89000004-200
KA 310 STC Installation Manual
Rev 0
4-3
© Honeywell International Inc. Do not copy without express permission of Honeywell.
4.5.2
Aircraft without Existing ELA
An electrical load analysis must be completed to show the capacity of the alternator(s)/generator(s) is
sufficient for the additional electrical load from the KA 310. Refer to ASTM F2490-05: Standard Guide for
Aircraft Electrical Load and Power Source Capacity Analysis for guidance on preparing and ELA for the
aircraft. Verify the electrical load including the KA 310 does not exceed 80% or maximum load published
in the AFM/AMM of the rated capacity of the installed generator(s)/alternator(s). If the additional load
of the KA 310 exceeds the rated capacity, alternate FAA approval is required for the installation of the KA
310 in the aircraft.
4.6
Aircraft Flight 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 the AFMS (Repair Station #,
Name, Address, Make and Model Airplane, Aircraft Registration # and Serial #).
4.7
KA 310 LRU and Wiring Location Data
The KA 310 Installation Worksheets in APPENDIX C must be completed by the installer. The LRU location
and wire routing information must be detailed enough to enable maintenance personnel to
troubleshoot, repair and service the electrical system. The Installation Worksheet should also include a
method of determining the connector type (if other than the connectors supplied in the KA 310
Installation Kits). The system wiring diagrams are descriptive data of the systems used on the aircraft
and are part of the ICA. Copy the applicable Interconnect diagrams from Appendix B and provide for
insertion in aircraft records.
REF:
RELEASED FOR THE EXCLUSIVE USE BY: HONEYWELL EMPLOYEE AMERICAS
UP793797
