BENDIXKing KA 310 User manual

© Honeywell International Inc. Do not copy without express permission of Honeywell.
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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
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ECCN: 7E994
PRODUCTION - Revision Superseded - 17 Jul 2019 18:30:00 UTC
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Safety Advisory
WARNING: BEFORE THE MATERIALS CALLED OUT IN THIS PUBLICATION ARE USED, KNOW THE HANDLING,
STORAGE AND DISPOSAL PRECAUTIONS RECOMMENDED BY THE MANUFACTURER OR SUPPLIER. FAILURE
TO OBEY THE MANUFACTURERS’ OR SUPPLIERS’ RECOMMENDATIONS CAN RESULT IN PERSONAL INJURY
OR DISEASE.
This publication describes physical and chemical processes which can make it necessary to use chemicals,
solvents, paints, and other commercially available materials. The user of this publication must get the
Material Safety Data Sheets (OSHA Form 174 or equivalent) from the manufacturers or suppliers of the
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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
Revision Date
Description
0
07/16/2019
Initial release
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TABLE OF CONTENTS
1INTRODUCTION ........................................................................................................................1-1
1.1 How to Use This Manual..........................................................................................................1-1
1.1.1 General..............................................................................................................................1-1
1.1.2 Observance of Manual Instructions..................................................................................1-1
1.1.3 Symbols.............................................................................................................................1-1
1.1.4 Units of Measure ..............................................................................................................1-2
1.1.5 Electrostatic Discharge .....................................................................................................1-2
1.2 References ...............................................................................................................................1-2
1.2.1 Honeywell/Vendor Publications .......................................................................................1-2
1.2.2 Other Publications ............................................................................................................1-2
1.3 Acronyms and Abbreviations...................................................................................................1-3
1.4 Definition .................................................................................................................................1-5
2GENERAL INFORMATION...........................................................................................................2-6
2.1 Introduction .............................................................................................................................2-6
2.2 Scope........................................................................................................................................2-6
2.2.1 Part 23 Aircraft Not Identified on the STC ........................................................................2-6
2.3 KA 310 Overview......................................................................................................................2-6
2.4 Regulatory Compliance............................................................................................................2-7
2.5 KA 310 Installation Overview...................................................................................................2-7
2.6 Pre-Installation Checklist .........................................................................................................2-8
2.7 Technical Specifications...........................................................................................................2-8
2.8 Installation Limitations ............................................................................................................2-9
2.9 Environmental Qualification form (EQF) ...............................................................................2-10
2.10 STC Permission.......................................................................................................................2-11
2.11 Repair and Return..................................................................................................................2-11
3INSTALLATION OVERVIEW.........................................................................................................3-1
3.1 Introduction .............................................................................................................................3-1
3.2 Available Equipment................................................................................................................3-1
3.3 Installation Materials ...............................................................................................................3-1
3.3.1 Accessories Available from BendixKing ............................................................................3-1
3.3.2 Materials Required but Not Supplied ...............................................................................3-1
3.3.3 Tools Required but Not Supplied......................................................................................3-2
3.4 Unpacking and Inspection........................................................................................................3-2
3.5 Installation Considerations ......................................................................................................3-2
3.5.1 KA 310 Installation Considerations...................................................................................3-2
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 ...........................3-6
3.6 ARINC 429 Interface.................................................................................................................3-6
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3.7 Placards and Labels..................................................................................................................3-7
3.8 Power Distribution...................................................................................................................3-7
3.8.1 Circuit Protection..............................................................................................................3-7
