Dynon Avionics RV-9 User Manual

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Autopilot Servo Installation Guide

RV9 Roll

This product is not approved for installation in type certificated aircraft

Document 101046-004, Revision G

May, 2014

Permission to print this this manual is granted to third parties

DYNON AVIONICS

Contact Information

Dynon Avionics, Inc.

19825 141st Place NE Woodinville, WA 98072 Phone: (425) 402-0433 - 8:00 AM – 5:00 PM (Pacific Time) Monday – Friday Dynon Technical Support available 7:00 AM–4:00 PM (Pacific Time) Monday – Friday Email: support@dynonavionics.com Fax: (425) 984-1751

Dynon Avionics offers online sales, extensive support, and frequently updated information on its products via its Internet sites:

www.dynonavionics.com –Dynon Avionics primary web site; including: docs.dynonavionics.com – Current and archival documentation including Installation Guides. downloads.dynonavionics.com – Software downloads. support.dynonavionics.com – Support resources. store.dynonavionics.com – Dynon’s secure online store for purchasing all Dynon products 24 hours a day. wiki.dynonavionics.com – Dynon’s Documentation Wiki provides enhanced, extended, frequently updated online

documentation contributed by Dynon employees and customers.

forum.dynonavionics.com – Dynon’s Internet forum where Dynon customers can interact with each other and

Dynon Avionics. A key feature of the forum is that it allows the exchange of diagrams, photos, and other types of files.

newsletter.dynonavionics.com – Dynon’s email newsletter. blog.dynonavionics.com – Dynon’s blog where you can find new and interesting Dynon-related content. register.dynonavionics.com – Register your Dynon Avionics product. license.dynonavionics.com – Redeem certificates for navigation mapping software, synthetic vision, and other

features for license codes that add new functionality to your SkyView system.

2008-2012 Dynon Avionics, Inc. All rights reserved. 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. Dynon Avionics 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.

Servo Mounting Instructions – RV-9 Roll Kit 1 101046-004 Rev G

DYNON AVIONICS

Kit Contents

Dynon Part #

QTY

Part Description

100836-000

Large Male Rod End

100870-001

RV7,8,9,10 Right Roll Bracket

100872-000

RV7,8,9,10 Right Support Bracket

100972-000

RV9 Attach Plate

100966-008

Aluminum Pushrod Tube - 3.0"

100975-002

AN315-4R Jam Nut

100976-011

AN365-1032A Nylon Insert Locknut

100977-000

AN970-3 Large Flat Washer

100978-003

AN960-10 Small Flat Washer

100979-002

MS35333-39 #10 Internal Star Washer

100981-000

AN3H-3A Bolt - 3/8"

100981-005

AN3H-10A Bolt - 1"

100981-012

AN3H-17A Bolt - 1 7/8"

100981-018

AN3H-25A Bolt - 2 5/8"

100982-001

Aluminum Spacer – 0.485"

100982-004

Aluminum Spacer - 0.875"

SERVO MOUNTING INSTRUCTIONS – RV-9 RIGHT WING ROLL KIT

The RV-9 right wing roll servo mounting kit includes a right wing mounting bracket, right wing support bracket, linkage attach plate, pushrod linkage, and most of the required fasteners to mount the servo and properly link it to the aircraft control system. All Dynon-supplied parts are illustrated in dark grey to distinguish them from existing aircraft hardware. The lower bell crank support bracket must be removed to install the supplied servo mounting bracket. Fasteners used to secure the existing brackets will be re-used to install the new Dynon brackets. It is up to the installer to determine if these fasteners are suitable for re-use (these fasteners are not available from Dynon).

The brackets that will replace the existing aircraft brackets are made of 4130 steel and plated per QQP416 CAD - Type II Class II Yellow. They have been designed to meet or exceed the original brackets in strength and corrosion resistance. Install the Dynon-supplied lower servo mounting bracket in place of the existing one, using the previously removed original fasteners.

With the bracket in place, install the 2 AN3H-3A bolts, MS35333-39 star washers, and AN960-10 flat washers to secure the servo to the bracket per the drawing, noting the orientation of the servo output arm. All AN bolts supplied by Dynon have drilled heads for use with safety wire.

Install the support bracket on the other side of the servo using the same bolt stack-up. Verify the wires on the side of the servo pass through the gap in the support bracket and are not pinched

Servo Mounting Instructions – RV-9 Roll Kit 2 101046-004 Rev G

DYNON AVIONICS

Neglecting to properly install and/or use Dynon autopilot hardware may result in failures which could cause loss of aircraft control resulting in aircraft damage, personal injury or death.

between it and the servo. Secure it to the upper bell crank support bracket using the existing fastener. Remove the necessary hardware in order to add the included linkage attach plate and

0.485" spacer using a combination of Dynon-supplied hardware, and existing hardware. With the servo and bell crank additions in place, torque all fasteners back to original installation specifications and add safety wire throughout.

With the servo installed, the linkage needs to be assembled. Refer to the illustration and follow proper rod end installation techniques. Screw at least half of the threads on each rod end into the push rod. To prevent the possibility of the servo arm going over-center, the servo arm must not travel more than a total of +/-60º from neutral throughout the control system's range of travel. The linkage geometry should be installed as close to the Dynon recommendation drawing as possible. Dynon suggests installing the linkage at the middle hole of the servo arm. Changing this location will affect servo torque output, servo arm travel, control surface resolution, and the amount of force required to shear the safety screw, and should only be changed if the installer has an understanding of these implications. See the diagram on the following page which illustrates the linear travel and available force for each mount point on standard-arm servos.

