE PSEUDO VALID + YAW RATE PSEUDO VALID + Figure B - 8 KA 310 Installation in KFC 225 Flight Control System Sheet 1 of 2 89000004-200 KA 310 STC Installation Manual Rev 0 ©...

  • Page 53: Figure B - 9 Ka 310 Installation In Kfc 225 Flight Control System

    LIMIT SHIELDED WIRE EXPOSURE TO 3 INCHES MAXIMUM. ALL SHIELD GROUNDS MUST BE TERMINATED TO THE AUTOPILOT GROUND STUD WITH MAXIMUM LENGTH NOT TO EXCEED 6 INCHES. Figure B - 9 KA 310 Installation in KFC 225 Flight Control System Sheet 2 of 2 89000004-200...

  • Page 54: Ka 310 Installation Worksheet

    Aircraft Serial Number: Complete Table C-1: Identify the location of the KA 310 and any applicable aircraft access panels. Include all information necessary to gain access to the KA 310 when access plates are not provided. Table C-1: KA 310 LRU Location...

  • Page 55: Figure C - 1 Ka 310 And Cable Routing (Top View

    RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS On Figure C-1: Draw in the location of the KA 310 and the wiring routing. Figure C - 1 KA 310 and Cable Routing (Top View) 89000004-200 KA 310 STC Installation Manual Rev 0 ©...

  • Page 56: Figure C - 2 Ka 310 And Cable Routing (Side View

    RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS On Figure C-2: Draw in the location of the KA 310 and the wiring routing. Figure C - 2 KA 310 and Cable Routing (Side View) On Figure C-3: Draw in the KA 310 Circuit Breaker location on the cockpit depiction.

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