Introduction; Configuration Procedure; Power On; Aircraft Configuration - Honeywell BENDIX KING KMH 880 System Installation Manual

B
POST INSTALLATION CONFIGURATION AND CHECK OUT
4.0

INTRODUCTION

This Section describes the procedure for configuring and testing the KMH 880/KTA 870
System after it is installed in the aircraft.
4.1 POST CONFIGURATION TEST
This Post-Installation Test verifies the proper operation of the KMH 880/KTA 870 System.
These procedures are used after the units have been initially installed. Thereafter, these
procedures can be used as an operational check. These tests are performed on the
ground.
Many of the test can be performed indoors. The scenario tests should be done in an area
where the local traffic and signal multipaTH are not a factor. The bearing accuracy tests
should be conducted outside away from operating aircraft. 115 VAC, 60 Hz power may be
required for the test equipment.
ADVISE THE LOCAL AIR TRAFFIC CONTROL BEFORE TESTING THE
TRANSPONDERS OR THE KMH 880/KTA 870 SYSTEM WITH A SYNTHETIC
ALTITUDE TO ACKNOWLEDGE POSSIBLE INTERACTION WITH OTHER
TAS/TCAS-EQUIPPED AIRCRAFT.
4.2

CONFIGURATION PROCEDURE

This section describes the configuration options available to be programmed into the
Configuration Module of the KMH 880/KTA 870 System.

4.2.1 Power On

Turn the KMH 880/KTA 870 System on.

4.2.2 Aircraft Configuration

Aircraft Configuration strapping is stored in the configuration module via a
personal computer executing TASDIAG software across theRS-232 port. Follow
instructions for configuration programming in the TASDIAG Diagnostic, Appen-
dix D of this manual.
Rev 0, October/2000
SECTION IV
CAUTION:
10609I00.ZIPCDL
KMH 880/KTA 870
Page 4-1