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____________________________________________________________________________

89000004-101

KI 300 Installation Manual

Rev 1

Page T-5

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

N/A

Initial release

4.7.3

KA310-205

–

Updates from Sandia Aerospace.



SAISW-44 - Add Diagnostic Mode (Setup menu)



SAISW-55 - Add Yaw Rate Alignment to setup pages



SAISW-73

–

Setup Page for Panel Type

Содержание KI 300

Страница 1: ...027 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 e...

Страница 2: ...Blank Page...

Страница 3: ...h 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 bet...

Страница 4: ...nt 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 ret...

Страница 5: ...rial Safety Data Sheets OSHA Form 174 or equivalent from the manufacturers or suppliers of the materials to be used The user must know the manufacturer supplier data and obey the procedures recommenda...

Страница 6: ...sonable efforts have been made in the preparation of this document to assure its accuracy Honeywell assumes no liability resulting from any errors or omissions in this document or from the use of the...

Страница 7: ...oneywell RECORD OF REVISIONS Revision Revision Date Description 0 10 26 2017 Initial release 1 6 10 2018 KA310 207 Update to capture changes in the KI 300 setup pages CURRENT REVISION DESCRIPTION Sect...

Страница 8: ...2 7 2 4 Regulatory Compliance 2 8 2 5 Technical Specifications 2 8 2 6 Environmental Qualification form EQF 2 10 2 7 Repair and Return 2 11 3 INSTALLATION CONSIDERATIONS 3 1 3 1 Introduction 3 1 3 2 C...

Страница 9: ...3 5 V Speed Settings 4 11 4 7 3 6 IAS Units 4 12 4 7 3 7 Baro Units 4 12 4 7 3 8 Default Baro Setting 4 12 4 7 3 9 IVSI Damping 4 12 4 7 3 10 Slip Skid Type 4 13 4 7 3 11 Diagnostic Mode 4 13 4 7 3 12...

Страница 10: ...ir Data Display Options 4 11 Figure 4 12 KI 300 Slip Skid Indicator Display Options 4 13 Figure 5 1 Li Poly Battery Pack 5 2 Figure 5 2 Li Poly Battery Connections 5 3 LIST OF TABLES Table 1 1 Acronym...

Страница 11: ...operation or maintenance procedure which if not obeyed can cause damage to the equipment A NOTE gives data not commands The NOTE helps personnel when they do the related instruction 4 Warnings and ca...

Страница 12: ...v fdsys pkg GPOSTYLEMANUAL 2008 content detail html IEEE Std 260 1 Standard Letter Symbols for Units of Measurement available from the American National Standards Institute at http www ansi org ASME Y...

Страница 13: ...d Abbreviations Definition AC Advisory Circular AHRS Attitude and Heading Reference System AMP Ampere ANSI American National Standards Institute AP Autopilot ARS Attitude Reference System ARINC Aerona...

Страница 14: ...Pound m Meter mb millibars Min minute mm Millimeter Mph Miles per hour NA Not Applicable NiMh Nickel Metal Hydride No Number Nm Newton Meter NVM Non Volatile Memory PBA Printed Board Assembly PBIT Po...

Страница 15: ...______________________________________________________________________ 89000004 101 KI 300 Installation Manual Rev 1 Page 1 5 Honeywell International Inc Do not copy without express permission of Hone...

Страница 16: ...ertical speed and slip The instrument is self contained and directly incorporates all of the sensors required to measure and display the listed flight parameters All information is displayed on a colo...

Страница 17: ...SO d functions 2 2 2 System Interfaces Airspeed and altitude are derived from internal pressure sensors that are connected to the aircraft s pitot and static lines Airspeed is determined by the pressu...

Страница 18: ...or TSO C8E Type B Battery RTCA DO 347 Small Lipo 4 81Wh 2 5 Technical Specifications Table 2 2 KI 300 Technical Specifications Characteristic Specification Unit Dimensions 2 25 inches x 3 52 inches x...

Страница 19: ...cal Speed Range 5 000 to 5 000 Feet Min Baro Correction Range 28 00 to 31 00 inHg 948 to 1050 mb Roll Pitch Accuracy 1 Static Conditions Roll Pitch Range Unlimited Slip Range 7 Displayable Slip Accura...

Страница 20: ...8 000 to 35 000 Feet 15 000 Feet 5 0 Temperature Variation C 2 C minute 6 0 Humidity A 7 0 Operational Shocks and Crash Safety B AC Type 5 Random 8 0 Vibration S curve M Zone 2 fixed wing 9 0 Explosiv...

Страница 21: ...n 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...

Страница 22: ...determine that the aircraft installation conditions are within the TSO standards TSO articles must have separate approval for installation in an aircraft The article may be installed only according t...

Страница 23: ...cument for minimum guaranteed operating time under different conditions Reference the KI 300 Pilots Guide PN 89000004 201 for additional details on battery operation 3 2 5 Functional Dependencies The...

Страница 24: ...evel non accelerated flight conditions NOTE APPROXIMATELY NINE PERCENT OF THE POPULATION HAS SOME SORT OF COLOR VISION DEFICIENCY WHAT IS COMMONLY CALLED COLOR BLINDNESS IT SHOULD ALSO BE NOTED THAT T...

