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BENDIXKing KI 300 Installation Manual

Electronic attitude indicator
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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)
KI 300 ELECTRONIC ATTITUDE INDICATOR
INSTALLATION MANUAL
Document P/N 89000004-101 Rev 1
June 2018
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.

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  • Page 1 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) KI 300 ELECTRONIC ATTITUDE INDICATOR INSTALLATION MANUAL Document P/N 89000004-101 Rev 1 June 2018 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 Blank Page...
  • Page 3 No license to use any Honeywell trademarks or patents is granted under this License Agreement. 89000004-101 KI 300 Installation Manual Rev 1 Page T-1 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 4 Honeywell and may only be modified by a writing duly executed by the duly authorized representatives of the parties. 89000004-101 KI 300 Installation Manual Rev 1 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. 89000004-101 KI 300 Installation Manual Rev 1 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 ____________________________________________________________________________ RECORD OF REVISIONS Revision Revision Date Description 10/26/2017 Initial release 6/10/2018 KA310-207 – Update to capture changes in the KI 300 setup pages CURRENT REVISION DESCRIPTION Section Description Initial release KA310-205 – Updates from Sandia Aerospace.  SAISW-44 - Add Diagnostic Mode (Setup menu) 4.7.3...

  • Page 8: Table Of Contents

    Pneumatic Source ........................3-4 Cooling Considerations ......................3-4 Available Equipment ........................ 3-5 Installation Materials ....................... 3-5 3.6.1 Accessories Available from BendixKing ................3-5 3.6.2 Materials Required But Not Supplied ................3-5 3.6.3 Tools Required But Not Supplied ..................3-6 Unpacking and Inspection......................3-6 Handling Considerations ......................
  • Page 9 5.4.1 Altimeter System Test and Inspection ................5-4 5.4.2 Airspeed Trim Procedure ....................5-4 5.4.3 Altitude Trim Procedure ....................5-5 TROUBLESHOOTING ........................6-1 89000004-101 KI 300 Installation Manual Rev 1 Page TC-2 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 10 Table 3-2: KI 300 Accessories and Installation Kits ..................3-5 Table 3-3: KI 300 Installation Kit (PN 89000004-103) ................3-5 Table 3-4: KI 300 Front Mounting Kit (PN 89500004-100) ................ 3-5 Table 3-5: Installation Materials Required But Not Supplied ..............3-5 Table 3-6: Tools Required But Not Supplied ....................

  • Page 11: 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. 89000004-101 KI 300 Installation Manual Rev 1 Page 1-1 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 12: Units Of Measure

    Electrostatic Discharge Control Handbook for Protection of Electrical and Electronic Parts, MIL-HDBK-263 Assemblies and Equipment (Excluding Electrically Initiated Explosive Devices) (Metric) (available from any military standards database) 89000004-101 KI 300 Installation Manual Rev 1 Page 1-2 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 13: Acronyms And Abbreviations

    Federal Aviation Administration Federal Aviation Regulation Flight Control System Flight Director Government Printing Office Input/Output Instructions for Continued Airworthiness 89000004-101 KI 300 Installation Manual Rev 1 Page 1-3 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 14 United States of America Universal Serial Bus USMS United States Measurement System Volt Volts Direct Current Visual Flight Rule 89000004-101 KI 300 Installation Manual Rev 1 Page 1-4 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 15 ____________________________________________________________________________ 89000004-101 KI 300 Installation Manual Rev 1 Page 1-5 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 16: General Information

    Introduction This manual describes the installation of the BendixKing KI 300 Electronic Attitude Indicator. It is intended for use by FAA certified repair stations to install the KI 300 indicator and includes both mechanical and electrical installation information. System configuration, and continued airworthiness are included. The installer must ensure that all functions are operating properly according to their intended purpose in their particular installation.

  • Page 17: System Interfaces

    The KA 310 Autopilot Adapter is an optional remote mounted analog and digital unit. The unit receives attitude data from the KI 300 and converts the serial data into analog or digital outputs to support an interface to BendixKing legacy autopilots. Refer to the KA 310 AML STC Installation Manual PN 89000004-200 for detailed installation information on the KA 310.

  • 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. Table 2-1 KI 300 TSO Authorization Function TSO/SAE/RTCA Category Airspeed TSO-C2d Type B Turn and Slip TSO-C3e Bank and Pitch...

  • Page 19: Table 2-3 Ki 300 Performance Characteristics

    ____________________________________________________________________________ Table 2-3 KI 300 Performance Characteristics Characteristic Specification Time to Initialize < 3 Minutes Typical Airspeed Range 30 to 400 Knots (30 to 460 Mph) Altitude Range -1500 to 35,000 Feet Vertical Speed Range -5,000 to 5,000 Feet/Min 28.00 to 31.00 inHg...

