89000004-200
KA 310 STC Installation Manual
Rev 0
Page 2-6
© Honeywell International Inc. Do not copy without express permission of Honeywell.
2
GENERAL 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.
REF:
RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS
UP793797
