SkyView Airplane Flight Manual Supplement

SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | i SkyView Airplane Flight Manual Supplement (or Supplemental Airplane Flight Manual) STC SA02594SE For Software Version 16.7.2 103272-000 Copyright © 2024 by Dynon Avionics, Inc. Dynon Avionics grants third parties' permission to print this document SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | ii Contact Information Dynon Avionics, Inc. 19825 141st Place NE Woodinville, WA 98072 Technical Support Phone: +1 (425) 399-7742, 8:00 AM – 5:00 PM (Pacific Time) Monday – Friday Email: support@dynoncertified.com Sales Phone: +1 (425) 650-1269, 8:00 AM – 5:00 PM (Pacific Time) Monday – Friday Email: sales@dynoncertified.com Find Us on the Web dynoncertified.com – Dynon Certified homepage dynoncertified.com/docs – Product documentation dynoncertified.com/download – Software updates for products dynoncertified.com/support – Support resources dynoncertified.com/register – Register your Dynon Avionics product Stay in Touch dynoncertified.com/newsletter – Sign up to receive Dynon’s newsletter forum.flydynon.com – Dynon-hosted forum for customers and pilots preflight.dynon.com – Dynon’s blog facebook.com/dynonavionics instagram.com/dynonavionics twitter.com/dynon Videos and Training youtube.com/DynonAvionics – Training, events, and other videos on YouTube Copyright ©2024 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 (dynon.com) for current updates and supplemental information concerning the use and operation of this and other Dynon Avionics products. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | iii FAA Approval Dynon Avionics 19825 141st Pl NE Woodinville, WA 98072 (425) 402-0834 Airplane Registration: ______________________________ Airplane Manufacturer: ______________________________ Airplane Model: ______________________________ Airplane Serial Number: ______________________________ This document serves as a supplement to the aircraft flight manual, or as a supplemental flight manual. It must be attached to the FAA Approved Airplane Flight Manual (AFM) or, when no AFM exists, used as a supplemental aircraft operating manual when the SkyView HDX system is installed in accordance with STC SA02594SE. The information contained herein supplements the information of the basic Airplane Flight Manual. For Limitations, Procedures, and Performance information not contained in this Supplement consult the basic Airplane Flight Manual or the placards and markings in the aircraft. The following sections of this document are FAA APPROVED: 2: Limitations 3: Emergency & Non-Normal Procedures 4: Normal Operations 5: Performance 9: Appendix 1: Cessna Models 172F through 172S 10: Appendix 2: Cessna Models 182E–T, T182, R/TR182 11: Appendix 3: Beechcraft Bonanza P35 through V35B 12: Appendix 4: Beechcraft Bonanza 36 13: Appendix 5: Piper PA-34 Seneca 14: Appendix 6: Beechcraft Baron 58, 58A 15: Appendix 7: Mooney M20J and M20K ___________________________________________________________, for Manager, Flight Test and Human Factors Branch, AIR-710 Federal Aviation Administration Approved Date SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | iv Revision History REV DYNON SUBMITTAL DATE FAA ACCEPTANCE DATE CHANGE DESCRIPTION V 05/02/2024 ECO 391623 Mooney Autopilot Changes: • Added Mooney M20J and M20K to FAA Approval Section. • Added Section 15: Appendix 7: Mooney M20J and M20K. Software 16.7.2 Changes: • Green range fill coloring on CHT and EGT widgets fixed. Updated Figure 30 in Section 7.11.5. U 12/13/2023 ECO 388468 FAA APPROVED Al Wilson, Manager, AIR-710, 12/13/2023 • Added Beechcraft Baron 58, 58A to FAA Approval Section. • Added Section 14: Appendix 6: Beechcraft Baron 58, 58A. T 7/12/2023 ECO 376163 FAA APPROVED Al Wilson, Manager, AIR-710, 8/24/2023 • Added STC # to cover page per FAA feedback. • Revised first paragraph in Section 1: General per FAA feedback on similar documents. • Added SkyView HDX System Functional Overview document to Section 1.5: Reference Documents. • Revised procedures in Section 3: Emergency & Non-Normal Procedures per DER feedback on similar document. • Revised Section 7.9: Operational Software to point to SkyView HDX Installation document. • Revised and updated alert artwork in Section 7.10: Flight Crew Alerting System per latest S/W and per DER feedback on similar document. (No change bars if change was only new artwork.) • Revised Section 7.9: Operational Software to point to SkyView HDX Installation document. • Revised and updated screenshots in Section 7.11.2: Engine Monitoring per latest S/W and DER feedback. • Updated screenshots in Section 7.12: Autopilot per latest software. • Revised Section 7.12.6.2: Trim Alerts to list all possible alerts. • Added Section 7.12.6.6: Servos Offline per latest software. Subsequent sections renumbered. • Added Section 7.12.6.7: Servo Errors per latest software. Subsequent sections renumbered. S 6/28/2023 ECO 387323 FAA APPROVED Al Wilson, Manager, AIR-710, 6/28/2023 • Updated the title block in FAA Approval section. • Removed reference to EFIS-D10A and added references to new Dynon D30 standby display in Sections 2.1, 4.3, and 7.2. R 9/8/2022 ECO 377682 Accepted by Seattle AIR-715 on 10/06/2022 • Added Cessna 182E-T, T182, R/TR182 to FAA Approval Section. • Added new Section 10: Appendix 2: Cessna 182 E-T, T182, R/TR182. Subsequent sections renumbered. Q 11/05/2021 ECO 360038 Accepted by Seattle AIR-715 on 11/08/2021 • Revised Contact Information section and links within doc with current info and locations. • Revised following sections per feedback received from FAA 11/04/2021: ▪ 1.1: Document Control, added verbiage about what revision of doc is posted. ▪ 3.2.1: Loss of Airspeed, Altitude, Attitude, and/or Heading Display, revised procedure to clarify the aural annunciation. ▪ 4.5: Autopilot Operation Check, moved note to Section 4.5.2. ▪ 7.10.3: Caution Alerts and Table 3, revised procedures to sync with emergency and non-normal procedures. • 7.12: Autopilot, added verbiage about autopilot not controlling throttle. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | v REV DYNON SUBMITTAL DATE FAA ACCEPTANCE DATE CHANGE DESCRIPTION P 10/28/2021 ECO 360038 Not Accepted • Revised following sections per feedback received during Dynon/FAA meeting on 10/27/2021: ▪ 1: General, revised verbiage about optional autopilot. ▪ 2.6: Autopilot, added two new limitations. ▪ 3.1.1: Airspeed, Altitude, and/or Attitude Unreliable, revised emergency procedure to sync with Alerting tables. ▪ 3.1.4: Trim Runaway, revised emergency procedure to sync with Alerting tables. ▪ 3.2.1: Loss of Airspeed, Altitude, Attitude, and/or Heading Display, revised non-normal procedure to sync with Alerting tables. ▪ 3.2.4: GPS # Fail, revised verbiage to sync with Alerting tables. ▪ 3.2.5: GPS Position # Fail, revised verbiage to sync with Alerting tables. ▪ 3.2.6: Autopilot Disconnect, revised verbiage to sync with Alerting tables. ▪ 3.2.7: Yaw Damper Disconnect, revised verbiage to sync with Alerting tables. ▪ 4.1.11: G Meter, revised verbiage about G Meter being automatically removed. ▪ 4.4: Autopilot Controls, revised verbiage about optional autopilot. ▪ 4.4.1: Engage Autopilot, revised verbiage about SkyView Auto-trim. ▪ 4.4.3: AP DISC (Autopilot Disconnect) Button, revised verbiage about SkyView Auto-trim. ▪ 4.5: Autopilot Operation Check, revised verbiage about optional yaw damper. ▪ 7.10.2: Warning Alerts and Table 2, revised verbiage to sync with emergency and non-normal procedures. ▪ 7.10.3: Caution Alerts and Table 3, revised verbiage to sync with emergency and non-normal procedures. ▪ 7.10.4: Messages and Table 4, revised verbiage to sync with emergency and non-normal procedures. ▪ 7.12.2: Protective Features, revised verbiage to make autopilot bank limit clearer. ▪ 7.12.5: SkyView Auto-trim, revised verbiage about SkyView Auto-trim and trim power switch. ▪ 7.12.11: Yaw Damper, revised verbiage about yaw damper function. ▪ 9: Supplements (old section removed from document) ▪ 9.1: Autopilot (old section and subsections moved to Section 7.12) • 9.1, 10.1, 11.1, 12.1: Autopilot Limitations, added new limitation. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | vi REV DYNON SUBMITTAL DATE FAA ACCEPTANCE DATE CHANGE DESCRIPTION O 10/14/2021 ECO 360038 Not Accepted • Revised format of Revision History table per FAA feedback. • All but one instance of "Frangible Link" changed to "Shear Screw" to standardize nomenclature across Dynon documentation. • Revised format of Section 2.1: IFR Operations to standardize format with other subsections. • Added Section 2.6: Autopilot per FAA feedback. • Revised Section 3.1.1: Airspeed, Altitude, and/or Attitude Unreliable for clarity and usability. • Added Section 3.1.4: Trim Runaway. • Added Section 4.1.11: G Meter. Subsequent sections renumbered. • Updated Section 4.4.1: Engage Autopilot with info about Auto-Trim. • Revised Section 4.4.2: Disengage Autopilot. • Revised Section 4.4.3: AP DISC Button. • Added Section 4.4.4: AP POWER Switch. Subsequent sections renumbered. • Added Section 4.4.5: TRIM POWER Switch. Subsequent sections renumbered. • Revised Section 6: Weight and Balance per FAA feedback. • Revised format of Section 7: System Overview to remove installation info. • Revised format of Section 7.4: Map for clarity and usability. • Added Section 7.6: Traffic Information. Subsequent sections renumbered. • Added Section 7.6.1: Traffic Targets. • Added Section 7.6.2: Target Symbols. • Added Section 7.6.3: Traffic Alerts. • Added Section 7.7: Weather Information. Subsequent sections renumbered. • Updated external links in Section 7.8 Navigation Databases. • Updated external links in Section 7.9 Operational Software. • Revised Section 7.10: Flight Crew Alerting System per FAA feedback. • Revised Section 7.10.1: Notification Methods per FAA feedback. • Revised and updated Section 7.10.2: Warming Alerts per FAA feedback and to add new alerts and alerts that were shown elsewhere in doc. • Revised and updated Section 7.10.3: Caution Alerts per FAA feedback and to add new alerts and alerts that were shown elsewhere in doc. • Revised and updated Section 7.10.4: Messages per FAA feedback and to add new messages and messages that were shown elsewhere in doc. • Revised format of Section 8: Handling, Service, and Maintenance to remove installation info. • Updated Section 9.1.4.1: Autopilot Indications to show all AP activity in the AP Info Bar. • Added Section 9.1.5: Auto-Trim. Subsequent sections renumbered. • Added Section 9.1.6.5: G Limit Alert. • Added new Section 12: Appendix 3: Beechcraft Bonanza 36. Subsequent appendices renumbered. N 10/23/2020 ECO 360164 Accepted by Seattle AIR-715 on 10/29/2020 • Moved FAA Approval page per FAA request. (page iii) M 10/08/2020 ECO 358194 Not Accepted • Moved FAA Approval page to first page per GAMA 1 guidelines. • Moved References page to Section 1: General • Added new Section 2.2: Engine Monitoring Visibility to Section 2: Limitations. Subsequent Section 2 headings renumbered. • Moved old Section 3.1.2: Autopilot / Yaw Damper Override to new Section 9.1.1. Subsequent Section 6 headings renumbered. • Updated language in new Section 3.1.3 Autopilot / Yaw Damper Servo Jam. • Updated language in Table 2: Warning Alerts, Table 3: Caution Alerts, Table 4: Messages per FAA feedback. • Updated language in 7.9.2: Engine Monitoring per FAA feedback. L 9/14/2020 ECO 356791 Not Accepted • Updated document footers per GAMA 1 guidelines (all pages affected). • Updated FAA Approval section (Page X) per FAA feedback. • Updated Tables 2, 3, 4 (Pages 7-4 through 7-20) with new column heads and some language/terminology changes per FAA feedback. • Updated Sections 10 (Page 10-1), 11 (Page 11-1), 12 (Page 12-1) to use prohibitive language per FAA feedback. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | vii REV DYNON SUBMITTAL DATE FAA ACCEPTANCE DATE CHANGE DESCRIPTION K 08/11/2020 ECO 353760 Not Accepted • Reorganized document according to GAMA 1 guidelines. • Aircraft-specific information moved to separate Appendices to aid technical reviews of document as more Autopilots are added to airplanes on the AML. • Failure Modes (now Section 3.2) renamed to Non-Normal Procedures and content converted to GAMA style procedures. Emergency Procedures: Autopilot Disconnect and Yaw Damper Disconnect moved from Emergency Procedures to Non-Normal Procedures. • Engage Autopilot (now Section 4.4.1) updated per feedback from FAA/Dynon meeting. • Warning Alerts (now Section 7.8.2) updated per Dynon software developer input. • Caution Alerts (now Section 7.8.3) updated per feedback from FAA/Dynon meeting and Dynon software development input. • Message Alerts (now Section 7.8.4) updated per Dynon software developer input. • Airspeed Indicators (now Section 7.9.1) updated per feedback from FAA/Dynon meeting. • Engine Monitoring (now Section 7.9.2) updated per feedback from FAA/Dynon meeting. • Autopilot Protective Features (now Section 9.1.1) updated to include servo break-away information. J 05/01/2020 ECO 346986 Not Accepted • Addressed FAA review feedback on Rev H: ▪ Re-ordered Table 1: Warnings, Table 2 Cautions, and Table 3: Messages. Ordering is by 1) core system, 2) component, 3) function per type of alert. ▪ Updated Section 4.2.1, 4.2.3, and 4.2.3 with additional screenshots and verbiage to clearly differentiate single- and twin-engine EMS indications. ▪ Updated Section 4.5 with new screenshot. ▪ Added Table 4: Autopilot Fail Down Modes in Section 6.1, describing Autopilot fail down modes. Subsequent tables renumbered. ▪ Re-arranged screenshots in Section 6.4 for readability. Updated screenshot in Section 6.4.4 to reflect UI. ▪ Removed table from Section 6.4, as information was outdated. Updated Sections 6.4.1 through 6.4.4 to sync with info in Section 3. ▪ Updated procedure in Section 7.14 to disable Dual Mode. ▪ Updated verbiage in Section 7.18 to be clearer. ▪ Added new Section 7.26.2: Yaw Axis Operation Check. Subsequent sections renumbered. ▪ Removed 2 limitations from Section 9: Limitations per FAA request. • Updated Section 10.6: Autopilot / Yaw Damper Servo Jam to clearly describe role of frangible link. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | viii REV DYNON SUBMITTAL DATE FAA ACCEPTANCE DATE CHANGE DESCRIPTION I 04/10/2020 ECO 346079 Not Accepted • Addressed FAA review comments on Rev H, including: ▪ Update Section 2: System Overview to better distinguish between Primary, Secondary, and Standby EFIS displays. ▪ Replace Section 3: Flight Crew Alerting System with new, updated information. ▪ Updated the following sections of Section 4: Indications for technical accuracy: o 4.1 Airspeed Indicator o 4.3 Landing Gear Position Indicators ▪ Updated the following sections of Section 6: Autopilot for technical accuracy: o 6.1: Protective Features o 6.4.2: Trim Messages o 6.4.3: Slip Trim Messages o 6.5: Autopilot Controls o 6.6: Vertical Guidance Source Loss o 6.9: Yaw Damper ▪ Updated the following sections of Section 7: Normal Operations for technical accuracy: o 7.10: Course (OBS) Setting o 7.11: HDX Backup Power Check o 7.13: Backup EFIS-D10A Battery Condition Check o 7.16: Yaw Damper o 7.10: Course (OBS) Setting o 7.11: HDX Backup Power Check o 7.13: Backup EFIS-D10A Battery Condition Check o 7.16: Engage Autopilot o 7.17: Engage Flight Director o 7.18: Disengage Autopilot o 7.22: Go Around o 7.25: Approaches o 7.26: Autopilot Operational Check ▪ Updated the following sections of Section 9: Limitations for technical accuracy: o 9.1: General o 9.2: Backup Power o 9.6.4: Piper Aircraft PA-34 Seneca ▪ Updated Section 10:1: Airspeed, Altitude and/or Attitude Unreliable for technical accuracy. • Proofread document and fixed language, layout, and linking issues. • Removed outdated links and references. H 03/03/2020 ECO 344060 Not Accepted • Applied new document template. • Added information in Section 3.7, 3.10, 3.11 for twin engine airplanes / Dual EMS. • Added Section 4.5: Temperature Indicators. • Added Section 4.6: Synchroscope. • Added Section 6.4.2: Trim Messages. • Added Section 6.4.3: Slip Trim Messages. • Revision to Section 6.9: Yaw Damper behavior. • Added Section 9.6.4: Piper Aircraft PA-34 Seneca. G 07/02/2019 ECO 331341 Accepted by Seattle AIR-715 on 07/02/2019 • Changed name of document to "SkyView HDX Airplane Flight Manual Supplement". • Added note regarding use of this document as an SAFM. F 04/29/2019 ECO 327677 Not Accepted • Changed section 3.6 to reference "14 CFR 23.1545" instead of "FAR 23.1545". • Changed wording in section 5.5 to read "pull" instead of "turn off" with reference to circuit breakers. • Updated Figure 18 E 04/10/2019 ECO 326715 Not Accepted • Added autopilot slip, trim, slip/trim, airspeed high/low message. • Added autopilot VNAV engagement caution. • Formatted emergency procedures for improved clarity. • Added autopilot servo jam emergency procedure. • Clarified language on FAA approval signature page. • Formatted section 5.5 (Autopilot Operation) for improved clarity. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | ix REV DYNON SUBMITTAL DATE FAA ACCEPTANCE DATE CHANGE DESCRIPTION D 04/01/2019 ECO 324900 Not Accepted • Added 6-cylinder EGT/CHT, Flaps and Landing Gear functionality, • Revised illustrations, • Moved Airplane Limitations to section 8, and Emergency Procedures to Section 9, • Revised format of Emergency Procedure checklist, • Deleted the appendix. • Revised limitations section for new models C 07/10/2018 Accepted by Seattle AIR-715 on 10/11/2018 • Added knob modules and updated operating limitation. B 06/08/2018 Accepted by Seattle AIR-715 on 07/20/2018 • Added 91.227 Language A 03/05/2018 Not Accepted • Initial Submission. Technical changes since previous revision are tracked with change bars in margins. Formatting and style changes are not tracked. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | x Table of Contents 1 General .................................................................................................. 1-1 1.1 Document Control........................................................................................................... 1-1 1.2 Using this Document ...................................................................................................... 1-1 1.3 Intended Audience.......................................................................................................... 1-1 1.4 Manual Iconography ....................................................................................................... 1-2 1.5 Reference Documents.................................................................................................... 1-2 2 Limitations ............................................................................................ 2-1 2.1 IFR Operations................................................................................................................ 2-1 2.2 Engine Monitoring Visibility ............................................................................................ 2-1 2.3 Synthetic Vision .............................................................................................................. 2-1 2.4 Map.................................................................................................................................. 2-1 2.5 Autopilot .......................................................................................................................... 2-2 3 Emergency & Non-Normal Procedures ............................................... 3-1 3.1 Emergency Procedures .................................................................................................. 3-1 3.2 Non-Normal Procedures................................................................................................. 3-3 4 Normal Operations................................................................................ 4-1 4.1 General............................................................................................................................ 4-1 4.2 SkyView HDX Backup Power Check............................................................................. 4-8 4.3 Standby Flight Display Backup Battery Condition Check............................................. 4-9 4.4 Autopilot Controls ........................................................................................................... 4-9 4.5 Autopilot Operation Check ........................................................................................... 4-14 5 Performance.......................................................................................... 5-1 6 Weight and Balance .............................................................................. 6-1 7 System Overview .................................................................................. 7-1 7.1 SkyView HDX Display Units........................................................................................... 7-1 7.2 Standby Display System ................................................................................................ 7-1 7.3 Synthetic Vision .............................................................................................................. 7-1 7.4 Map.................................................................................................................................. 7-1 7.5 Terrain Alerts .................................................................................................................. 7-2 7.6 Traffic Information ........................................................................................................... 7-2 SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | xi 7.7 Weather Information ....................................................................................................... 7-5 7.8 Navigation Databases .................................................................................................... 7-5 7.9 Operational Software...................................................................................................... 7-5 7.10 Flight Crew Alerting System........................................................................................... 7-6 7.11 Indications ..................................................................................................................... 7-28 7.12 Autopilot ........................................................................................................................ 7-39 8 Handling, Service, and Maintenance ................................................... 8-1 9 Appendix 1: Cessna 172F–S ................................................................ 9-1 9.1 Autopilot Limitations ....................................................................................................... 9-1 9.2 Autopilot Servo Shear Screw Break-Away Forces ....................................................... 9-1 10 Appendix 2: Cessna 182E–T, T182, R/TR182 .................................... 10-1 10.1 Autopilot Limitations ..................................................................................................... 10-1 10.2 Autopilot Servo Shear Screw Break-Away Forces ..................................................... 10-1 11 Appendix 3: Beechcraft Bonanza Models P35–V35B ....................... 11-1 11.1 Autopilot Limitations ..................................................................................................... 11-1 11.2 Autopilot Servo Shear Screw Break-Away Forces ..................................................... 11-1 12 Appendix 4: Beechcraft Bonanza 36.................................................. 12-1 12.1 Autopilot Limitations ..................................................................................................... 12-1 12.2 Autopilot Servo Shear Screw Break-Away Forces ..................................................... 12-1 13 Appendix 5: Piper Seneca PA-34 ....................................................... 