  • Page 20: Environmental Qualification Form (Eqf)

    ____________________________________________________________________________ Environmental Qualification form (EQF) Table 2-4: KI 300 Environmental Qualification Form (EQF) DO-160G Condition Category Notes Section Temperature A1/C1 Ground Survival Low -55°C Short Term Low -40°C Operating Low -20°C Ground Survival High +85°C Short Term High +70°C Operating High +55°C...

  • Page 21: Repair And Return

    Refer to the troubleshooting instructions in Section 6 - Troubleshooting. If repair is necessary, the unit must be sent to a BendixKing repair facility. There are no field repairable items inside the KI 300. For information on returning the unit, contact BendixKing support.

  • Page 22: Installation Considerations

    If installation is being performed on an aircraft with a retro-fit EFIS/PFD installation, the FAA approved installation guidance for that product must be considered when installing the KI 300 as a backup to those installations. Compatibility with the primary EFIS/PFD must be evaluated and considerations may include: ...

  • Page 23: Substitution Of Rate-Of-Turn Indicator

    The KI 300 may be eligible to replace the Rate-Of-Turn Indicator in certain applications. Refer to FAA AC 91-75 for additional details. 3.2.4 Battery Operation The battery sub-system in the KI 300 is designed to fulfill the needs of an independent power source per 14 CFR 23.1353(h). Considerations are as follows: ...

  • Page 24: Tso Deviations

    TSO-C2d § a(3), §a(3)(i), § c(1)(xi), §c(2)(vii)  TSO-C3e § 3(e), § 6(h)  TSO-C113a § 3(e), § 6(g) 89000004-101 KI 300 Installation Manual Rev 1 Page 3-3 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 25: Degraded Mode Operations

    The above deviations have been FAA approved. 3.2.8 Degraded Mode Operations Errors will not exceed TSO limit specifications. When a cross check message is present, the KI 300 is considered to be in degraded mode. The TSO tested maneuvers represent typical flight. Degraded mode may occur if a pilot maintains an accelerated frame of reference (i.e.

  • Page 26: Available Equipment

    Hex Wrench, 3/32” L-WR Short 3.6.2 Materials Required But Not Supplied The KI 300 is intended for use with standard aviation accessories. The following items are required for installation but not supplied: Table 3-5: Installation Materials Required But Not Supplied...

  • Page 27: Tools Required But Not Supplied

    Turret) Unpacking and Inspection Exercise extreme caution when unpacking the equipment. Do a visual inspection of the KI 300 unit for evidence of damage incurred during shipment. If a damage claim must be filed, save the shipping container and all packing materials to substantiate your claim. The claim must be filed as soon as possible.

  • Page 28: Installation Procedures

    Figure 4-1 Unit Front and Rear Views Mounting Hole The KI 300 is designed to mount in a standard 3” round mounting hole. The supplied front mounting bracket and rear mounting bracket (Kit PN 89500004-100) must be utilized to mount the instrument.

  • Page 29: Mounting Bracket Installation

    4. Minor roll error can be corrected by slightly rotating the bracket prior to tightening and during the configuration of the unit. 89000004-101 KI 300 Installation Manual Rev 1 Page 4-2 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 30: Wiring Installation

    3. Keep power and ground lines less than 1 meter in length. The KI 300 is supplied with one 9 pin Sub-D female mating connector and back-shell. The Sub-D connector uses screw lock assemblies to secure the connector to the unit.

  • Page 31: Figure 4-4 Sub-D Back-Shell

    All electrical connections are made on the single rear mounted 9 pin Sub-D. Connections indicated as Reserved - Do Not Connect (DNC) should not be connected in the installation. Power and ground are applied to pins 5 and 9 respectively. Table 4-1: KI 300 Electrical Pin Out PIN # FUNCTION...

  • Page 32: Pneumatic Line Installation

    When selecting alternate fittings, do not allow the threads to penetrate more than 0.3 inches into the unit, otherwise sensor damage will occur. Do not remove the foam filter located in the body of the unit. 89000004-101 KI 300 Installation Manual Rev 1 Page 4-5...

  • Page 33: Unit Mounting

    4. Hold the unit at a slight angle off of the instrument panel (as shown below) and align the upper tabs with the slots on the rear of the unit. Motion 1: Motion 2: Motion 3: 89000004-101 KI 300 Installation Manual Rev 1 Page 4-6 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 34: System Configuration

    System Configuration The following section provides instructions for initial setup configuration of the KI 300. For complete operation guide, including normal and abnormal operation, see the Pilot Guide (PN 89000004-201).