3.9 Cable and Wiring Considerations.............................................................................................3-8
3.9.1 Shield Termination............................................................................................................3-8
3.10 Electrical Bonding Considerations ...........................................................................................3-8
4INSTALLATION PROCEDURES .....................................................................................................4-1
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
4.2 Weight and Balance .................................................................................................................4-1
4.3 Cable and Wiring......................................................................................................................4-2
4.4 Wiring, and Power Checks .......................................................................................................4-2
4.5 Aircraft Electrical Load Analysis (ELA)......................................................................................4-2
4.5.1 Aircraft with Existing ELA..................................................................................................4-2
4.5.2 Aircraft without Existing ELA ............................................................................................4-3
4.6 Aircraft Flight Manual Supplement (AFMS).............................................................................4-3
4.7 KA 310 LRU and Wiring Location Data.....................................................................................4-3
5CONNECTOR PINOUT INFORMATION.........................................................................................5-1
5.1 KA 310......................................................................................................................................5-1
6SYSTEM CONFIGURATION .........................................................................................................6-1
6.1 KI 300 Setup Mode Entry .........................................................................................................6-1
6.2 Autopilot Configuration ...........................................................................................................6-1
6.3 Application Software Part Number Confirmation ...................................................................6-2
7SYSTEM CHECKOUT...................................................................................................................7-3
7.1 Flight Control System Alignment .............................................................................................7-3
7.1.1 KAP 100/KAP 150/KFC 150/KAP 200/KFC 200/KFC225 Flight Control System Alignment7-3
7.1.2 KI 300/KA 310 AP Alignment Feature ...............................................................................7-3
7.2 Yaw Damper Checkout.............................................................................................................7-5
7.3 EMC Interaction Checkout.......................................................................................................7-7
7.4 Post Installation Flight Checks .................................................................................................7-7
7.4.1 KAP 100/KAP 150/KFC 150/KAP 200/KFC 200/KFC225 Flight Control System Flight Checks
7-7
8TROUBLESHOOTING..................................................................................................................8-1
8.1 Built-in-Test Function...............................................................................................................8-1
8.2 Power-Up Failures....................................................................................................................8-1
8.3 In-Flight Failures.......................................................................................................................8-1
8.4 KA 310 Analog Output to Autopilot Failure .............................................................................8-1
OUTLINE AND INSTALLATION DRAWINGS................................................................. A-1
INTERCONNECT DIAGRAMS...................................................................................... B-1
KA 310 INSTALLATION WORKSHEET.......................................................................... C-1
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LIST OF FIGURES
Figure 1-1 Symbols....................................................................................................................................1-2
Figure 3-1 Installation of KA310 in KAP 150/KAP 200/KFC 150/KFC 200 Flight Control System .............3-4
Figure 3-2 Installation of KA310 in KFC 225 Flight Control System ..........................................................3-5
Figure 3-3 Installation of KA310 in KAP 100 Flight Control System...........................................................3-6
Figure 3-4 Termination Procedure.............................................................................................................3-8
Figure 6-1 Setup Mode Menu ....................................................................................................................6-1
Figure 6-2 Autopilot Type Setup Page .......................................................................................................6-2
Figure 6-3 Software Part Number Display Page.........................................................................................6-2
Figure 7-1 Autopilot Alignment Setup Page...............................................................................................7-3
Figure 7-2 AP Alignment Pitch Setup Page ................................................................................................7-4
Figure 7-3 AP Alignment Roll Setup Page ..................................................................................................7-4
Figure 7-4 AP Alignment Yaw Rate Setup Page .........................................................................................7-4
Figure 7-5 Rudder Deflection Orientation .................................................................................................7-6
Figure A - 1 KA 310 Base Unit.................................................................................................................... A-1
Figure A - 2 KA 310 Mounting Hole Location............................................................................................ A-1
Figure A - 3 KA 310 Center of Gravity ....................................................................................................... A-2
