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RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS

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Summary of Contents for KA 310

Page 1: ...R 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 softwa...

Page 2: ...Blank Page REF RELEASED FOR THE EXCLUSIVE USE BY HONEYWELL EMPLOYEE AMERICAS UP793797...

Page 3: ...ms 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 acknowledge...

Page 4: ...d 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...

Page 5: ...or suppliers of the materials to be used The user must know the manufacturer supplier data and obey the procedures recommendations warnings and cautions set forth for the safe use handling storage an...

Page 6: ...re its accuracy Honeywell assumes no liability resulting from any errors or omissions in this document or from the use of the information contained herein Honeywell Aerospace Online Technical Publicat...

Page 7: ...of Honeywell RECORD OF REVISIONS 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 Revis...

Page 8: ...Limitations 2 9 2 9 Environmental Qualification form EQF 2 10 2 10 STC Permission 2 11 2 11 Repair and Return 2 11 3 INSTALLATION OVERVIEW 3 1 3 1 Introduction 3 1 3 2 Available Equipment 3 1 3 3 Ins...

Page 9: ...10 LRU and Wiring Location Data 4 3 5 CONNECTOR PINOUT INFORMATION 5 1 5 1 KA 310 5 1 6 SYSTEM CONFIGURATION 6 1 6 1 KI 300 Setup Mode Entry 6 1 6 2 Autopilot Configuration 6 1 6 3 Application Softwar...

Page 10: ...0 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...

Page 11: ...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 In Fli...

Page 12: ...mage to the equipment A NOTE gives data not commands The NOTE helps personnel when they do the related instruction 4 Warnings and cautions go before the applicable paragraph or step Notes follow the a...

Page 13: ...ywell publications in this manual are shown in the list that follows Document Number Description 006 00287 0000 IM KAP 100 KAP 150 KFC 150 Flight Control System for Piper Models PA 46 310P and PA 46 3...

Page 14: ...s Assemblies and Equipment Excluding Electrically Initiated Explosive Devices Metric available from any military standards database MIL STD 1686 Electrostatic Discharge Control Program for Protection...

Page 15: ...ation FD Flight Director GND Ground GPO Government Printing Office I O Input Output ICA Instructions for Continued Airworthiness ID Identification IEC International Electrotechnical Commission IEEE In...

Page 16: ...evision TSO Technical Standard Order TX Transmit U S A United States of America USMS United States Measurement System V Volt VDC Volts Direct Current VFR Visual Flight Rule 1 4 Definition Terms Descri...

Page 17: ...10 under a Supplemental Type Certificate 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 ma...

Page 18: ...the ability to source the additional KA 310 electrical load Once the installation is complete perform the post installation checkout described in Section 7 before closing the work area in case proble...

Page 19: ...300 TSO IM PN 89000004 101 Installation operational limitations reviewed to ensure no adverse impact to the installation Section 2 8 and Section 3 5 Aircraft electrical system is sufficient for KA 310...

Page 20: ...and II installations It is not designed to meet installations in 14 CFR Part 27 rotorcraft The KA 310 is not approved to support installations in composite structure airplanes This article meets the m...

Page 21: ...0 Audio Frequency Conducted Susceptibility B 19 0 Induced Signal Susceptibility ZCX 20 0 Radio Frequency Susceptibility Radiated and Conducted RR See Note 2 21 0 Emission or Radio Frequency Energy M 2...

Page 22: ...yaerospace com 2 11 Repair and Return 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...

Page 23: ...ociated 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 installation but n...

Page 24: ...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 Confirm receipt o...

Page 25: ...KI 300 if flight director functionality is available in the flight control system The KA 310 is compatible with the flight control systems listed in Table 3 5 Table 3 5 List of Compatible Flight Cont...

Page 26: ...KFC 150 KFC 200 autopilot system refer to Figure 3 1 for a system depiction of the wiring that will be required Refer to Figure B 4 and Figure B 6 for Interconnect diagrams AIRPLANE POWER PRIMARY BUS...

Page 27: ...56 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 Refer to Figure B 8 for Interconnect diagram AIRPLANE POWER...

Page 28: ...llation of KA310 in KAP 100 Flight Control System 3 6 ARINC 429 Interface The KA 310 provides the following ARINC 429 interfaces Attitude output Airdata output Flight director input The interface spee...

Page 29: ...the following requirements The font size of the new placard shall be the same size as the original placard The color of the new placard shall be the same as the color of the original placard The text...

Page 30: ...of grounding the shield UNIT BACKSHELL 3 00 Figure 3 4 Termination Procedure 3 10 Electrical Bonding Considerations The KA 310 must be electrically bonded to the airframe This is accomplished by ensur...

Page 31: ...ENDIX B 4 Remove existing wiring connected to the autopilot on the pins that are to be interfaced to the KA 310 5 Wire the connections between the KA 310 and the autopilot refer to APPENDIX B 6 Wire t...

Page 32: ...ower bus and the KA 310 Point to point continuity must be checked on all wiring to identify any faults such as shorting to ground Any faults or discrepancies must be corrected before proceeding Upon c...

Page 33: ...ght Manual Supplement AFMS The BendixKing KA 310 Autopilot Adapter Aircraft Flight Manual Supplement AFMS shall be filled out and provided to the aircraft owner Complete the information on page iii of...

Page 34: ...Out 12 Reserved 13 ARINC429 FD In A In 14 SPARE 15 SPARE 16 Power 1 Return 17 Interlock Low Out 18 Yaw Rate Pseudo Valid Out 19 Vertical Gyro Excitation Out 20 Analog Roll Angle Out 21 DH 14V In 22 R...

