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89000004-200

KA 310 STC Installation Manual

Rev 0

Page 3-6

3.5.2.4

KA310 Installation Considerations in KAP 100 Flight Control System

When installing the KA310 with the KI 300 to provide intended functions of the KG258 in KAP 100
autopilot system, refer to Figure 3-3 for a system depiction of the wiring that will be required.

Refer to Figure B-4 for Interconnect diagram.

AIRPLANE POWER

PRIMARY BUS

(28V OR 14V)

DECISION HEIGHT

ALERT

(OPTIONAL FOR

INSTALLATION WITH

RADAR ALTIMETER)

KC 190

(KAP 100 SYSTEM)

2 AMP

ELECTRONIC

ATTITUDE

INDICATOR

KA 310

Figure 3-3 Installation 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 speed is a common setting for all interfaces and is set to high (100 kbps).

The following ARINC 429 labels are required for the flight director input:



Octal Label 140 - Flight Director - Roll (BNR label)



Octal Label 141 - Flight Director - Pitch (BNR label)

The following ARINC 429 labels contain the attitude data output:



Octal Label 203 – Baro-uncorrected Altitude (BNR label)



Octal Label 204 – Baro-corrected Altitude (BNR label)



Octal Label 206 – Indicated Airspeed (BNR label)



Octal Label 212 – Altitude Rate (BNR label)



Octal Label 324 – Pitch Angle (BNR label)



Octal Label 325 – Roll Angle (BNR label)

REF:

RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS

UP793797

Содержание KA 310

Страница 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...

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

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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...

Страница 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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