Figure B - 1 KA 310 Installation –KI 300 Interconnect...............................................................................B-1
Figure B - 2 KA 310 –Power and (optional) Radar Altimeter ....................................................................B-1
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..............................................B-5
Figure B - 7 KA 310 Installation in KAP 200/KFC 200 Flight Control System..............................................B-6
Figure B - 8 KA 310 Installation in KFC 225 Flight Control System............................................................B-7
Figure B - 9 KA 310 Installation in KFC 225 Flight Control System.............................................................B-8
Figure C - 1 KA 310 and Cable Routing (Top View) ....................................................................................C-2
Figure C - 2 KA 310 and Cable Routing (Side View)....................................................................................C-3
Figure C - 3 KA 310 Circuit Breaker Location .............................................................................................C-3
LIST OF TABLES
Table 1-1: Acronyms and Abbreviations....................................................................................................1-3
Table 2-1: KA 310 TSO Authorization.........................................................................................................2-7
Table 2-2: Pre-Installation Checklist ..........................................................................................................2-8
Table 2-3: KA 310 Specification..................................................................................................................2-8
Table 2-4: KA 310 Environmental Qualification Form (EQF)....................................................................2-10
Table 3-1: KA 310 Part Numbers................................................................................................................3-1
Table 3-2: KA 310 Installation Kit 89000004-104.......................................................................................3-1
Table 3-3: Materials Required but Not Supplied .......................................................................................3-1
Table 3-4: Tools Required but Not Supplied..............................................................................................3-2
Table 3-5 List of Compatible Flight Control Systems .................................................................................3-3
Table 4-1: KA 310 LRU Weight ...................................................................................................................4-2
Table 5-1. KA 310 DB-44 Pin Descriptions .................................................................................................5-1
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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. In-Flight Failures Troubleshooting Chart ..................................................................................8-1
Table C-1: KA 310 LRU Location.................................................................................................................C-1
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1INTRODUCTION
1.1 How to Use This Manual
1.1.1 General
(1) This publication gives installation and maintenance instructions for the equipment shown on the
Title page.
(2) Standard maintenance procedures that technicians must know are not given in this manual.
(3) Warnings, cautions, and notes in this manual give the data that follows:
A WARNING gives a condition or tells personnel what part of an operation or
maintenance procedure, which if not obeyed, can cause injury or death.
A CAUTION gives a condition or tells personnel what part of an 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 cautions go before the applicable paragraph or step. Notes follow the applicable
paragraph or step.
1.1.2 Observance of Manual Instructions
(1) Make sure that you carefully obey all safety, quality, operation, and shop procedures for the
unit.
(2) All personnel who operate equipment and do maintenance specified in this manual must know
and obey the safety precautions.
1.1.3 Symbols
(1) The symbols and special characters agree with IEEE Publication 260 and IEC Publication 27.
Special characters in text are spelled out.
(2) The signal mnemonics, unit control designators, and test designators are shown in capital
letters.
(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.
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Figure 1-1 Symbols
1.1.4 Units of Measure
Measurements, weights, temperatures, dimensions, and other values are expressed in the USMS
followed by the appropriate SI metric units in parentheses. Some standard tools or parts such as drills,
taps, bolts, nuts, etc. do not have an equivalent.
1.1.5 Electrostatic Discharge
Touch the items susceptible to electrostatic discharge in accordance with MIL-HDBK-263. Refer to MIL-
STD-1686 for definition of the standards and conditions.
1.2 References
1.2.1 Honeywell/Vendor Publications
Related Honeywell 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-
46-350P
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
These publications are standard references. Check for latest version of publication.
Document Number
Description
The United States GPO Style Manual (available at
http://www.gpo.gov/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)
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Document Number
Description
ASME Y14.38
Abbreviations for Use on Drawings and Related Documents (available from the American
National Standards Institute at http://www.ansi.org)
ASME Y14.5
Dimensioning and Tolerancing (available from the American National Standards Institute
at http://www.ansi.org)
ANSI/IEEE Std 91
Graphic Symbols for Logic Functions (available from the American National Standards
Institute at http://www.ansi.org)
H4/H8 CAGE Codes (available from DLA Logistics Information Services at
http://www.logisticsinformationservice.dla.mil)
IEEE 315/ANSI Y32.2
Graphic Symbols for Electrical and Electronics Diagrams (available from the American
National Standards Institute at http://www.ansi.org)
MIL-HDBK-263
Electrostatic Discharge Control Handbook for Protection of Electrical and Electronic Parts,
Assemblies and Equipment (Excluding Electrically Initiated Explosive Devices) (Metric)
(available from any military standards database)
MIL-STD-1686
Electrostatic Discharge Control Program for Protection of Electrical and Electronic Parts,
Assemblies and Equipment (Excluding Electrically Initiated Explosive Devices) (Metric)
(available from any military standards database).