13-1 13.1 Autopilot Limitations ..................................................................................................... 13-1 13.2 Autopilot Servo Shear Screw Break-Away Forces ..................................................... 13-1 14 Appendix 6: Beechcraft Baron 58, 58A.............................................. 14-1 14.1 Autopilot Limitations ..................................................................................................... 14-1 14.2 Autopilot Servo Shear Screw Break-Away Forces ..................................................... 14-1 15 Appendix 7: Mooney M20J and M20K................................................ 15-1 15.1 Autopilot Limitations ..................................................................................................... 15-1 15.2 Autopilot Servo Shear Screw Break-Away Forces ..................................................... 15-1 SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 1-1 1 General This document is the Airplane Flight Manual Supplement (AFMS) for the Dynon SkyView HDX system. The information herein is applicable to all airplanes on the Approved Model List (AML) of Supplemental Type Certificate (STC) SA02594SE. SkyView is an integrated system that aggregates air, engine, traffic, and navigation information for display to the pilot. The information is portrayed on the SkyView HDX display, which is a touchscreen, coupled with mechanical knobs and buttons. The SkyView HDX display provides Primary Flight Information (PFI) on the Primary Flight Display (PFD), Map with current position, and optionally Engine Monitoring information. Subsystems, such as the Autopilot, Communications, Transponder, as well as third-party equipment integrate with SkyView HDX to perform their functions. (See the 103014-000 Skyview HDX System Functional Overview document at dynoncertified.com/docs for additional information about all SkyView components, feature, and functions.) 1.1 Document Control This document is released, archived, and controlled according to the Dynon Avionics document control system. To revise this document, a letter is submitted to the FAA with the revision. The FAA then accepts and approves any revision to the content listed in the FAA Approval section. After FAA acceptance/approval, Dynon posts the revised document for customer use at dynoncertified.com/docs. Only the latest revision of the document is made available. STC owners and installers are notified of the new revision via an official Dynon Marketing email release. 1.2 Using this Document To reduce paper, Dynon does not provide a printed version of this manual. However, Dynon grants permission to third parties to print this manual, as necessary. The most recent PDF version is available for download at dynoncertified.com/docs. This manual is updated periodically. It is mandatory to keep a printed copy of the most recent revision in the airplane. 1.3 Intended Audience This document is intended for owners and/or operators of aircraft retrofitted with a Dynon SkyView HDX system. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 1-2 1.4 Manual Iconography This manual uses the following iconography: Alerts reader to important information that mitigates potential unsafe conditions and/or equipment damage. Alerts reader to noteworthy technical information. Alerts reader to helpful tips or suggestions. 1.5 Reference Documents • 103014-000 Skyview HDX System Functional Overview • 102949-000 SkyView HDX Pilot’s User Guide (current revision) • 103261-000 SkyView HDX System Installation Manual (current revision) • 103221-000 SkyView HDX System General Maintenance Manual (current revision) • 104004-000 D30 Airplane Flight Manual Supplement (current revision) SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 2-1 2 Limitations The limitations listed in this section apply to all airplanes with a SkyView HDX system. 2.1 IFR Operations SkyView HDX system must have at least one of each of the following components in fully functioning condition, with no error messages displayed: • SkyView HDX display unit, • SV-ADAHRS-200 module, • SV-BAT-320 backup battery, • EFIS-D10A or D30 standby display, • Functioning external navigation source, either an IFR GPS Navigator or NAV radio. IFR flight with Yellow or Red Backup Battery indicator status displayed is prohibited. 2.2 Engine Monitoring Visibility For all airplanes equipped with an Engine Monitoring System (EMS): • Configuring the screen layout of a SkyView HDX display unit so the primary engine instruments are not visible to the pilot is prohibited. For twin-engine airplanes with an EMS: • A secondary (non-PFD) Skyview HDX display unit must be installed and dedicated to present Engine Monitoring information. • The SkyView HDX display unit dedicated to present Engine Monitoring information must be configured to always show (no exceptions) EMS information in either 100% or 50% display page layout during takeoffs and landings. 2.3 Synthetic Vision SkyView HDX Synthetic Vision feature is advisory in nature and must not be used as the sole means of terrain and obstacle avoidance. 2.4 Map The SkyView HDX Map and Flight Planning function is advisory in nature and must not be used as the sole means of terrain and obstacle avoidance. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 2-2 2.5 Autopilot Autopilot limitations for specific airplane makes/models are listed in separate appendices at the end of this document. For all airplanes equipped with the SkyView Autopilot system: • Use of the autopilot when any servo shear screw is broken is prohibited. • Use of the autopilot without a successful preflight operations check is prohibited. (See Section 4.5: Autopilot Operation Check for instructions) For airplanes equipped with the Yaw Damper function: • Use of the Yaw Damper function during takeoff and landing is prohibited. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 3-1 3 Emergency & Non-Normal Procedures 3.1 Emergency Procedures Airspeed, Altitude, and/or Attitude Unreliable CONDITION: Airspeed, Vertical Speed, and/or Altimeter indications are not consistent with Pitch Attitude. CHECK PITOT HEAT or CROSS CHECK ATTITUDE alert may be displayed. 1. Fly by reference to Standby Flight Display and Whiskey Compass. 2. Autopilot__________________________________________________ DISCONNECT. 3. Standby Flight Display____________________________________________ MONITOR. 4. Pitot Heat Switch_____________________________________________________ ON. 5. Alternate Static Air Source______________________________________________ ON. 6. Maneuver aircraft to avoid icing conditions. 7. Alternate Static Air Source no longer needed _______________________________ OFF. Autopilot / Yaw Damper Disable CONDITION: One or more autopilot servos are operating in a confusing or un-commanded fashion. 1. AP Power Switch____________________________________________________ OFF. 2. Fly Manually. • Power has been removed from the Autopilot servos. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 3-2 Autopilot / Yaw Damper Servo Jam CONDITION: One or more flight controls fail to move as expected and are jammed by an autopilot servo. 1. Autopilot__________________________________________________ DISCONNECT. 2. Flight Controls_________________________________ APPLY BREAK-AWAY FORCE. 3. Flight Controls_________________________________________________ OPERATE. 4. AP POWER Switch__________________________________________________ OFF. 5. Plan to land at nearest suitable airport. • When pilot applies force to flight control system, shear screw will break and safely disconnect flight controls from malfunctioning Autopilot servo. • Once shear screw breaks, pilot needs to relax flight control input to avoid over correction. The flight controls will then operate normally. • Autopilot operation is prohibited until the cause of the malfunction has been determined and corrected. Trim Runaway CONDITION: TRIM RUNAWAY alert is displayed. 1. AP DISC Button__________________________________________ PRESS AND HOLD. 2. TRIM POWER Switch_________________________________________________ OFF. 3. Mechanical Pitch Trim____________________________________ MOVE AS NEEDED. 4. Fly Manually. • In the event of a trim runaway event the pilot should be prepared to apply significant forces to the flight controls upon autopilot disconnect. The autopilot can mask out-of- trim conditions associated with a trim runaway. • Power has been removed from the Trim motor. • DO NOT use electric Trim system until cause of malfunction has been determined and corrected. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 3-3 3.2 Non-Normal Procedures Loss of Airspeed, Altitude, Attitude, and/or Heading Display CONDITION: Red X replaces the airspeed, altitude, attitude and/or heading indicators. If autopilot is engaged, "AUTOPILOT DISCONNECT" alert is annunciated. 1. Fly by reference to Standby Flight Display and Whiskey Compass. 2. Autopilot__________________________________________________ DISCONNECT. 3. Standby Flight Display___________________________________________ MONITOR. 4. Aircraft Attitude_____________________ MAINTAIN / REGAIN AIRCRAFT CONTROL. 5. Plan to land at nearest suitable airport. Loss of Electrical Power CONDITION: AIRCRAFT POWER LOST message is displayed, and the Main Menu indicates STAY ON and POWER OFF. 1. STAY ON Button __________________________________________________ PRESS. 2. Plan to land at nearest suitable airport. • The system is operating on the Backup Battery. • The system will continue to operate normally until the Backup Battery is depleted. • There is no indicator for Backup Battery power or time remaining. A fully charged Backup Battery provides 45 minutes of operation at a minimum. Engine Monitoring System Failure CONDITION: Red X replaces all engine and fuel indications. 1. Control engine power by sound and control lever position. Monitor engine performance using airspeed and vertical speed. 2. Plan to land at nearest suitable airport. GPS # Fail CONDITION: GPS # FAIL alert is displayed. ("#" being the configured GPS source (1, 2, 3, etc.)). • The GPS position source has failed. • The system is operating on the next available GPS position source. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 3-4 GPS Position Source # Fail CONDITION: POSITION SOURCE # FAIL alert is displayed. ("#" being the configured position source (1, 2, 3, etc.)). 1. Use other navigational means. • The system has no remaining GPS position sources available. • The Map is no longer available. Autopilot Disconnect CONDITION: The autopilot needs to be disconnected for any reason. 1. Disconnect Autopilot: • Press and release AP DISC Button (either yoke- or panel-mounted). –OR– • Press AP Button on the Autopilot Control Panel. –OR– • Press the AP Button on the Autopilot Control Menu. –OR– • Turn AP POWER switch/breaker OFF. 2. Fly manually. Yaw Damper Disconnect CONDITION: The yaw damper needs to be disconnected for any reason. 1. Disconnect Yaw Damper: • Press and release AP DISC Button (either yoke- or panel-mounted). –OR– • Press the YD Button on the Autopilot Control Menu. 2. Fly manually. