EFIS-D60 Installation Guide - Dynon Avionics
EFIS-D60 Installation Guide - Dynon Avionics EFIS-D60 Installation Guide - Dynon Avionics
Appendixthese lines, you may drill all the way through the outer metal without affecting the probe’swaterproofing.DIMENSIONSStandard mount5-12 EFIS-D60 Installation Guide
AppendixBoom mountPLUMBINGNOTE: Because the pitot and AOA plumbing tubes have not been annealed, they work-hardenrapidly when manipulated. Make gentle bends, and only bend any given section once.After mounting the probe, route the pitot and AOA lines from the probe to your EFIS-D60. Thetube closest to the snout is the pitot line, while the tube in the rear is the AOA line. There is nostatic source on the probe.After mounting the probe, install adapters to connect the 3/16 plumbing lines from the probe towhatever plumbing lines run back to the EFIS-D60 in your aircraft (AN 919-2D for 3/16 to ¼).We strongly recommend using aircraft grade fittings such as standard AN fittings. Make sure theplumbing lines do not chafe or interfere with any aircraft control systems.PRESSURE CHECKDynon’s pitot design deliberately has a pin-sized leak hole in each of the two tubes to permitdraining any moisture which might accumulate inside. These holes are located in the middle ofthe tube at the bottom. Plugging these holes does not guarantee a pneumatic seal (although one issometimes present). The leak that may exist does not affect the performance of the probe. Youwill, however, need to take it into account when doing pressure/leak tests on your pitot systemCALIBRATIONCAUTION: It is your responsibility to fly your plane safely while performing anyconfiguration or calibration in flight. The best scenario would include a second person toperform any necessary steps on the EFIS-D60.Once you are flying straight and level at a safe altitude for stalls, enter the SETUP > AOACALmenu. While the AOACAL menu is displayed, oscillate the aircraft between ± 5° pitch 4 times atfast cruise airspeed. During this maneuver the EFIS-D60 records the lowest angle of attack thatyou usually see during flight. You do not need to push any additional buttons before starting thismaneuver.Refer to the list below of the stalls recommended to complete the user calibration. The generalidea is to record stall data to find the lowest angle of attack stall. The list we have suggested is astarting point and produces a good calibration under most circumstances. However, if there areEFIS-D60 Installation Guide 5-13
- Page 1: EFIS-D60Installation GuideThis prod
- Page 5: Table of ContentsContact Informatio
- Page 8 and 9: IntroductionAbout this GuideIn the
- Page 10 and 11: Wiring Overview25-Pin Female EFIS H
- Page 12 and 13: Wiring OverviewWIRING SYSTEM OVERVI
- Page 14 and 15: Instrument Installation• All moun
- Page 16 and 17: Instrument InstallationPC CONNECTIO
- Page 18 and 19: Instrument InstallationSERIAL ALTIT
- Page 20 and 21: Instrument InstallationPanel Locati
- Page 23 and 24: 4. EFIS CALIBRATION AND CONFIGURATI
- Page 25 and 26: EFIS Calibration and ConfigurationE
- Page 27 and 28: 5. APPENDIXThe appendices contain a
- Page 29 and 30: Alert Message Description End condi
- Page 31 and 32: AppendixProblemAfter performing a m
- Page 33 and 34: AppendixAppendix B: Dynon AOA/Pitot
- Page 35 and 36: Appendixinstructions on the followi
- Page 37: Appendixcontroller. Remember that e
- Page 41 and 42: AppendixAppendix C: Encoder Serial-
- Page 43 and 44: AppendixEFISDB25Pin#13Dynon EFIShar
- Page 45: AppendixAppendix F: WeightsAdding a
AppendixBoom mountPLUMBINGNOTE: Because the pitot and AOA plumbing tubes have not been annealed, they work-hardenrapidly when manipulated. Make gentle bends, and only bend any given section once.After mounting the probe, route the pitot and AOA lines from the probe to your <strong>EFIS</strong>-<strong>D60</strong>. Thetube closest to the snout is the pitot line, while the tube in the rear is the AOA line. There is nostatic source on the probe.After mounting the probe, install adapters to connect the 3/16 plumbing lines from the probe towhatever plumbing lines run back to the <strong>EFIS</strong>-<strong>D60</strong> in your aircraft (AN 919-2D for 3/16 to ¼).We strongly recommend using aircraft grade fittings such as standard AN fittings. Make sure theplumbing lines do not chafe or interfere with any aircraft control systems.PRESSURE CHECK<strong>Dynon</strong>’s pitot design deliberately has a pin-sized leak hole in each of the two tubes to permitdraining any moisture which might accumulate inside. These holes are located in the middle ofthe tube at the bottom. Plugging these holes does not guarantee a pneumatic seal (although one issometimes present). The leak that may exist does not affect the performance of the probe. Youwill, however, need to take it into account when doing pressure/leak tests on your pitot systemCALIBRATIONCAUTION: It is your responsibility to fly your plane safely while performing anyconfiguration or calibration in flight. The best scenario would include a second person toperform any necessary steps on the <strong>EFIS</strong>-<strong>D60</strong>.Once you are flying straight and level at a safe altitude for stalls, enter the SETUP > AOACALmenu. While the AOACAL menu is displayed, oscillate the aircraft between ± 5° pitch 4 times atfast cruise airspeed. During this maneuver the <strong>EFIS</strong>-<strong>D60</strong> records the lowest angle of attack thatyou usually see during flight. You do not need to push any additional buttons before starting thismaneuver.Refer to the list below of the stalls recommended to complete the user calibration. The generalidea is to record stall data to find the lowest angle of attack stall. The list we have suggested is astarting point and produces a good calibration under most circumstances. However, if there are<strong>EFIS</strong>-<strong>D60</strong> <strong>Installation</strong> <strong>Guide</strong> 5-13