Page 35: ...ission of Honeywell 42 Ground 43 Ground 44 Ground Table 5 2 KA 310 DB 9 Pin Descriptions KA 310 Pin P3102 Description I O 1 Serial 1 TX Out 2 Serial 1 RX In 3 Reserved 4 Reserved 5 Reserved 6 Reserved...

Page 36: ...page is exited 6 2 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 T...

Page 37: ...ique part number that identifies the software version On the 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...

Page 38: ...C Installation Manual and supplemented with the KI 300 alignment instructions must be performed by the installer Refer to the KA310 Autopilot Adapter Approved Model List for the approved aircraft inst...

Page 39: ...ernational Inc Do not copy without express permission of Honeywell 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 REF RELE...

Page 40: ...when using the AP Align Roll the Pitch outputs is always zero Tilt the attitude gyro to 10 nose up Turn the rotary knob until 10 is displayed in the AP Align Pitch setup menu page Tilt the attitude gy...

Page 41: ...ection is determined by standing behind the aircraft facing towards the nose of the aircraft Refer to Figure 7 5 9 Turn the rotary knob on the KI 300 counter clockwise to a 0 deg sec yaw rate setting...

Page 42: ...aircraft systems 4 Exit setup mode in KI 300 5 If the autopilot includes the Flight Director Command Bar functionality push the FD button to display the flight director bars Turn other aircraft system...

Page 43: ...nit to the manufacturer 8 3 In Flight Failures Refer to Table 8 2 for the in flight failures troubleshooting chart Table 8 2 In Flight Failures Troubleshooting Chart Symptom Possible Cause Solution AP...

Page 44: ...neywell International Inc Do not copy without express permission of Honeywell OUTLINE AND INSTALLATION DRAWINGS Figure A 1 KA 310 Base Unit Figure A 2 KA 310 Mounting Hole Location REF RELEASED FOR TH...

Page 45: ...tion Manual Rev 0 A 2 Honeywell International Inc Do not copy without express permission of Honeywell TOP VIEW FRONT VIEW Figure A 3 KA 310 Center of Gravity REF RELEASED FOR THE EXCLUSIVE USE BY HONE...

Page 46: ...OWER GROUND BACKSHELL WH BL OR WH BL OR 3 4 3 4 6 P3102 P3001 EXISTING Figure B 1 KA 310 Installation KI 300 Interconnect Sheet 1 of 3 KA 310 6 DECISION HEIGHT 28V 6 DECISION HEIGHT 28V 36 DECISION HE...

Page 47: ...ALL BE 22 AWG 2 TERMINATE ALL CONDUCTORS TO CONTACT FOLLOW PIN ASSIGNMENT PRINTED ON CONNECTORS AND LABELS 3 ALL SHIELD GROUNDS MUST BE TERMINATED INSIDE THE BACKSHELL WITH MAXIMUM LENGTH NOT TO EXCEE...

Page 48: ...R ENGAGE 16 FLIGHT DIRECTOR ENGAGE C ROLL COMMAND BAR C ROLL COMMAND BAR A FD COMMAND BAR REFERENCE A FD COMMAND BAR REFERENCE 17 YAW INTERLOCK LOW 17 YAW INTERLOCK LOW 33 YAW RATE OUTPUT REFERENCE 33...

Page 49: ...TORS AND LABELS 3 ALL SHIELD GROUNDS MUST BE TERMINATED INSIDE THE BACKSHELL WITH MAXIMUM LENGTH NOT TO EXCEED 6 INCHES 4 MAXIMUM OF 4 RING TONGUES PER BACKSHELL GROUNDING SCREW IS ALLOWED 5 SPLICE TO...

Page 50: ...MMAND BAR w VERTICAL GYRO EXCITATION w VERTICAL GYRO EXCITATION p FLIGHT DIRECTOR ENGAGE p FLIGHT DIRECTOR ENGAGE EE ROLL COMMAND BAR EE ROLL COMMAND BAR F FD COMMAND BAR REFERENCE F FD COMMAND BAR RE...

Page 51: ...ALL SHIELD GROUNDS MUST BE TERMINATED INSIDE THE BACKSHELL WITH MAXIMUM LENGTH NOT TO EXCEED 6 INCHES 4 MAXIMUM OF 4 RING TONGUES PER BACKSHELL GROUNDING SCREW IS ALLOWED 5 SPLICE TO BE WITHIN THE ASS...

Page 52: ...DIRECTOR ENGAGE 48 FLIGHT DIRECTOR ENGAGE 49 ROLL COMMAND BAR 49 ROLL COMMAND BAR 51 FD COMMAND BAR REFERENCE 51 FD COMMAND BAR REFERENCE 18 YAW RATE PSEUDO VALID 18 YAW RATE PSEUDO VALID 33 YAW RATE...

Page 53: ...TACT FOLLOW PIN ASSIGNMENT PRINTED ON CONNECTORS AND LABELS 3 ALL SHIELD GROUNDS MUST BE TERMINATED INSIDE THE BACKSHELL WITH MAXIMUM LENGTH NOT TO EXCEED 6 INCHES 4 MAXIMUM OF 4 RING TONGUES PER BACK...

Page 54: ...odel 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...

Page 55: ...International Inc Do not copy without express permission of Honeywell 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 REF RELEASED...

Page 56: ...neywell 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 d...

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