EFIS-D100 Installation Guide - Dynon Avionics

More documents

Recommendations

Info

Appendix controller. Rem ember that even when the controller is powered on, it only heats the probe the amount necessary to maintain temperature. The black wire should be permanently connected to ground. Cutting power to the heater controller should occur via the red power line, not the black ground line. Heater Status Connection Note: The probe heater functions properly whether or not you make this connection. It is simply a status output for your convenience. The white heater status wire is grounded when the probe heater is turned off or not functioning properly. This wire should be connected to a light on the pa nel, whose other terminal is connected to switched aircraft power. When the heater is on and functioning properly, the white heater status line is open, leaving the indicator light turned off. When there is no power to the heater controller – or it is not functioning properly – the white line is grounded, turning the indicator light on. Aircraft Spruce P/N 17-410 is an example of a light that will work for this application. An LED and resistor in series will also suffice. If you use an LED as the indicator, you must choose a resistor that delivers the appropriate current to the LED, and can accommodate the power required for its current and voltage drop. If you own a Dynon EMS-based product, you may also use one of its two contact input to display an onscreen indication. Connect this heater status output directly to the desired EMS contact input, with no additional resistors or lights. You must configure the contact display as described in your EMS-based product’s Installation Guide. AOA/PITOT PROBE MOUNTING The Dynon Avionics AOA/Pitot probe has been designed as an under-wing pitot. The following information applies to this type of installation. If you wish to mount your pitot on nose boom mount, contact us so we can make the appropriate adjustments to your pitot. The heated version of Dynon’s AOA/Pitot Probe does not come in a boom-mount configuration. AOA/Pitot Probe Mount Location The Dynon Avionics AOA/Pitot probe only functions correctly when mounted in a location where the airflow over the probe is relatively undisturbe d by the aircraft. In general, we recommend that you mount it at least 6 inches below the wing and with the tip of the probe between 2 and 12 inches behind the leading edge of the wing. Typically, pitot probes are mounted about mid-wing span wise to minimize the effects of both the propeller and the wing tips. Testing during the probe development has shown that the standard mounting locations for the pitot probe in the RV series of aircraft also works for the Dynon probe. AOA/Pitot Probe Mounting Instructions After the mounting location has been determined, mount the pitot mounting kit per the included instructions or fabricate your own mount. In either case, mount the probe securely to the wing such that the body of the probe is horizontal during level flight. Drill and tap mounting holes (#6- 32) on the probe to match your mounting bracket. Use caution when drilling the holes, ensuring that you avoid drilling into the pitot and AOA pressure lines. As long as you do not penetrate 7-28 EFIS-D100 Installation Guide
these lines, you may drill all the way through the outer metal without affecting the probe’s waterproofing. DIMENSIONS Standard mount Appendix EFIS-D100 Installation Guide 7-29
Page 1:
EFIS-D100 Installation Guide This p
Page 5 and 6:
Table of Contents Contact Informati
Page 7 and 8:
1. INTRODUCTION This manual provide
Page 9 and 10:
2. WIRING OVERVIEW Please follow th
Page 11 and 12:
Wiring Overview The pin assignments
Page 13 and 14:
3. INSTRUMENT INSTALLATION This sec
Page 15 and 16:
Instrument Installation The metal s
Page 17 and 18:
e accessed whenever you need to upd
Page 19 and 20:
Instrument Installation (range, MPG
Page 21 and 22:
Instrument Installation SERIAL ALTI
Page 23 and 24:
Instrument Installation Dynon Smart
Page 25:
Connecting Static & Pitot Lines The
Page 28 and 29:
EFIS Calibration and Configuration
Page 30 and 31:
EFIS Calibration and Configuration
Page 32 and 33:
DSAB Configuration Example Networks
Page 34 and 35:
DSAB Configuration Initial Setup As
Page 36 and 37:
DSAB Configuration Network Status T
Page 38 and 39:
Autopilot Installation and Configur
Page 40 and 41:
Page 42 and 43:
Page 44 and 45:
Page 46 and 47: Autopilot Installation and Configur
Page 69 and 70: 7. APPENDIX The appendices contain
Page 71 and 72: Alert Message Description End condi
Page 73 and 74: Appendix Problem After performing a
Page 75 and 76: Appendix Appendix B: Dynon OAT Prob
Page 77 and 78: Appendix CALIBRATION AND ADJUSTMENT
Page 79 and 80: Pinouts and Function Description Ap
Page 81 and 82: Generic Device Connections Appendix
Page 83 and 84: Appendix EFIS-D100 Installation Gui
Page 85 and 86: Appendix PANEL LOCATION AND MOUNTIN
Page 87 and 88: Appendix HS34 CONFIGURATION This se
Page 89 and 90: Appendix occur first in the NAV por
Page 91 and 92: NAV and/or GPS Fail-over Appendix W
Page 93 and 94: TOOLS AND MATERIALS REQUIRED Dynon
Page 95: Appendix Heater Controller Wiring B
Page 99 and 100: Appendix flight regimes not listed
Page 101 and 102: Appendix output, connect this to th
Page 103 and 104: Appendix Appendix F: Replacing the
show all

EFIS-D100 Installation Guide - Dynon Avionics

Create successful ePaper yourself

Delete template?

Save as template?