1.3 Acronyms and Abbreviations
(1) The abbreviations are used in agreement with ASME Y14.38.
(2) Acronyms and non-standard abbreviations used in this publication are as follows in Table 1-1.
Table 1-1: Acronyms and Abbreviations
Acronyms and
Abbreviations
Definition
AC
Advisory Circular
ADPT
Adapter
AFCS
Automatic Flight Control System
AFMS
Aircraft Flight Manual Supplement
AMP
Ampere
ANSI
American National Standards Institute
AP
Autopilot
ARINC
Aeronautical Radio, Incorporated
AS
Aerospace Standard
ASME
American Society of Mechanical Engineers
ASTM
American Society for Testing and Materials
AWG
American Wire Gauge
BNR
Binary Number
C
Celsius
CAGE
Commercial and Government Entity
Cat
Category
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Acronyms and
Abbreviations
Definition
CBIT
Continuous Built-in Test
CFR
Code of Federal Regulations
COM
Communication
CS
Conducted Susceptibility
DC
Direct Current
ECCN
Export Control Classification Number
ELA
Electrical Load Analysis
EQF
Environmental Qualification Form
EMI
Electromagnetic Interference
ESD
Electrostatic Discharge
ESDS
Electrostatic Discharge Sensitive
F
Fahrenheit
FAA
Federal Aviation Administration
FAR
Federal Aviation Regulation
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
Institute of Electrical and Electronics Engineers
IM
Installation Manual
IMM
Installation and Maintenance Manual
in-lb
inch-pound
kbps
kilobytes per second
kg
Kilogram
kPa
kilopascal
lb
Pound
LRU
Line Replaceable Unit
m
Meter
mm
Millimeter
NA
Not Applicable
Nm
Newton Meter
PBIT
Power-up Built-in Test
PN
Part Number
RAM
Random Access Memory
RS
Radiated Susceptibility
RTCA
Radio Technical Commission for Aeronautics
RX
Receive
SAE
Society of Automotive Engineers
SI
International System of Units
SN
Serial Number
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Acronyms and
Abbreviations
Definition
STC
Supplemental Type Certificate
TR
Temporary Revision
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
Description
KI 255
Flight Director Indicator
KI 256
Flight Director Indicator
KG 258
Attitude Horizon Indicator
KRG 331
Yaw Rate Gyro
KRG 332
Yaw Rate Gyro
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89000004-200 KA 310 STC Installation Manual
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2GENERAL INFORMATION
2.1 Introduction
This manual describes the physical, mechanical, and electrical characteristics, as well as installation
instructions, conditions and limitations for the installation and approval of the BendixKing KA 310
Autopilot Adapter (PN 89000004-110-00[ ]). The information in this document is subject to change
without notice. Visit the BendixKing web site (www.bendixking.com) for current updates and
supplemental information concerning the operation of this and other BendixKing products.
2.2 Scope
This installation manual applies to the modification of an aircraft to support the installation of the
BendixKing KA 310 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 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.
2.3 KA 310 Overview
The KA 310 Autopilot Adapter (P/N 89000004-110-00[ ]) is intended for installation with a specific
BendixKing electronic attitude indicator, the KI 300 (PN 89000004-100-00). The KA 310 converts the
serial attitude data (pitch, roll, and yaw) from the KI 300 to analog outputs for an autopilot interface.
The KA 310 includes the input capability for flight director engage, flight director commands, and
decision height data. The flight director commands and decision height data is then provided to the KI
300 for display to the pilot.
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2.4 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).
