Dynon Avionics EFIS-D100 Manual de usuario

EFIS-D100

Installation Guide

*** It is the installer’s responsibility to ensure a correct installation. ***

Revised: Wednesday, August 24, 2005

EFIS-D100 Installation Manual

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2005 Dynon Avionics Inc.

This Installation Guide and the information contained herein is the proprietary data of Dynon

Avionics. No part of this manual may be reproduced, copied, transmitted, disseminated or stored

in any storage medium, for any purpose without the express written permission of Dynon

Avionics, Inc. Dynon Avionics, Inc. hereby grants permission to download a single copy of this

manual and of any revision to this manual onto a hard drive or other electronic storage medium

to be viewed for personal use, provided that such electronic or printed copy of this manual or

revision must contain the complete text of this copyright notice and provided further that any

unauthorized commercial distribution of this manual or any revision hereto is strictly prohibited.

Information in this document is subject to change without notice. Dynon Avionics reserves the

right to change or improve its products and to make changes in the content without obligation to

notify any person or organization of such changes. Visit the Dynon Avionics website

(www.DynonAvionics.com) for current updates and supplemental information concerning the

use and operation of this and other Dynon Avionics products

EFIS-D100 is a trademark of Dynon Avionics Inc.

All other brand names and trademarks are the property of their respective holders.

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EFIS-D100 Installation Manual

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Table of Contents .......................................................................................................................... 3

A Note from Dynon Avionics ....................................................................................................... 4

Introduction................................................................................................................................... 5

Description..................................................................................................................................... 5

Tools And Equipment................................................................................................................... 5

Included ...................................................................................................................................... 5

Optional ...................................................................................................................................... 5

Required but not supplied........................................................................................................... 6

Electrical Installation.................................................................................................................... 7

Recommended wiring practices.................................................................................................. 7

Wiring......................................................................................................................................... 8

Power Harness Wiring.............................................................................................................. 10

Altitude Encoder Wiring........................................................................................................... 11

PC Communication Cable Wiring ............................................................................................ 12

EDC-D10A Communication Cable Wiring.............................................................................. 14

Dynon Smart Avionics Bus (DSAB) Wiring............................................................................ 15

Physical Installation.................................................................................................................... 16

Weight....................................................................................................................................... 16

Selecting an appropriate panel location for the EFIS-D100..................................................... 16

Selecting an external magnetic sensor probe location.............................................................. 17

Connecting Static & Pitot Lines ............................................................................................... 18

Mounting into the Panel............................................................................................................ 19

Calibration and configuration ................................................................................................... 20

Ensuring Proper Installation ..................................................................................................... 20

Setting Zero Pitch (In flight)..................................................................................................... 20

Entering the Inclination (Dip) Angle........................................................................................ 20

EDC-D10A Heading Calibration (on ground only).................................................................. 21

Configure Airspeed Color Thresholds...................................................................................... 22

Configure Checklists and Data Panels – PC Connection ......................................................... 23

Appendix...................................................................................................................................... 24

Appendix A: Instructions for Continued Airworthiness........................................................... 25

Appendix B: Dynon OAT Probe Installation and Usage.......................................................... 30

Appendix C: Dynon AOA Pitot Installation and Calibration Guide ........................................ 33

Appendix D: Blind Encoder Serial-to-Parallel Converter Installation ..................................... 36

Appendix E: Replacing the EFIS-D100 battery pack............................................................... 40

Appendix F: EFIS-D100 Installation Checklist........................................................................ 41

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EFIS-D100 Installation Manual

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Congratulations on your purchase of the Dynon Avionics EFIS-D100. As you probably know,

EFIS (Electronic Flight Information System) technology has progressed greatly over the past

several years. Because of the many advances in the technology upon which an EFIS system is

based, we are able to bring you extremely capable avionics at a surprisingly low price.

The EFIS-D100 was designed to be both easy to install and to operate. This guide will walk you

through EFIS-D100 installation while the User’s Guide will help you through the operation of

the unit. For the most up-to-date copy of this manual, visit our website at

www.DynonAvionics.com.