Thread both large rod ends with jam nuts into the supplied 3.0" tube. Standard mounting of the linkage to the servo arm will include the AN3H-10A bolt, AN970-3 large diameter flat washer (for capturing the rod end bearing), 2 AN960-10 flat washers on each side of the servo arm itself, and the AN365-1032A lock nut. The other end of the linkage will require the same type of stack-up, with the addition of the 0.875" spacer and longer AN3H-17A bolt to secure to the drilled aileron bell crank bracket.

The distance between the servo arm and the control system attachment point must allow for the angle between the servo arm and the push rod to be at approximately 90º when the controls are at neutral. Use the adjustability in the rod ends to achieve this, and then tighten the jam nuts to lock the rod ends in place. Installers should always keep in mind the range of motion of the servo. Total servo arm travel is limited, but verify that the arm and linkage do not interfere with anything during the full motion of the control stick. The built-in control stops of the aircraft will limit the servo arm travel when installed correctly. We recommend the use of the optional Range of Motion Limiting Bracket, supplied with the servo to eliminate the chance of the servo arm going over-center. This bracket should not be used as a normal stop; the aircraft's built-in stops should always be the primary range limit.

Your servo(s) and AP74/76 (if ordered) came with a CD containing the latest documentation for all Dynon products (also available at dynonavionics.com). Please read through that documentation to understand the wiring and configuration process for your Autopilot system. We also maintain a collaborative set of this documentation, which is often updated with new information by both Dynon and fellow builders. Visit wiki.dynonavionics.com to view and contribute to the latest version of these documents.

You can also visit forum.dynonavionics.com to discuss and share installation notes, pictures, and suggestions with other builders.

Servo Mounting Instructions – RV-9 Roll Kit 3 101046-004 Rev G

DYNON AVIONICS

Red Black Green Blue Yellow Wht/Grn Wht/Blu

Servo 1

Wires

Pilot-accessible

Servo Power

Switch/Breaker

Aircraft GND

Red Black Green Blue Yellow Wht/Grn Wht/Blu

Servo 2

Wires

Aircraft GND

Aircraft Power (10-30V)

Pitch and Roll Servos

are wired identically, and can

share wiring for convenience at

any point along the run.

5 kohm

Optional resistor for

detecting broken

disengage lines

Pilot-accessible

Disengage/CWS button (Normally open, momentary) Usually mounted to the stick

Power (10-30V) Ground SkyView Network 1 A or DSAB A SkyView Network 1 B or DSAB B Disengage SkyView Network Data 2 A * SkyView Network Data 2 B *

Servo Current Draw at 12V (halve the current values for 24V systems)

SV32 Powered but disengaged: 0.1 amps Engaged and holding, 100% torque: 0.80 amps Engaged and moving, 100% torque: 1.33 amps

SV42 Powered but disengaged: 0.1 amps Engaged and holding, 100% torque: 1.11 amps Engaged and moving, 100% torque: 2.03 amps

SV52 Powered but disengaged: 0.1 amps Engaged and holding, 100% torque: 1.52 amps Engaged and moving, 100% torque: 2.80 amps

Aircraft GND

Use 22 AWG wire for SkyNet

and Disengage signals.

Use appropriate wire gauge for

servo power based on current

consumption and length of wire run

Green

Blue

Twisted Pair

D10A/D100/D180

D25

CONNECTOR

SKYVIEW

CONNECTOR

N/A N/A

5 4

4 8 6 1

WHT/BLU WHT/GRN

BLU GRN

Wht/Grn

Wht/Blu

*NOT USED FOR D10A/D100/D180

Wiring Overview

The following diagram provides an overview of the autopilot-specific wiring installation. For the complete set of wiring and configuration instructions, please see the latest Installation Guide for your Dynon EFIS product. For a SkyView system please reference the Autopilot Servo Installation, Configuration, and Calibration chapter of your SkyView System Installation guide. For EFIS-D10A, EFIS-D100 or FlightDEK-D180 please reference the Autopilot Installation and Configuration chapter of each respective Installation Guide.

Servo Mounting Instructions – RV-9 Roll Kit 4 101046-004 Rev G

DYNON AVIONICS

Long-arm variants

(not needed in most

installations)have

linkage mount holes

at 1.5”, 1.75”, and

2.0”

Weight

SV32

2.17”

2 lb

SV42

3.10”

3 lb

SV52

4.02”

4 lb

Servo Dimensions

Use the following dimensions (in inches) for reference when planning and implementing your installation.

Servo Mounting Instructions – RV-9 Roll Kit 5 101046-004 Rev G

DYNON AVIONICS

Standard Arm

Max Linear Travel A: 2.6”, B: 2.2”, C: 1.8”

Max Force @ 100% Torque SV32 - A: 24lb, B: 29lb, C: 36lb

Linkage mount position force and travel

The diagram below illustrates the maximum travel and force available at each linkage mounting point. As can be seen, the closer you mount the linkage to the shaft, the more force the servo can deliver. However, this also means the travel of the arm is shorter. Again, ensure that the servo arm is nowhere near going over-center throughout the entire range of the control system.

Position B should be used in most RV-9 roll installations. Modify mount position with caution and take all precautions to ensure that a near over center condition cannot occur

The autopilot safety shear screw should NEVER be removed or adjusted during this

operation. If the shear screw has broken and needs replacement, there is specific

documentation available for this purpose at http://docs.dynonavionics.com.

Mounting Drawings

The following pages provide detailed views of the mounting and assembly of the servo and this kit.

Servo Mounting Instructions – RV-9 Roll Kit 6 101046-004 Rev G