EFIS-D100 Installation Guide - Dynon Avionics

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Autopilot Installation and Configuration SERVO DIMENSIONS Use the following dimensions (in inches) for reference when planning and implementing your installation. Long-arm variants (not needed in most installations) have linkage mount holes at 1.5”, 1.75”, and 2.0” L SV32 2.17” SV42 3.10” SV52 4.02” Weight 2 lb 3 lb 4 lb 6-8 EFIS-D100 Installation Guide
Autopilot Installation and Configuration LINKAGE MOUNT POSITION FORCE AND TRAVEL The two diagrams below illustrate 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. 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 SV42 - A: 36lb, B: 44lb, C: 55lb SV52 - A: 48lb, B: 58lb, C: 72lb Long Arm Max Linear Travel A: 3.4”, B: 3.0”, C: 2.6” Max Force @ 100% Torque SV32L - A: 18lb, B: 20lb, C: 24lb SV42L - A: 27lb, B: 31lb, C: 36lb SV52L - A: 36lb, B: 41lb, C: 48lb In most instances, it is recommended to connect the servo arm to the control linkages using the outer-most hole of the servo arm (position A). This position provides the greatest amount of travel, with the least amount of drive force. If, when testing the autopilot, you find that the servos cannot adequately drive the control system (indicated by a yellow “slip indicator” in the AP status at the bottom left of the EFIS screen), you may move the linkage mount point inward, provided there is still enough travel to accommodate the control system at the servo location. Using either of the two inner-most holes of the servo arm affects the final amount of force that EFIS-D100 Installation Guide 6-9
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 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 and 96:
Appendix Heater Controller Wiring B
Page 97 and 98:
these lines, you may drill all the
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
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EFIS-D100 Installation Guide - Dynon Avionics

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