These units are intended for experimental aircraft only at this time. Dynon Avionics makes no

claim as to the suitability of its products in connection with FAR 91.205

EFIS-D100 Installation Manual

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The information presented in this manual pertains to the physical, electrical, and plumbing

installation of the EFIS-D100, EDC-D10A, optional OAT, and optional AOA pitot probe.

Because you may not have purchased all the components, you need only read through the

relevant sections of this guide. Information about the operation of the EFIS-D100 can be found

in the EFIS-D100 User’s Guide

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The EFIS-D100 is a flight information system that utilizes solid-state sensor technology

combined with the power of four microprocessors to give an accurate and easy-to-understand

display. To ensure accuracy in its readings, it is very important that you install the unit correctly

and perform the specified calibration steps. This installation guide will help you through that

process.

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The following parts are included with your EFIS-D100 purchase.

•1 EFIS-D100 main unit

•1 EDC-D10A remote mount compass

•1 EFIS-D100 mounting tray

•1 USB-to-Serial dongle

•1 User Manual

•1 Installation Manual

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The following parts may or may not be included with your EFIS-D100 depending on which

options you selected when you purchased your unit.

•1 Internal emergency battery (already installed, if ordered)

•1 AOA (Angle of Attack) Pitot tube

•1 External outside air temperature (OAT) sensor

•1 Wiring harness

•1 Blind Encoder Serial-to-Parallel Converter

EFIS-D100 Installation Manual

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•Wire cutters

•#2 Phillips screwdriver

•7/64” Allen wrench

•Riveting, welding, or other tools necessary for desired tray installation

•Standard RS232 serial cable

•Laptop computer (or desktop computer close to the plane) for uploading checklists and

new software. It must be running Windows 98 or higher; with at least 64 MB of RAM

and a serial port (or utilize the supplied USB-to-serial adapter).

•Tubes and fittings for routing pitot, static and AOA pressures to the unit.

•1/2” wrench

•1/8”-NPT connectors for mating to pitot, static, and AOA lines

•If you have not purchased the optional Dynon-supplied full wiring harness:

oWire (22 AWG); see recommended wiring practices

oConnector crimp tool

oD25 Female connector with crimp pins

oD9 Female connector with crimp pins for PC interface

oD9 Female connector with crimp pins for EDC-D10A remote mount compass.

EFIS-D100 Installation Manual

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Dynon Avionics sells a wiring

harness with all necessary

connections for operating the EFIS-

D100. If you purchased this harness,

it is recommended that you still read

this entire section to ensure a

complete and accurate installation.

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The following section describes the wiring

requirements for using the EFIS-D100. Please follow

these instructions explicitly as improper wiring

can result in permanent damage to your unit.

All electrical power and data lines interface with the

EFIS-D100 via the 25-pin D-Sub connector on the

back of the unit. You should ensure that all electrical

connections are tested and properly working before

completing the final physical assembly.

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NOTE: For all electrical connections, use correct wiring techniques, taking care to properly

insulate any exposed wire. A short circuit between any of the wires may cause damage to the

EFIS-D100 and/or your airplane. Make all connections to your harness before plugging it into

any of the components of the system. Do not make electrical changes to the harness while it is

connected to the EFIS-D100 or EDC-D10A. For all wiring we recommend that standard aircraft

grade wiring and connectors be used during installation.

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You may use 22 gauge wire for all data wires such as those to the EDC-D10A Magnetic Sensor

Module. 22 gauge wire is normally sufficient for the power supply and ground lines, but you

should consult a wire sizing chart and determine the size required for your routing length. Make

sure you protect the power lines with either a circuit breaker or fuse sized appropriate to the wire

you select.

The EFIS-D100 system-wide power requirements are 12 Watts typical and 24 Watts maximum

(when charging a completely dead internal battery). With a 12 volt system, a 3 amp circuit

breaker or fuse is sufficient. We recommend you use wire meeting Mil Standard MIL-W-

22759/16 (Tefzel insulation) which is available from various suppliers such as Aircraft Spruce.