  • Page 35: Entry & Exit From Setup Mode

    IAS speed markings, etc), will all be updated real-time with user adjustment. This can be useful for trimming certain parameters such as airspeed and altitude trim. 89000004-101 KI 300 Installation Manual Rev 1 Page 4-8 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 36: Setup

    Each pages’ value is internally stored when the corresponding page is exited, not upon exit of the last page. 4.7.3 Setup Pages A total of 29 setup pages are available as follows: Table 4-2: KI 300 Setup Parameters Reference Setup Page Purpose...

  • Page 37: Pitch Trim And Roll Trim

    After the aircraft is level, enter the appropriate pitch and roll trim values in the setup menu by turning the rotary knob to the value that levels the ownship symbol on the KI 300 display and then pressing in the knob to move to the next menu item.

  • Page 38: Adc Calibration

    ____________________________________________________________________________ Figure 4-11 KI 300 Air Data Display Options Select the preferred display option by turning the rotary knob and then pressing in the knob to save the value and move to the next menu item. The air data display setting selected is pilot preference, and the configuration should be communicated to the operator.

  • Page 39: Ias Units

    Select the preferred IVSI damping option by turning the rotary knob and then pressing in the knob to save the value and move on to the next menu item. 89000004-101 KI 300 Installation Manual Rev 1 Page 4-12 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 40: Slip/Skid Type

    Starvation Timer expiring (progress bar)  Bias Tracking indication (one for each axis) 4.7.3.12 Autopilot Type When the KI 300 is connected to the KA 310 the type of autopilot must be configured. There are four options: 89000004-101 KI 300 Installation Manual...

  • Page 41: Software Part Numbers

    ____________________________________________________________________________  None – This option is selected when the KI 300 is not connected to the KA 310 or when the KI 300 is connected to the KA 310 and the KA 310 is not connected to an autopilot.

  • Page 42: Yaw Rate Alignment

    This allows installation to manually check rudder movement. Refer to the KA 310 AML STC Installation Manual PN 89000004-200 for details. 89000004-101 KI 300 Installation Manual Rev 1 Page 4-15 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 43: Instructions For Continued Airworthiness

    The altimeter function must be tested and inspected in accordance with 14 CFR 91.411. Battery Maintenance The KI 300 contains a field-replaceable Li-Poly battery pack. This battery requires periodic replacement to ensure sufficient capacity is available to meet performance specifications.

  • Page 44: Battery Replacement Procedure

    CONNECTORS ARE UTILIZED FOR EACH. FOLLOW THE INDICATED COLOR CODING. DAMAGE TO THE UNIT MAY OCCUR. Heater Leads (Red/Red) Battery Polarization Leads Keys (Red/Black) Figure 5-1 Li-Poly Battery Pack 89000004-101 KI 300 Installation Manual Rev 1 © Honeywell International Inc. Do not copy without express permission of Honeywell.

  • Page 45: Figure 5-2 Li-Poly Battery Connections

    Figure 5-2 Li-Poly Battery Connections 1. Only the approved batteries are to be used. See specification section of this document for the applicable BendixKing part number(s). 2. Ensure power is not supplied to the unit by either pulling the applicable circuit breaker, or turning off the master switch.

  • Page 46: Airspeed And Altimeter Test & Calibration

    1. Connect the pitot-static test set to the aircraft static system. The KI 300 must be connected to the aircraft static system. 2. Apply power to the KI 300 while holding the pushbutton down in order to enter setup mode and allow the internal encoder to stabilize.

  • Page 47: Altitude Trim Procedure

    5. Configure the pitot-static test set to obtain an airspeed reading of 30 kts. 6. On the KI 300, adjust the trim setting until the airspeed tape reads 30 kts, then press the knob to proceed to the “IAS Trim @ 400 kts” page.

  • Page 48: Troubleshooting

    ____________________________________________________________________________ 6 TROUBLESHOOTING The following information can be utilized to recognize and correct probable malfunctions. Table 6-1: KI 300 Troubleshooting Symptom Possible Solutions  Ensure proper supply power is available. Attitude remains Red-X’ed  Return unit for service.  Ensure proper supply power is available.
  • Page 49 ____________________________________________________________________________ 89000004-101 KI 300 Installation Manual Rev 1 © Honeywell International Inc. Do not copy without express permission of Honeywell.
  • Page 50 © Honeywell International Inc. Do not copy without express permission of Honeywell.

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