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-1 4 Normal Operations 4.1 General Although operation of the primary functions of the SkyView HDX system is intuitive, it does require a reasonable degree of familiarity to utilize all its functions without compromising attention to other flying tasks. Users are encouraged to read the SkyView Pilot's User Guide thoroughly before flight and to take advantage of the training videos available on youtube.com/DynonAvionics. Knobs and Buttons Knobs are located on the left and right sides of the display. They can be rotated both directions and pushed. The current knob function is indicated by the "soft" label above the knob. Knob function is contextual and can change when the contents of the screen are changed by the pilot (see Figure 1). Eight buttons are located across the bottom of each display. The area immediately above the buttons is the Main Menu, which shows "soft" labels that identify the function of each button. Buttons have different functions depending on the information being shown on the display. The labels for each button on the Main Menu will change accordingly (see Figure 1). Figure 1: SkyView HDX Hardware Controls SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-2 Touch Controls SkyView HDX displays contain touchscreen functionality. Touching various items on the display allows for the item to be selected and the value adjusted. For example, touching the HSI data source allows for alternate sources to be selected. Pilot-selectable choices for the layout of each screen can be selected by pressing DISPLAY button on Main Menu. This allows the pilot to choose whether a display should show PFD, Map, or Engine information, or some combination thereof. See Figure 2 for details for the touchable screen areas of main flight functions. Additionally, the Timer function has touchscreen control, and if a compatible NAV device is connected, the Course (CRS) functions as well. Figure 2: HDX Touch Controls Synthetic Vision Synthetic Vision can be turned on or off by pressing the MENU button on the Main Menu, touching the PFD TOOLS screen icon, and then touching the SYNVIS screen icon. A green highlight on the SYNVIS icon means it is turned on. No highlight means it is turned off. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-3 HSI Data Source To cycle through the available sources of navigation data for display on HSI: • Press MENU button on Main Menu, then select PFD TOOLS > HSI SRC. Repeated touches of HSI SRC will cycle through available HSI data sources. Or, • Touch HSI SRC area near lower right corner of the PFD and beneath the Altimeter. Repeated touches of HSI SRC area will cycle through available HSI data sources. Adjusting Values and Bugs To adjust bug values using the left knob: 1. Touch applicable area on screen (see Figure 2). The function is shown and highlighted above knob. 2. Rotate left knob as needed to set value. Or, 1. Push left knob to enter Knob Function Menu. 2. Rotate knob as needed to set value. 3. Push left knob to close menu (menu will also close automatically after 5 seconds). This assigns function to knob. 4. Rotate knob as needed to set value. The value is shown and highlighted on screen. If a function is not present in the Knob Function Menu, then it does not have a touchable screen area and cannot be assigned to the left knob. To add or remove bugs to/from the Knob Function Menu, go to MENU > PFD TOOLS > BUGS. BARO Setting The Barometer setting can be adjusted with the left knob on the display or the BARO knob on the optional Knob Control Panel (see Section 4.1.12). Using the knob on the control panel simplifies the adjustment by eliminating the need to assign the function to the left knob. To change the Barometer setting: 1. Push left knob to enter Knob Function Menu. 2. Rotate knob to highlight BARO. 3. Push knob to close menu (menu will also close automatically after 5 seconds). This assigns BARO Bug to knob, and BARO is shown above knob. The Barometer area on the PFD is also outlined to show that it is selected. 4. Rotate knob to adjust Barometer setting. While Barometer setting is changing, screen area is highlighted in Cyan to draw attention to it. 5. To synchronize Altimeter with the Barometer settings in Table 1, push and hold BARO knob (on display or control panel) until a SYNC message appears on PFD. The following occurs: ▪ Altimeter is set to the nearest METAR (when ADS-B is available in-flight). SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-4 ▪ Standard pressure is set (29.92 inHg or 1013 millibars when at/above 18k feet or no ADS-B on board). ▪ Altimeter is set to match the published airport elevation (when on the ground). ▪ Altimeter is set to match GPS altitude (when on the ground). If none of the conditions in Table 1 are met, the Altimeter will not synchronize, and a NO SYNC message appears on the PFD. Table 1: BARO Settings With SV-ADSB-472 Installed Without SV-ADSB-472 Installed On the Ground: Adjusts the altimeter based on the current GPS Altitude. After the (BARO) is synchronized a GPSALT message will appear in the altimeter box on the PFD. In the Air: Adjusts the altimeter based on the METAR of the flight plan's destination airport if within 20nm. If there is no flight plan waypoint or it is too far away, then the altimeter is set to the nearest ADS-B METAR within 100nm with a valid altimeter setting. After the (BARO) is synchronized a SYNC message will appear in a window above the knob and the airport identifier will appear in the altimeter box on the PFD. Adjusts the altimeter to the standard pressure setting (i.e., 29.92 in Hg, 1013 mbar, or 760 mm Hg) Above 18,000 ft indicated altitude Resets the altimeter to standard pressure altitude for use in the flight levels (i.e., 29.92 in Hg, 1013 mbar, or 760 mm Hg). Altitude Bug The Altimeter can be adjusted with the left knob on the display or the ALT knob on the optional Knob Control Panel (see Section 4.1.12). Using the knob on the control panel simplifies the adjustment by eliminating the need to assign the function to the left knob. To change the Altitude bug: 1. Push left knob to enter the Knob Function Menu. 2. Rotate knob to highlight ALT. 3. Push knob to close menu (menu will also close automatically after 5 seconds). This assigns ALT to knob, and ALT is shown above knob. The Altimeter area on the PFD is also outlined to show that it is selected. 4. Rotate knob to adjust ALT bug. While ALT bug is changing, screen area is highlighted in Cyan to draw attention to it. 5. To synchronize Altimeter to airplane's current altitude, push and hold ALT knob (on display and control panel) until SYNC message appears above left knob on display. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-5 Minimum Altitude Bug To set the Minimum Altitude bug: 1. Push left knob to enter Knob Function Menu. 2. Rotate knob to highlight MIN. 3. Push knob to close menu (menu will also close automatically after 5 seconds). This assigns MIN to knob, and MIN is shown above knob. The Minimum Altimeter area on the PFD is also outlined to show that it is selected. 4. Rotate knob to adjust MIN bug. While MIN bug is changing, screen area is highlighted in Cyan to draw attention to it. HDG/TRK Bug Heading/Track can be adjusted with the left knob on the display or the HDG/TRK knob on the optional Knob Control Panel (see Section 4.1.12). Using the knob on the control panel simplifies the adjustment by eliminating the need to assign the function to the left knob. To set the Heading/Track bug: 1. Press left knob to enter Knob Function Menu. 2. Rotate knob to highlight HDG or TRK. 3. Push knob to close menu (menu will also close automatically after 5 seconds). This assigns HDG or TRK to knob, and HDG or TRK is shown above knob. The Heading or Track area on the PFD is also outlined to show that it is selected. 4. Rotate knob to adjust HDG or TRK bug. While HDG or TRK bug is changing, screen area is highlighted in Cyan to draw attention to it. 5. To synchronize Heading and Track to airplane's current heading/track, push and hold HDG/TRK knobs (on display or control panel) until SYNC message appears above left knob on display. Course (OBS) Setting To set the HSI course (OBS): 1. Press left knob to enter Knob Function Menu. 2. Rotate knob to highlight CRS. 3. Push knob to close menu (menu will also close automatically after 5 seconds). This assigns CRS to knob, and CRS is shown above knob. The HSI course area on the PFD is also outlined to show that it is selected. 4. Rotate knob to adjust CRS setting. While CRS setting is changing, screen area is highlighted in Cyan to draw attention to it. The CRS value for each available HSI source is retained when that source is deselected and will be used when that HSI source is re-selected. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-6 G Meter When triggered or enabled by the pilot, the G Meter replaces the HSI on the PFD (see Figure 3). The G Meter has an analog needle that indicates the G loading of the aircraft. Digital G information is also instantaneously shown in the center of the gauge. Depending on how the G Meter is configured, the analog range may have yellow and/or red ranges to indicate that the aircraft’s G limits are being approached. The numerical magnetic heading above the HSI area remains displayed when the G Meter is displayed. The G Meter is automatically displayed when the aircraft’s G loading reaches the yellow threshold configured during initial system setup. (See the 103261-000 SkyView HDX System Installation Manual document for more information). If the G Meter was automatically displayed, it will be removed when the aircraft’s G loading returns to normal range, and the HSI will be restored. Pilots can also choose to display the G Meter at any time by selecting MENU (Button #6) > PFD TOOLS icon > G METER icon. The G METER icon toggles the indicator on/off. The smaller digital numbers above and below the Digital G information are the maximum (top) and minimum (bottom) Gs that the aircraft has experienced since the G Meter was last reset. These can be reset at any time by selecting MENU (Button #6) > PFD TOOLS icon > RESET G icon. Figure 3: Example of G Meter Being Displayed SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-7 Knob Control Panel The Knob Control Panel (see Figure 4) is an optional panel-mounted module for SkyView. This control panel has three knobs dedicated to the most common SkyView bug functions – ALT, BARO, and HDG/TRK. This module is particularly useful in systems with the SkyView Autopilot installed because it directly controls the bugs that allow the selection of Altitude (ALT), Heading (HDG) or Track (TRK), and Barometric Setting (BARO). Rotating the knob change the value of the associated bug. Pushing and holding the ALT and HDG/TRK knobs synchronizes the bugs with current values. Pushing and holding the BARO knob sets the Altimeter to match the GPS altitude, standard pressure if above 18,000 feet, or (if SV-ADSB-472 is installed), the nearest appropriate METAR station. Figure 4: Knob Control Panel (Horizontal and Vertical Configurations) VHF COM Radio The optional COM Radio Control Panel (see Figure 5) tunes frequencies by airport and station type and allows the simultaneous reception of two frequencies, referred to as Dual Mode. To use the radio: 1. Press the APT button and use the knob to scroll through nearby airports. 2. Press the knob to select an airport. 3. TWR, ATIS, GND, and ATC will now select appropriate frequencies for the selected airport. 4. Press the knob to toggle the selected active and standby frequencies. 5. Press and hold the knob to monitor both active and standby frequencies (i.e., Dual Mode). The active frequency will have priority. 6. To exit Dual Mode, push and hold the knob again, or press DUAL on the Radio Menu. 7. Adjust frequencies with the labeled buttons or manually with the dual concentric knob. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-8 Figure 5: COM Control Panel (Horizontal and Vertical Configurations) 4.2 SkyView HDX Backup Power Check When the SkyView HDX system detects that it is not moving, and power is removed from a display connected to a backup battery, the system will automatically run an additional 30 seconds on backup battery power. This is so it can complete a battery condition test. The result of the test will appear in the battery status indicator at next system startup. The battery icon is displayed next to the clock to indicate battery status: • No icon: Last battery check was satisfactory. • Yellow battery icon: ▪ The manual battery test has not been accomplished within the last 365 days. Refer to the SkyView installation manual for instructions on performing the manual battery test. ▪ The automatic condition test failed during the last three attempts. Perform the manual battery test according to the SkyView installation manual. • Red X battery icon: battery check or annual test failed, or the battery is not connected IFR flight with a yellow or red back up battery status indicator displayed is prohibited. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-9 4.3 Standby Flight Display Backup Battery Condition Check The charge on the EFIS-D10A or D30 backup battery needs to be checked prior to IFR flight. To check the charge on the EFIS-D10A backup battery: 1. Enter menu system by pressing any button (except far left and right buttons) on an EFIS page, and then press EFIS > MORE > INFO > LEFT > VMETER. 2. Make sure backup battery is charged to at least 16.0 volts. To check the charge on the D30 backup battery: Refer to the D30 Airplane Flight Manual Supplement document at dynoncertified.com/docs. 4.4 Autopilot Controls This section covers the primary means of operating the optional SkyView Autopilot. Additional methods and shortcuts can be found in the Pilot’s User Guide. The primary means of controlling the autopilot is via the Autopilot Control Menu (see Figure 41). • On the HDX primary page, press MENU, then AUTOPILOT to display the Autopilot Control Menu. • Or touch the Autopilot Mode Display to enter the Autopilot Control Menu. In the Autopilot Control Menu: • A green bar indicates the function is active. • A white bar indicates the function is armed. • A black bar indicates the function is off or not selected. • Gray button labels indicate the mode is not available (e.g., gray NAV indicates no valid NAV source). • HSI source color indicates the type of source. Magenta indicates a GPS-based source; Green indicates a radio-based source (VOR or localizer). The optional Autopilot Control Panel (see Figure 6) for the SkyView Autopilot provides dedicated buttons for engaging the Flight Director, autopilot, and all control modes, including coupled approaches, VNAV, IAS Hold, and mode sequencing (provided that IFR navigation sources are installed). It also has a Level button to immediately return the airplane to straight and level flight. The "ALT" and "SRC" buttons on the control panel are abbreviations for "ALT HOLD" and "HSI SRC" in the Autopilot menu. The control panel buttons are illuminated for low-light visibility, but do not indicate autopilot operation status. Use the autopilot mode display and/or the autopilot menu to determine autopilot operation status. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-10 Figure 6: SV-AP-PANEL (Horizontal and Vertical Configurations) Engage Autopilot Press the AP button to engage the servos. The Flight Director is automatically engaged. SkyView Auto-trim is also automatically engaged if the airplane is equipped with an electric trim system and an SV-AP-TRIMAMP Trim Motor Adapter is installed. If an AP mode or modes have been preselected, that mode will become active when the AP button is pressed, and the servos will engage. See below to pre-select an AP mode. If no mode has been selected, the Autopilot will turn on and engage the servos in Roll Hold mode and Vertical Speed mode with the targets set to the current aircraft roll attitude and vertical speed. Different modes may then be selected. Normally, the Autopilot will not engage if airspeed is outside the normal speed range configured by the installer during initial system setup. The only exception is LEVEL Mode, which will engage at any speed. Disengage Autopilot The Autopilot is disengaged by the following: • Pressing "AP" button on the Autopilot Control Panel (see Figure 6). • Pressing "AP" button on the Autopilot Control Menu (see Figure 41). • Pressing AP DISC button (see Section 4.4.3 below): ▪ Press button once to disengage the autopilot servos but leave Modes and Flight Director active. ▪ Press button twice (i.e., double-click) to disengage the autopilot servos and cancel all Modes and Flight Director. • Turning AP POWER switch/breaker OFF (see Section 4.4.4 below). SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-11 AP DISC (Autopilot Disconnect) Button SkyView HDX systems with SkyView Autopilot will have a button labeled, AP DISC, mounted either on the wheel/yoke or prominently on the instrument panel. This button, when pressed, will immediately disengage the autopilot. If the SkyView Auto-trim feature is installed, it will also temporarily interrupt power to the trim motor(s). If the SkyView Auto-trim feature is installed, releasing the AP DISC button restores power to the trim motor(s). To permanently disable electric trim, turn the TRIM POWER switch OFF. Where the AP DISC button is mounted depends upon the autopilot installation: • If the SkyView Auto-trim feature is installed, the AP DISC button will be on the yoke/wheel grip, opposite the throttle control. • If the airplane does not have SkyView Auto-trim, the AP DISC button will be on either the yoke/wheel grip or prominently on the instrument panel. AP POWER Switch SkyView HDX systems with SkyView Autopilot will have a switch/breaker labeled AP POWER that is mounted prominently on the instrument or circuit breaker panel. This switch/breaker, when turned OFF, immediately removes power from all autopilot servos. TRIM POWER Switch SkyView HDX systems with SkyView Auto-trim will have a switch/breaker labeled TRIM POWER that is mounted prominently on the instrument or circuit breaker panel. This switch/breaker, when turned OFF, immediately removes power from all electric trim motors. Engage Flight Director The Flight Director is engaged by pressing the "FD" button instead of the "AP" button. To subsequently engage the servos, press the "AP" button. Level Mode Press the LEVEL button on the panel to engage Level Mode. Level Mode can be selected at any time, even if Autopilot is disconnected. The level function cannot guarantee recovery below VNE in all starting attitudes due to G limiting and servo effort limiting. Recoveries have only been demonstrated from 45 degrees of bank and 10 degrees nose down pitch. Climb or Descend to a New Altitude at a Set Vertical Speed 1. Adjust the altitude bug to the new desired altitude. 2. Press the VS button. If ALT HOLD is currently engaged VS bug will be set to zero. If no vertical mode is currently engaged, the VS bug will synchronize with the current vertical speed. 3. Adjust the vertical speed bug using the NOSE UP / DN buttons. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-12 In ALT HOLD mode, the NOSE UP / NOSE DOWN buttons may be used to command a vertical speed transition without pressing the VS button. The initial press of NOSE UP/DN selects the default vertical speed of 500 fpm in the desired direction. The AP limits airspeed to a safe value if the commanded vertical speed would over- speed or under-speed the aircraft. 4. ALT capture is automatically armed. 5. Engage the servos if not already engaged by pressing the AP button. ALT capture is automatically activated as the airplane approaches the target altitude. Climb or Descend to a New Altitude at a Set Airspeed 1. Adjust the altitude bug to the new desired altitude. 2. Press the IAS button. The IAS bug will synchronize to the current airspeed. 3. NOSE UP / DN buttons to adjust the Autopilot’s target airspeed. Airspeed command is limited to the Autopilot minimum and maximum limits configured by the installer during initial system setup. 4. ALT capture is automatically armed. 5. Engage the servos if not already engaged by pressing the AP button. ALT capture is automatically activated as the airplane approaches the target altitude. Go Around The Go Around function is available when the Autopilot is engaged in vertical guidance and is tracking a vertical deviation (i.e., status bar shows "VNAV" or "GS" as the active mode). To engage the Go Around function, press the NOSE UP button on the AP Control panel. Pressing Go Around (NOSE UP) at any time automatically switches Pitch and Roll Modes to: 1. TRK Mode, with value defaulting to the current GPS track, and 2. One of the following, depending upon how owner/pilot configured system in Autopilot Setup menu: • VS Mode defaulting to the default climb rate, or • IAS Mode, defaulting to the current airspeed The need for airplane trim changes during the go-around may cause the autopilot servos to slip. The pilot must adjust the pitch trim to prevent the pitch servo from slipping. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-13 HDG and TRK Hold 1. Adjust the HDG/TRK bug to the desired value. 2. Select HDG to follow a magnetic heading equal to the bug value. 3. Select TRK to follow a GPS referenced ground track equal to the bug value. 4. Engage the servos if not already engaged. Enroute Lateral Navigation - VOR or GPS This procedure is identical whether you are tracking using an enroute navigation source (GPS or VOR) or a non-precision approach (GPS, VOR or LOC). 1. Select a navigation source on the HSI (MENU > AUTOPILOT > HSI SRC). The navigation source must be providing valid course and deviation information. 2. Press the NAV button. If the CDI is already near-centered NAV mode will immediately become active. Otherwise, NAV mode will arm. If NAV mode is armed, adjust the current mode’s target (heading, track, or roll) to establish the desired intercept with the navigation source. NAV mode will become active once the navigation source CDI can be captured by the autopilot. Approaches 1. While navigating on a course intercepting the approach course, select a navigation source on the on the HSI (MENU > AUTOPILOT > HSI SRC). 2. If appropriate, tune and identify the station and set the OBS appropriately via the CRS setting. The external navigation source must be providing valid course and deviation information. 3. When cleared for the approach: a. Press the NAV button in the Roll Menu to arm the NAV mode. b. Press the VNAV button in the Pitch Menu to arm VNAV mode. NAV and VNAV modes arm and activate independently from each other. There is no limitation upon the order the modes can be armed or activated. Autopilot pitch authority may be exceeded when lowering the flaps. Trim appropriately during changes in flap settings. If a precision GPS approach is being flown with an approach approved GPS navigator and the autopilot is already in NAV mode (i.e. not flying vectors to final) arming of NAV mode is not necessary. Only VNAV will need to be armed when cleared for the approach. VNAV mode will only capture vertical approach guidance from below. Plan your glide slope or a glide path capture accordingly. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-14 If an ILS approach is being flown with another navigation source being used in the transition, for example an approach approved GPS navigator, upon being cleared for and activating the approach the SkyView HDX's HSI source must be switched from GPS to NAV. This may happen one of two ways: 1. If the GPS Navigator does not support auto-switching from GPS to NAV, you must manually perform this action by using AUTOPILOT > HSI SRC. 2. Some devices, such as the Garmin 430, 430W, and GTN series, can automatically change from the GPS to the localizer and send a signal to the SkyView to automatically change the HSI source at the appropriate time. If the external GPS/NAV device is configured with this behavior enabled, one important detail is that such devices ALWAYS control whether its GPS or NAV radio is providing guidance. Thus, when configured for auto-switching, you must use that navigators’ CDI or NAV/GPS toggle to change whether NAV or GPS guidance is shown on SkyView HDX’s HSI. SkyView HDX’s own HSI SRC button can only see EITHER the GPS or NAV side of the navigator at any time. 4.5 Autopilot Operation Check Perform the following on the ground (i.e., during a pre-flight inspection) to test the functionality of the optional SkyView Autopilot. Pitch and Roll Axis Operation Check With master switch and autopilot servo power switches ON: 1. Center flight control yoke, and lightly hold in place. The weight of an unbalanced elevator may cause the servo to slip. Lightly hold the controls in the centered position when operating the autopilot on the ground to offset this effect. 