Страница 25: ...tion in this mode meets the applicable performance requirements of TSO C201 DO 334 2 2 4 2 Degraded Mode Accuracy 2 2 4 2 1 Degraded Mode Pitch Accuracy 2 2 4 2 2 Degraded Mode Roll Accuracy for basic...

Страница 26: ...S X4 6 32 x 3 8 Nut Nylon Insert Std Zinc X4 6 32 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 i...

Страница 27: ...iate your claim The claim must be filed as soon as possible Confirm receipt of all installation components refer to Table 3 1 Table 3 2 and Table 3 3 for the appropriate part lists Inspect all compone...

Страница 28: ...nstructing connecting the pneumatic lines installing the vibration gasket and mounting the unit to the bracket Power On is then performed followed by unit configuration and finally unit checkout proce...

Страница 29: ...he rear bracket is utilized to fasten the unit to the panel The supplied screws and nuts must be used to retain the brackets 4 3 Mounting Bracket Installation 1 Inspect the mounting bracket to ensure...

Страница 30: ...ain un painted and be bonded to the aircraft frame or equivalent for composite aircraft with a resistance of 2 5 milliohms or less This can be achieved by cleaning and or removing paint from the rear...

Страница 31: ...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 TYPE NOTES 1 Seri...

Страница 32: ...es 3 Connect the Pitot line to the rear of the unit on the fitting labeled P 4 Connect the Static line to the rear of the unit on the fitting labeled S The pitot and static connections are provided by...

Страница 33: ...it connects to the mounting bracket utilizing two upper tabs and a lower fastener 2 Place vibration gasket on unit before installing unit onto bracket 3 The unit is installed by engaging the two upper...

Страница 34: ...r tabs remain fully engaged 8 While holding in ward and down ward pressure on the unit tighten the lower screw with the 3 32 hex drive Torque to 5 inch lbs CAUTION DO NOT OVER TIGHTEN 9 Verify that th...

Страница 35: ...Exit From Setup Mode Setup mode is enabled when the unit is powered on while the rotary knob is being held in the pressed state After verifying basic power on cycle power to the unit and enter the set...

Страница 36: ...50 1kt or mph 4 7 3 4 IAS Trim 400 knots Used to adjust for minor variations in airspeed at 400 knots 50 50 1kt or mph 4 7 3 4 ALT Trim 0 ft Used to adjust for minor variations in altitude at 0 ft 99...

Страница 37: ...0 degrees 1 degree 4 7 3 15 AP Align Roll Used to set the Roll output value for autopilot alignment 60 degrees 60 degrees 1 degree 4 7 3 15 Yaw Rate Alignment This allows installation to manually chec...

Страница 38: ...he 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 4 7 3 4 ADC Calibration...

Страница 39: ...to the next menu item The baro units setting selected is pilot preference and the configuration should be communicated to the operator 4 7 3 8 Default Baro Setting The default baro setting can be sele...

Страница 40: ...or Display Options Select the preferred slip skid indication option by turning the rotary knob and then pressing in the knob to save the value and move on to the next menu item The slip skid indicatio...

Страница 41: ...This option is selected when the KI 300 is connected to the KA 310 and the KA 310 is connected to a BendixKing autopilot that uses digital communication The setting selected is determined by the type...

Страница 42: ...1 KI 300 Installation Manual Rev 1 Page 4 15 Honeywell International Inc Do not copy without express permission of Honeywell 4 7 3 16 Yaw Rate Alignment This allows installation to manually check rudd...

Страница 43: ...n screen battery icon The battery fails to charge during normal operation The battery fails the full duration load test described below The battery pack is over 5 years old as measured by the battery...

Страница 44: ...aker and cancel the power down sequence by pressing the knob 5 Note the current time and allow unit to operate for 2 hours At the end of the 2 hour period if the unit has shut down or on screen parame...

Страница 45: ...tain the battery cover 5 Extract the battery pack 6 Grasp the leads in pairs and gently pull the connectors loose from the unit Do not pull excessively on just one individual wire The connector is a h...

Страница 46: ...eed and Altimeter Test Calibration Both the airspeed and attitude sensors have the ability to be tested and calibrated in the field Greater accuracy will be obtained by allowing the unit to fully stab...

Страница 47: ...IC SYSTEM THAT CANNOT HANDLE AN ALTITUDE INPUT OF 35 000 FT THE KI 300 MUST BE REMOVED FROM THE AIRCRAFT AND THE ALTITUDE TRIM PROCEDURE MUST BE COMPLETED ON THE BENCH 5 4 3 Altitude Trim Procedure 1...

Страница 48: ...installed Perform battery load test Replace battery Return unit for service Battery icon is Red X ed For deeply discharged batteries pre charge as follows 1 Apply power for 10 minutes 2 Momentarily re...

Страница 49: ..._________________________________________________________________________ 89000004 101 KI 300 Installation Manual Rev 1 6 2 Honeywell International Inc Do not copy without express permission of Honeyw...

Страница 50: ...Honeywell International Inc Do not copy without express permission of Honeywell...

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