Table 2-1: KA 310 TSO Authorization
Function
TSO/SAE/RTCA
Category
Automatic flight guidance and
control systems
TSO-C198 (Incomplete)
DO-325
Class A1, C
2.5 KA 310 Installation Overview
Always follow acceptable avionics installation practices per AC 43.13-1B, AC 43.13-2B, or later FAA
approved revisions of these documents. Follow the installation procedures in Section 4, as it is
presented, to accomplish a successful installation. Read the entire section before beginning the work.
Prior to installation, consider the structural integrity of the KA 310 as defined in Section 3.4. Complete
an electrical load analysis in accordance with the instructions in Section 4.5 on the aircraft prior to
starting the modification to ensure the aircraft electrical system has 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 problems occur.
When working with avionics equipment, be aware of the following warnings and cautions.
CAUTION
SERVICE TECHNICIANS MUST OBEY STANDARD SAFETY PRECAUTIONS, SUCH AS WEARING SAFETY
GLASSES, TO PREVENT PERSONAL INJURY WHILE INSTALLING OR PERFORMING SERVICE ON THIS
UNIT.
CAUTION
TURN OFF POWER BEFORE DISCONNECTING WIRING. DISCONNECTING WIRING WITHOUT
TURNING POWER OFF MAY CAUSE VOLTAGE TRANSIENTS THAT CAN DAMAGE THE SYSTEM.
CAUTION
THIS EQUIPMENT INCLUDES ITEMS THAT ARE ELECTROSTATIC DISCHARGE SENSITIVE (ESDS)
DEVICES. ESDS DEVICES ARE SUBJECT TO DAMAGE BY EXCESSIVE LEVELS OF VOLTAGE AND/OR
CURRENT. THE LOW-ENERGY SOURCE THAT MOST COMMONLY DESTROYS ESDS DEVICES IS THE
HUMAN BODY, WHICH, IN CONJUNCTION WITH NONCONDUCTIVE GARMENTS AND FLOOR
COVERINGS, GENERATES AND RETAINS STATIC ELECTRICITY. TO ADEQUATELY PROTECT ESDS
DEVICES, THE DEVICE AND EVERYTHING THAT CONTACTS IT MUST BE BROUGHT TO GROUND
POTENTIAL BY PROVIDING A CONDUCTIVE SURFACE AND DISCHARGE PATHS. USE STANDARD
INDUSTRY PRECAUTIONS TO KEEP RISK OF DAMAGE TO A MINIMUM WHEN TOUCHING,
REMOVING, OR SERVICING THE EQUIPMENT.
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2.6 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. Ensure each of the items outlined are completed as necessary before beginning the
modification.
Table 2-2: Pre-Installation Checklist
Item
Reference
Complete
KI 300 installed as the primary flight display
KI 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
Section 4.5

Aircraft weight and balance with KA 310 is
within aircraft limits.
Section 4.2

Acceptable mounting provision have been
identified.
Section 3.5.1

2.7 Technical Specifications
Table 2-3: KA 310 Specification
Characteristic
Specification
Dimensions
5.81 inches x 5.25 inches x 1.25 inches (L x W x H)
(148 mm x 133 mm x 32 mm)
Mounting Information
Vertically or horizontally with four screws
Weight
1.07 lbs. (0.48 kg)
Current Draw
Typical (28VDC): 0.145 A, Max (28VDC): 0.200 A
Typical (14VDC): 0.245 A, Max (14VDC): 0.380 A
Operating Voltage
+9.0 to 32.2 VDC
Circuit Breaker
2.0 Amps
Software
RTCA/DO-178C Level C
Hardware
NA
Connectors
DB-44, DB-9
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Characteristic
Specification
Certification
TSO-C198 (Incomplete) Class A1, C
2.8 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.
The KA 310 is not approved to support installations in composite structure airplanes.
This article meets the minimum performance and quality control standards required by a
technical standard order (TSO). Installation of this article requires separate approval.
The KA 310 was shown to meet the applicable performance standards only when installed with
the compatible equipment and systems provided in Section 3.5.
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