2. Align HDG/TRK bug with current heading. 3. Select ALT and HDG. 4. Engage Autopilot. 5. Set Vertical Speed +1000. 6. Set Altitude 1000 feet above current. Feel yoke move in "Nose Up" direction. 7. Press and hold ALT button to return altitude bug to current. Feel yoke move to neutral. 8. Change HDG/TRK bug to right of current heading. Feel yoke move in "Right Roll" direction. 9. Change HDG/TRK bug to left of current heading. Feel yoke move in "Left Roll" direction. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 4-15 Yaw Axis Operation Check If the autopilot is a two-axis (pitch and roll) control system, do not perform the following check. Autopilot systems without a Yaw Damper will not have Yaw Damper (YD) controls in the Autopilot Control Menu (see Figure 41). With master switch and autopilot servo power switches ON: 1. Move rudder pedals left and right to feel operation. 2. Center rudder pedals, and lightly hold in place. 3. Engage Yaw Damper. 4. Move rudder pedals to the left. Rudder pedals should encounter some resistance to movement; the servo may slip. 5. Move rudder pedals to the right. Rudder pedals should encounter some resistance to movement; the servo may slip. 6. Disconnect Yaw Damper. 7. Move rudder pedals left and right to feel operation. Resistance should not occur. The resistance offered by the servo indicates that the system is operating normally. Autopilot Disconnect Check With master switch and autopilot servo power switches ON: 1. Engage Autopilot. 2. Accomplish all that apply: • Press the AP button in the Autopilot Control menu, and ensure the autopilot disconnects. "AUTOPILOT DISCONNECT" aural should be heard. • Turn the AP Servo Power switch to OFF, and ensure the autopilot disconnects. "AUTOPILOT DISCONNECT" aural should be heard. • Press the AP button on the Autopilot Control Panel (if installed), and ensure the autopilot disconnects. "AUTOPILOT DISCONNECT" aural should be heard. • Press the panel mounted disconnect button (if installed), and ensure the autopilot disconnects. "AUTOPILOT DISCONNECT" aural should be heard. • Press the yoke mounted disconnect button (if installed), and ensure the autopilot disconnects. "AUTOPILOT DISCONNECT" aural should be heard. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 5-1 5 Performance Use of the SkyView HDX system has no effect on the airplane's performance. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 6-1 6 Weight and Balance Installation of a SkyView HDX system impacts the airplane's level weight and balance once, during initial installation. Certified installers must add new empty weight and balance information to airplane's Aircraft Flight Manual. Refer to the airplane's Pilot's Operating Handbook and associated Aircraft Flight Manual and supplements. Pilots manage loading weight and balance according to the Aircraft Flight Manual. SkyView HDX has no impact on operational loading. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-1 7 System Overview 7.1 SkyView HDX Display Units The SkyView HDX display unit installed in the pilot's position is designated the Primary Display. It is configured during initial setup to always present PFD. It can also present Map and Engine Monitoring. Additional installed display units (referred to as Secondary Displays) have no PFD restrictions and can present any combination of PFD, Map, or Engine Monitoring. A Secondary Display may also function as a backup should the Primary Display fail. Primary Displays and Secondary Displays share attitude, air data and engine data. However, SkyView HDX systems include a Standby Display to provide instant attitude and air data. The standby display is a separate system from the SkyView HDX system. 7.2 Standby Display System SkyView HDX-equipped airplanes always include a Standby Display that provides a display screen and an ADAHRS in a single component with a back-up battery to present attitude, altitude, and airspeed information. The approved Standby Display for the SkyView HDX system. is either the Dynon EFIS-D10A or Dynon D30. (If your aircraft is equipped with a D30, see the D30 Airplane Flight Manual Supplement document at dynoncertified.com/docs). 7.3 Synthetic Vision SkyView HDX provides a synthetic vision representation of the local terrain and obstacles. This display is for advisory purposes only and must not be used as the sole means of avoidance. 7.4 Map SkyView HDX can present a Map to display airport, airspace, obstacle, and other available aviation data using navigation databases (FAA Obstacle/Terrain and Airport) databases and GPS-derived airplane position data. The Map can also be used for flight planning and plot navigational course guidance. The Map is for advisory purposes only and must not be used as a sole means of avoidance, nor is it an IFR-approved navigation source. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-2 7.5 Terrain Alerts Terrain clearance alerts are provided based on the predicted path of the airplane relative to the terrain database and the proximity of the aircraft to terrain. The synthetic vision alert is based both on altitude and on flight path. Terrain shown in red is an immediate threat to the aircraft. The map alert is based solely on GPS altitude. • Yellow terrain is between 100 and 1000 feet below aircraft GPS altitude. • Red terrain is above the aircraft, or 100 feet or less below the aircraft. Terrain advisories are configured per pilot preference during initial system setup, and they are enabled from the MENU under MAP LAYERS. When enabled, terrain alerts are suppressed prior to takeoff and are enabled approximately 200 feet above the takeoff altitude. Terrain alerts are provided any time they are enabled, even if topographical relief is not shown on the map. 7.6 Traffic Information SkyView HDX can display traffic information on the PFD and on the Map. The presentation of traffic information is for advisory purposes only and must not be used as a sole means of avoidance. The display of traffic information is enabled and configured during initial system setup by installers per aircraft owner/operator request and preference. Figure 7: Example of Traffic Displayed on Map SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-3 Traffic Targets Traffic targets are presented with symbols and information commonly used in aviation for traffic/TCAS systems. SkyView HDX can display up to 8 targets simultaneously. If there are more than 8 potential threats, the TIS ground station determines the highest priority targets. Figure 8: Example of a Traffic Target A traffic target includes the following: • A symbol that depicts the type of traffic target: Traffic Advisory (TA) target, Proximity Advisory target, or Non-threat target. See Section 7.6.2 for more information. • Relative altitude in hundreds of feet. This is displayed above the target symbol as a signed integer. In Figure 8, the target is +14, or 1400 feet higher than your aircraft. This area is blank if the altitude of a target is not known. • An up or down arrow to the right of the target symbol that indicates whether the target aircraft is climbing or descending. • Depending upon target aircraft equipment, an orange vector arrow that points in the target aircraft’s direction of travel. The length of arrow represents where the aircraft is expected to be in one minute based on its current trajectory. SkyView HDX assumes that all TIS targets are travelling at 150 knots. The target’s direction is shown to the nearest 45° increment (0°, 45°, 90°, etc.). • Depending upon target aircraft equipment, the aircraft’s tail number will be shown below target symbol. Target Symbols This section describes the types and significance of the symbols that SkyView HDX displays on the PFD and Map for traffic targets. Traffic Advisory (TA) Targets: These targets have a high chance of ending up near the aircraft. They often start as lower priority targets and become TA targets as they approach. SkyView HDX considers an aircraft a threat if the traffic device in the target aircraft is reporting that it is a threat. TIS reports a threat if a target aircraft is within a 1/4 mile of your aircraft and converging within 30 seconds. This calculation is 20 seconds if the target aircraft is not reporting altitude. ADS-B reports also use a 20 second calculation. Figure 9: TA Target Symbol (On-screen) Figure 10: TA Target Symbols (Off-screen) SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-4 If a TA target cannot be displayed on the screen because its location is beyond the edge of the Map at its current range, it will appear at the edge of the Map with shading, as shown in Figure 10. The shaded area of the symbol always points towards the edge of the screen. This provides threat awareness regardless of Map range level. Proximity Advisory and Non-Threat Targets: Proximity Advisory targets have less of a chance of being a factor based on their position. They are not considered TA targets because they are not converging with your aircraft within the next 30 seconds. A Proximity Advisory target is shown on the Map when it is closer than 5 nm and within +/- 1200 ft. of your altitude but does not meet the criteria to trigger a TA alert. Non-threat targets are any other detectable aircraft that are neither TA targets nor Proximity Advisory targets. Figure 11: Proximity Advisory Target Figure 12: Non-Threat Target Traffic Alerts "Traffic" is an aural and visual caution alert that notifies pilots that there are Traffic Advisory (TA) targets present. The visual notification is shown on the PFD (near Airspeed tape) and on the Map (lower right corner), as shown in Figure 13. Figure 13: Traffic Alert Notification SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-5 7.7 Weather Information SkyView HDX can display weather information on the Map, including lightning and PIREPS. Display of traffic information is for advisory purposes only and must not be used as a sole means of avoidance. The display of weather information is enabled from the IN-FLIGHT MENU under WEATHER OPTIONS. 7.8 Navigation Databases SkyView HDX uses a variety of databases containing navigation and obstacle related information. Depending on the database, these may be updated as frequently as every month. SkyView components should be kept updated with the latest available databases. These may be downloaded to a USB flash drive in accordance with the instructions found at dynoncertified.com/data. 7.9 Operational Software Software is updated using a USB flash drive in accordance with the instructions in the SkyView HDX System Installation Manual document at dynoncertified.com/download. Updating the SkyView software will automatically update all components connected to the SkyView Network as appropriate. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-6 7.10 Flight Crew Alerting System The Flight Crew Alerting System is a central feature of the SkyView HDX system. This system provides the pilot and crew with system information organized by condition priority for all installed SkyView components. The alerts and messages will vary depending upon the installed equipment. This section describes all possible alerts and messages. System information is delivered in the form of flight crew alerts and messages that are organized by severity into one of three categories: 1. Warning Alerts: Warning alerts are for conditions that require immediate flight crew awareness and immediate flight crew response. Most warning alerts are displayed in the Alert Notification Window (see Figure 15) and are identified with Red and have both visual and aural annunciations. Some warning alerts (see Table 2) are aural only when the display already presents a related indication. If a warning alert is flightpath or autopilot related, its visual annunciation is displayed directly on the PFD or on/near the AP Info Bar. 2. Caution Alerts: Caution alerts are for conditions that require immediate flight crew awareness and subsequent flight crew response. Most caution alerts are displayed in the Alert Notification Window (see Figure 15) and are identified with Yellow and have both visual and aural annunciations. Some caution alerts (see Table 3) are aural only when the display already presents a related indication. If a caution alert is flightpath or autopilot related, its visual annunciation is displayed directly on the PFD and Map or on/near the AP Info Bar. 3. Messages Messages are for conditions that require immediate flight crew awareness and may require subsequent flight crew response. Most messages are displayed in the Alert Notification Window (see Figure 15) and are identified with Grayscale and have both visual and aural annunciations. Some messages (see Table 4) are aural only when the display already presents a related indication. If a message is flightpath or autopilot related, its visual annunciation is displayed directly on the PFD or on/near the AP Info Bar. