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Av. Kit Install. Manual
190-00004-00 Rev. G
Page 21
APPENDIX A INSTALLATION DETAILS FOR BEECH B60
1.0 INTRODUCTION:
This appendix provides airframe specific information which is necessary to install the
GARMIN GPS 100 navigation system in the Beech Duke Model B60 in accordance with
STC (tbd). When so installed, the GPS 100 system is approved for use as a
supplementary navigation system under Visual Flight Rules (VFR) only. A functional
block diagram of the system is shown in Figure A-1.
The information provided herein is to be considered supplemental to the information
contained in the GARMIN GPS 100 Aviation Kit Installation Manual, P/N 190-00004-
00. Within this appendix, the base document will be referred to as the "Installation
Manual".
2.0 INSTALLATION INSTRUCTIONS
2.1 ANTENNA
The GPS 100 antenna is to be installed on top of the cabin on the aircraft centerline
at fuselage station 138.0. Figure A-2 illustrates the proper antenna positioning. Refer
to section 2.1 of the Installation Manual for general antenna mounting requirements.
2.2 AVIATION RACK INSTALLATION
The GPS 100 aviation rack is to be installed on the right side of the instrument panel
radio rack as shown in figure A-3. The controls and display of the GPS 100 must be
readily visible to the pilot when seated at the controls.
To install the aviation rack, position it in the instrument panel in the desired position,
assuring that the front is not twisted out of square. Match drill the flanges on the radio
rack to the installation holes on the GPS 100 aviation rack. Using 4 each #6-32 screws
and self locking nuts, attach the aviation rack to the aircraft panel. For additional
information, refer to the Installation Manual.
2.3 WIRING
Fabricate an appropriate cable to connect the GPS 100 aviation rack to 28VDC power,
a message annunciator, a remote switch (for selecting between GPS and standard
navigation equipment), a transfer switch with integral white, illuminated annuncia-
tors with black markings (to control and indicate the status of the remote switch).
Wiring connections are to be made in accordance with Figure A-4. Breaker locations
are to be as shown in Figure A-5. Route and connect the wiring in accordance with
Advisory Circular AC-43.13-2A. After the wiring installation is complete, carefully
check the operation of all flight controls throughout their range to assure that no
operational interference exists.