Another option is to use Teflon insulated wire (Alpha brand is available from Mouser electronics

www.mouser.com) which is available in various colors.

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The EFIS-D100 uses high quality machined pin D-Sub connectors and we recommend you use

machined pin connectors as mates. One source of the machined pins is B&C Specialty Products

(http://bandc.biz/) which also supplies the required crimp tool. Crimp connections have proven to

be the most reliable in aircraft installations. D-Sub shells to hold the pins are available from

various sources such as Mouser mentioned above.

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Make sure all connections are secure and all wires are routed and strain-relieved to ensure the

wires will not chafe against any other object in the aircraft.

EFIS-D100 Installation Manual

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The diagram on the following page details the external electrical connections for the EFIS-D100.

In practice, not all of connections may be needed. The only required electrical connections to

make the EFIS-D100 fully functional are: Master Power (pin 1), Master Ground (pin 3), the

RS232 PC Communication harness (pins 9,10,22), and the remote compass harness (pins 11, 12,

23, 24). A PC is required for loading checklists and new operational software; the EDC-D10A is

also required for magnetic heading information. Note that, as described in the Physical

Installation section, that pitot and static lines must also be connected to ensure proper operation

of the EFIS-D100.

The connector on the EFIS-D100 is a male D25 connector. Your harness needs to terminate with

a female D25 connector.

EFIS-D100 Installation Manual

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Pin Function Harness (typical)

1Master Power (10-30 Volts) Power

2Keep Alive Power (10-30

Volts, always on) Power

3Master GND Power

4DSAB-A Dynon Smart Avionics Databus

5DSAB-B Dynon Smart Avionics Databus

6NC N/A

7NC N/A

8NC N/A

9Serial 1 Gnd PC Communication/EFIS Flight Data

10 Serial 1 Tx PC Communication/EFIS Flight Data

11 EDC-D10A Data B EDC-D10A External Compass

12 EDC-D10A Power (12V) EDC-D10A External Compass

13 Serial 2 Tx Blind Encoder Serial Output

14 NC Do Not Connect

15 External Backup PWR Power

16 DSAB Gnd Dynon Smart Avionics Databus

17 NC N/A

18 Audio out Audio

19 NC N/A

20 NC N/A

21 Serial 2 Gnd Blind Encoder Serial Output

22 Serial 1 Rx PC Communication/EFIS Flight Data

23 EDC-D10A Data A EDC-D10A External Compass

24 EDC-D10A GND EDC-D10A External Compass

25 Serial 2 – Rx Not used – Do Not Connect



Figure 1 Rear view of D-25 connector

EFIS-D100 Installation Manual

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The EFIS-D100 has three separate power inputs. Of the three, only Master Power is required to

operate the unit. The other two inputs provide redundancy. Below is a table that explains the

three inputs and their purposes. All three of these inputs share a common ground signal, wired to

pin 3 on the D25 connector.

Master Power Pin 1 Provides primary power to the instrument. The EFIS-D100 will

switch on upon application of Master Power.

External Backup

Power Pin 15 Will operate the EFIS-D100 only if Master Power is not

present. The transition from losing Master Power to running off

External Backup Power will bring up a Power off warning,

requiring the user to press a button within 30 seconds to

acknowledge this in order to keep operating. This warning will

also display when transitioning from either Master or External

Backup to Internal Battery power.

Keep Alive Power Pin 2 A very low current power input which is only used if both

Master and External Backup Power are not applied. Keep Alive

draws just enough current to keep the clock running and keep

the battery charged. It draws less than 1 milliamp of current

when not charging the internal battery. When charging a

completely dead internal battery, the Keep Alive line can draw

up to an average of 0.4 Amps for 14 hours. If you have the

internal battery and do not wish the EFIS-D100 to draw current

from your plane’s battery, you do not need to connect Keep

Alive. The internal battery will maintain charge without Keep

Alive as long as the master switch power is turned for at least 1

hour per month.

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