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-7 Notification Methods Whenever a new non-flightpath alert is triggered, the Alert Notification Indicator (i.e., button label) shown in Figure 14, flashes Red for Warning alerts, Yellow for Caution alerts, and Gray for Messages. A corresponding voice aural annunciates a spoken word such as "WARNING", "CAUTION" or "MESSAGE" depending on the alert type. Some alerts and messages will annunciate the actual name, such as "OIL PRESSURE", or "AUTOPILOT DISCONNECT". Figure 14: Warning Notification Indication Pressing the WARNING, CAUTION, or MESSAGE button (i.e., Button #8) opens the Alert Notification Window. This window displays text associated with each active alert. After pressing the button, the alerts present in the window are considered acknowledged and the indicator stops flashing. The indicator color corresponds with highest alert level that is currently being triggered. Individual alerts may be configured by the installer to require acknowledgement after they have been triggered for the alert to disappear. The appearance of alerts within the Alert Notification Window change when first triggered and after acknowledgement. The difference between an un-acknowledged and acknowledged message is shown in Figure 15. This difference is consistent with all alerts, regardless of color. When no alerts are active, the Alert Indicator states, "NO MSG". When the Alert Notification Window is open, the displayed information is frozen and does not change. If a new alert or message is triggered or cleared, the pilot must re- open the window to refresh the information. Figure 15: Alert Notification Window, Alert Appearance SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-8 Warning Alerts Table 2 lists all SkyView system warning alerts alphabetically by 1) visual and 2) aural annunciation. Alerts are dependent upon installed systems and components. Table 2: Warning Alert Conditions and Associated Crew Responses WARNING ALERTS VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION "WARNING" The calibration of the ADAHRS module is corrupt. Do not fly. Monitor Standby Display System. "WARNING" SkyView has detected a problem with the ADAHRS module. Do not fly. Monitor Standby Display System. "WARNING" System sensor tests performed on the ADAHRS module failed. Do not fly. Monitor Standby Display System. "ELECTRICAL CURRENT" Electrical current indicator has entered configured red high range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "ELECTRICAL CURRENT" Electrical current indicator has entered configured red low range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "WARNING" The ARINC-429 module is not communicating with the SkyView HDX display unit. Do not fly if flight requires external navigation sources. SkyView will not display navigation from external sources. Use internal source, or follow navigation information on external devices. "WARNING" The audio alert system has failed. AoA system not operating. Do not fly. Use visual alerts to monitor status. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-9 WARNING ALERTS VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION Near AP Info Bar: "AUTOPILOT AIRSPEED HIGH" The autopilot is applying nose up inputs to protect the airplane from exceeding the configured maximum autopilot airspeed. Visual annunciation appears immediately; aural after 10 seconds. No action. Take command to manually decrease airplane's speed. Near AP Info Bar: "AUTOPILOT AIRSPEED LOW" The autopilot is applying nose down inputs to protect the airplane from slowing below the configured autopilot minimum airspeed. Visual annunciation appears immediately; aural after 10 seconds. No action. Take command to manually increase airplane's speed. On AP Info Bar: Status bar changes color and temporarily flashes. "AUTOPILOT DISCONNECT" Both pitch and roll autopilot axes have been disconnected. No action. Take command to fly manually. On AP Info Bar: Status bar changes color and temporarily flashes. "AUTOPILOT PITCH DISCONNECT" The autopilot pitch axis has been disconnected. No action. Take command to fly manually. On AP Info Bar: Status bar changes color and temporarily flashes. "AUTOPILOT ROLL DISCONNECT" The autopilot roll axis has been disconnected. No action. Take command to fly manually. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-10 WARNING ALERTS VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION "WARNING" The backup battery connected to the SkyView HDX display unit is in use and has entered a low charge state. Do not fly if flight requires Instrument Flight Rules (IFR). Allow backup battery to fully charge before flight. Avoid operations in Instrument Meteorological Conditions (IMC). Land at nearest suitable airport. "VOLTAGE" Voltage indicator has entered configured red high range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "VOLTAGE" Voltage indicator has entered configured red low range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual On PFD: "WARNING" Airspeed is no longer available, or is unreliable. Do not fly. Refer to Section 3.1.1: Airspeed, Altitude, and/or Attitude Unreliable. "CYLINDER HEAD TEMPERATURE" CHT indicator for identified sensor has entered configured red high range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "CYLINDER HEAD TEMPERATURE" CHT indicator for identified sensor has entered configured red low range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual On PFD: "WARNING" Airspeed is no longer available, or is unreliable. All GPS sources have failed. Do not fly. Refer to Section 3.1.1: Airspeed, Altitude, and/or Attitude Unreliable. "WARNING" The SkyView HDX display unit is in Demo Mode and is not airworthy. Do not fly. Monitor Standby Display System. "EXHAUST GAS TEMPERATURE" EGT indicator for identified sensor has entered configured red high range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-11 WARNING ALERTS VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION "EXHAUST GAS TEMPERATURE" EGT indicator for identified sensor has entered configured red low range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "WARNING" The identified EMS module has failed. Do not fly. Use control position(s) and aural cues to operate engine(s). Visual indication varies by configuration. "ENGINE MONITOR" A system monitored by EMS and configured as a general purpose input has entered the configured red range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual No visual indication. "FLAPS OVERSPEED" The value configured for VFE has been exceeded with flaps extended. No action. Take command to manually decrease airplane's speed until the flaps have been fully retracted. "FUEL FLOW" Fuel flow indicator has entered configured red high range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "FUEL FLOW" Fuel flow indicator has entered configured red low range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "FUEL PRESSURE" Fuel pressure indicator has entered configured red high range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "FUEL PRESSURE" Fuel pressure indicator has entered configured red low range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-12 WARNING ALERTS VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION Near AP Info Bar: No aural indication. Autopilot is engaged and vertical acceleration has exceeded the 0.5G to 1.5G range. No action. Monitor autopilot performance. If airplane departs from intended flight path, disconnect autopilot and take command to fly manually. No visual indication. "GEAR OVERSPEED" The value configured for VLE has been exceeded with gear extended. No action. Take command to manually decrease airplane's speed until the landing gear has been fully retracted. "FUEL QUANTITY" Fuel quantity indicator has entered configured red high range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "FUEL QUANTITY" Fuel quantity indicator has entered configured red high range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "OIL PRESSURE" Oil pressure indicator has entered configured red high range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "OIL PRESSURE" Oil pressure indicator has entered configured red low range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "OIL TEMPERATURE" Oil temerature indicator has entered configured red high range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "OIL TEMPERATURE" Oil temerature indicator has entered configured red low range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-13 WARNING ALERTS VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION No visual indication. "OVER GEES" The G-Meter has entered the configured red range. No action. Reduce loads acting on airplane using pitch and power as appropriate. No visual indication. "OVERSPEED" The value configured for VNE has been exceeded. No action. Take command to manually decrease airplane's speed below VNE On right side of AP Info Bar: No aural indication. An internal servo error has occurred or ADAHRS data is unreliable. Turn autopilot power OFF. Autopilot is disabled and must not be used until issue has been corrected. Turn autopilot power OFF. Do not use autopilot for remainder of flight. On left side of AP Info Bar: No aural indication. An internal servo error has occurred or ADAHRS data is unreliable. Turn autopilot power OFF. Autopilot is disabled and must not be used until issue has been corrected. Turn autopilot power OFF. Do not use autopilot for remainder of flight. "ENGINE SPEED" Tachometer indicator has entered configured red high range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "ENGINE SPEED" Tachometer indicator has entered configured red low range. Refer to Airplane Flight Manual Refer to Airplane Flight Manual "WARNING" A fault has been detected in wiring that provides power to SkyView Network. Failure of Flight, Engine, and/or Navigation information may be imminent. Do not fly. Monitor Standby Display System. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-14 WARNING ALERTS VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION Near AP Info Bar: No aural indication. The autopilot has carried a large trim load for an extended period, and the affected servo is slipping. No action. Turn trim motor power OFF. Trim airplane using mechanical pitch trim control. Near AP Info Bar: No aural indication. The autopilot has carried a large trim load for an extended period, and the affected servo is slipping. No action. Turn trim motor power OFF. Trim airplane using mechanical pitch trim control. "WARNING" The trim feedback monitor received a positive activity signal during system boot. Do not fly. Electric trim system must not be used until fault has been corrected. 1) Turn trim motor power OFF. 2) Trim airplane manually. Electric trim system must not be used until fault has been corrected. On PFD: "TRIM RUNAWAY" SkyView detected electric trim motor activity that was not commanded. Do not fly. Electric trim system must not be used until fault has been corrected. Refer to Section 3.1.4: Trim Runaway. Electric trim system must not be used until fault has been corrected. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-15 Caution Alerts Table 3 lists all SkyView system caution alerts alphabetically by 1) visual and 2) aural annunciation. Alerts are dependent upon installed systems and components. Table 3: Caution Alert Conditions and Associated Crew Responses CAUTION ALERTS VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION "CAUTION" ADAHRS module has detected vibration that affects performance of G-Meter, attitude indicator, and autopilot. Do not fly. Cross check and monitor instruments. If autopilot is enagaged, disengage, and turn AP Power switch OFF. Do not use autopilot for remainder of flight. "CAUTION" Calibration of the ADAHRS module is out-of-date. Do not fly. Avoid operations in Instrument Meteorological Conditions (IMC). On PFD: "GO AROUND" The autopilot Go Around function has been engaged. No action. Set power for Go- Around. "CAUTION" The autopilot disconnect monitor has detected a wiring fault. Turn autopilot power OFF. Autopilot is disabled and must not be used until fault has been corrected. Turn autopilot power OFF. Do not use autopilot for remainder of flight. "CAUTION" The autopilot disconnect monitor has detected a wiring fault. Turn autopilot power OFF. Autopilot is disabled and must not be used until fault has been corrected. Turn autopilot power OFF. Do not use autopilot for remainder of flight. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-16 CAUTION ALERTS VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION "CAUTION" Autopilot Control Panel is not communicating with SkyView. Autopilot control panel unavailable. Use SkyView Control Menu. Trim airplane manually. Autopilot control panel unavailable. Use SkyView Control Menu. Trim airplane manually. "CAUTION" SkyView sent a command to move the trim motor, but did not receive feedback that the motor is moving. A trim switch was held ON continuously for more than 5 seconds while SkyView Auto- trim was enabled. 1) Turn trim motor power OFF. 2) Trim airplane manually. Electric trim system must not be used until fault has been corrected. 1) Turn trim motor power OFF. 2) Trim airplane manually. Electric trim system must not be used until fault has been corrected. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-17 CAUTION ALERTS VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION "CAUTION" The SkyView HDX display unit presenting the alert has switched to backup battery power. Do not fly. Choose one: a) Alert appears on all displays, and airplane Master Switch is OFF: Turn airplane Master Switch ON, Confirm message(s) stop. b) Alert appears on one display, and airplane Master Switch is ON: Affected display will operate for 45 minutes. Remaining displays continue to function normally. c) Alert appears on all displays, and airplane Master Switch is ON: Displays will operate for 45 minutes. Plan to land at nearest suitable airport. "CAUTION" The SkyView HDX display unit presenting the message no longer detects the backup battery. Do not fly Avoid operations in Instrument Meteorological Conditions (IMC). "CAUTION" Backup battery test did not pass. Perform succsessful backup battery test prior to flight. N/A No visual indication. "CHECK GEAR" Gear is not DOWN, and airspeed is below configured Landing Gear Check Speed. Not Applicable. Confirm correct landing gear position. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-18 CAUTION ALERTS VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION "CAUTION" The SkyView HDX display unit presenting the message has critically high internal temperature. The display will automatically shutdown. Do not fly. Ensure nothing is obstructing airflow around affected display. If alert persists, contact Dynon Technical Support. Monitor remaining SkyView display and/or Standby Display System. Increase airflow or reduce ambient temperature near affected display. "CAUTION" EMS configuration files in SkyView HDX display units do not match. Update configuration file to most current version in all displays in SETUP MENU > SYSTEM SOFTWARE. No in-flight action. "CAUTION" The system has detected a wiring fault in the LEVEL button. Turn AP POWER switch OFF. Autopilot is disabled and must not be used until fault has been corrected. Turn AP POWER switch OFF. Do not use Autopilot for remainder of flight. On PFD: G-Meter is displayed. "GEES" The G-Meter has entered the configured yellow range. Do not fly. Operate elevator control to reduce G loading. "CAUTION" The identified GPS position source has failed. SkyView has switched to the next available GPS position source. Be aware that GPS redundancy has been reduced. Be aware that GPS redundancy has been reduced. "CAUTION" The Remote Magnetometer module has failed or is not communicating with SkyView. Heading information is unavailable. Use magnetic compass and GPS track for directional reference. Do not fly if flight requires Instrument Flight Rules (IFR). Use magnetic compass and GPS track for directional reference. Avoid operations in Instrument Meteorological Conditions (IMC). SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-19 CAUTION ALERTS VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION "CAUTION" Knob Control Panel is not communicating with SkyView. Use SkyView display unit knob controls. Use SkyView display unit knob controls. "CAUTION" The Remote Magnetometer's factory calibration is no longer valid. Heading information is unavailable. Use magnetic compass and GPS track for directional reference. Do not fly if flight requires Instrument Flight Rules (IFR). Use magnetic compass and GPS track for directional reference. Avoid operations in Instrument Meteorological Conditions (IMC). "CAUTION" Compass calibration for ADAHRS module not performed. Do not fly if flight requires Instrument Flight Rules (IFR). Avoid operations in Instrument Meteorological Conditions (IMC). "CAUTION" Angle of Attack (AoA) calibration for ADAHRS module not performed. Do not fly if flight requires Instrument Flight Rules (IFR). Avoid operations in Instrument Meteorological Conditions (IMC). "CAUTION" No high-resolution terrain database is installed for airplane’s current position. Install high- resolution database. Be aware that Synthetic Vision and Terrain Map resolution is degraded. "CAUTION" In a multi-display SkyView system, one HDX display unit is offline. Ensure power is supplied to offline display unit. If display contines to remain offline, contact Dynon Technical Support. Monitor operating HDX display unit and/or Standby Display System. "CAUTION" The identified position source has failed. Verify that all navigation equipment is powered ON. If message persists, use other navigational means. Use other navigational means. The system has no remaining GPS position sources available. The Map is no longer available. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-20 CAUTION ALERTS VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION "CAUTION" Software versions in SkyView HDX display units do not match. Before flight, update software to most current version in all displays in SETUP MENU > SYSTEM SOFTWARE. Do not use SkyView HDX display unit presenting Red Xs over indicators. "CAUTION" SkyView Network has lost a redundant network connection to one or more system components. Do not fly if flight requires Instrument Flight Rules (IFR). Avoid operations in Instrument Meteorological Conditions (IMC). "CAUTION" Touch screen functionality of affected SkyView HDX unit display not working. Use SkyView display unit knob controls. Use SkyView display unit knob controls. On PFD and Map: "TRAFFIC" A new Traffic Advisory (TA) target has been identified. No action, alert is suppressed on the ground. Pilot awareness only. Near AP Info Bar: "TRIM NOSE DOWN" The autopilot requires pitch trim in direction indicated. Visual annunciation appears immediately; aural after 10 seconds. No action. Apply pitch trim until the message stops. Near AP Info Bar: "TRIM NOSE UP" The autopilot requires pitch trim in direction indicated. Visual annunciation appears immediately; aural after 10 seconds. No action. Apply pitch trim until the message stops. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-21 CAUTION ALERTS VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION Near AP Info Bar: "TRIM ROLL LEFT" The autopilot requires roll trim in direction indicated. Visual annunciation appears immediately; aural after 10 seconds. No action. Apply roll trim until the message stops. Near AP Info Bar: "TRIM ROLL RIGHT" The autopilot requires roll trim in direction indicated. Visual annunciation appears immediately; aural after 10 seconds. No action. Apply roll trim until the message stops. "CAUTION" The system has detected a wiring fault in the Trim switch. Do not fly. Electric trim system must not be used until fault has been corrected. 1) Turn trim motor power OFF. 2) Trim airplane manually. Electric trim system must not be used until fault has been corrected. Near AP Info Bar: "TRIM YAW LEFT" The autopilot requires yaw trim in direction indicated. Visual annunciation appears immediately; aural after 10 seconds. No action. Apply yaw trim until the message stops. Near AP Info Bar: "TRIM YAW RIGHT" The autopilot requires yaw trim in direction indicated. Visual annunciation appears immediately; aural after 10 seconds. No action. Apply yaw trim until the message stops. SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-22 Messages Table 4 lists all SkyView system messages alphabetically by 1) visual and 2) aural annunciation. Messages are dependent upon installed systems and components. Table 4: Messages and Associated Crew Responses MESSAGES VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION "MESSAGE" ADS-B module has failed or not communicating with SkyView. Traffic and Weather is no longer availible, Use alternate sources for traffic and weather information. Traffic and Weather is no longer availible, Use alternate sources for traffic and weather information. No visual indication. "APPROACHING ALTITUDE" The airplane is approaching the bugged altitude. No action. Pilot awareness only. No visual indication. "APPROACHING MINIMUMS" The airplane's altitude is 200 feet above the selected MINIMUM altitude. No action. Pilot awareness only. No visual indication. "APPROACHING WAYPOINT" The airplane is within 30 seconds of crossing flight plan enroute waypoint. No action. Pilot awareness only. On AP Info Bar: Status bar flashes momentarily "AUTOPILOT" The autopilot has been engaged. Pilot awareness only. Pilot awareness only. On AP Info Bar: Status bar flashes momentarily "AUTOPILOT MODE" An autopilot mode has changed either manually or automatically since it was engaged. Pilot awareness only. Pilot awareness only. "MESSAGE" The backup battery connected to the SkyView HDX display unit has a low charge, but is not in use. Do not fly if flight requires Instrument Flight Rules (IFR). Allow backup battery to fully charge before flight. Avoid operations in Instrument Meteorological Conditions (IMC). SkyView Airplane Flight Manual Supplement, Rev V, 5/2/2024 Page | 7-23 MESSAGES VISUAL & AURAL ANNUNCIATION CONDITION PRE-FLIGHT ACTION IN-FLIGHT ACTION "MESSAGE" A year has passed since the previous backup battery test. Perform succsessful battery test prior to flight. N/A "MESSAGE" The current BARO setting and the nearest METAR- based altimeter setting are more than 0.1 INHG apart; or, the airplane has descended below FL180 and the BARO should be reset. Adjust BARO to field elevation. Adjust BARO setting as appropriate. "MESSAGE" COM Control Panel is not communicating with SkyView. If Dynon COM radio required for flight, do not fly. Use alternate communication equipment. If none available, use Lost Comms Procedures. "MESSAGE" COM Radio receiver is not communicating with SkyView. If Dynon COM radio required for flight, do not fly. Use alternate communication equipment. If none available, use Lost Comms Procedures. "MESSAGE" The SkyView HDX display unit’s internal temperature