Genesys IDU-680 Pilot's Manual
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Genesys IDU-680 Pilot's Manual

Electronic flight instrument system
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Summary of Contents for Genesys IDU-680

  • Page 2 Pilot Operating Guide and Reference Document 64-000099-080E (Fixed Wing) EFIS Software Version 8.0E Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 3 © 2016 Genesys Aerosystems All Rights Reserved No part of this document may be reproduced in any form, or by any means, without prior written consent of Genesys Aerosystems. FlightLogic and Virtual VFR are trademarks of Genesys Aerosystems. All other brand names and trademarks are the property of their respective holders.
  • Page 4 Retain this record in front of manual. Upon Record of receipt of a revision, insert changes and Revisions complete table below. Revision Number Revision Date Insertion Date/Initials Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 5: Table Of Contents

    General Arrangement ..........2-28 2.5. EICAS Display ............2-30 2.6. Color Conventions ............2-32 2.7. Warning/Caution/Advisory System ......2-34 2.8. Database and Software Updates ........2-64 2.8.1. Navigation and Obstruction Database ....2-64 2.8.2. Update Requirements .........2-64 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 6 ................2-68 Section 3 Display Symbology ........... 3-1 3.1. Introduction ..............3-10 3.2. IDU-680 PFD Display (Normal Mode) (Tapes) ..3-10 3.2.1. IDU-680 PFD Display (Normal Mode) with EICAS (Tapes) ................3-11 3.2.2. IDU-680 PFD Display (Basic Mode) (Tapes) ..3-12 3.3.
  • Page 7 Flight Director Symbology (FD1 Single Cue) (Tapes) ................3-49 3.5.27. Flight Director Symbology (FD2 Dual Cue) (Tapes) ................3-50 3.5.28. Course Deviation Indicator (Tapes) ....3-51 3.5.29. OBS Setting of CDI ..........3-53 3.5.30. Heading/Roll-Steering Sub-mode .......3-54 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 8 3.8.1. Clock and Groundspeed ........3-70 3.8.2. Fuel Remaining and Fuel Flow Data ....3-70 3.8.3. Waypoint Identifier Column ........ 3-71 3.8.4. VNAV and VNAV Offset Column ......3-71 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 9 HSI Screen VDI ..........3-87 3.17.3. Analog Navigation Symbology ......3-87 3.17.4. Air Data and Groundspeed .........3-90 3.17.5. Clock/Options .............3-90 3.17.6. Fuel Totalizer/Waypoint Bearing and Distance Functions ................3-90 Section 4 Reversionary Modes ..........4-1 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 10 PFD Failure Mode 4 (Normal Mode) (Tapes) .... 4-28 4.6.1. PFD Failure Mode 4 (Normal Mode) (Round Dials) ................4-29 4.6.2. MFD Failure Mode 4 (Normal Mode) ....4-30 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 11 5.2. Menu Synchronization ..........5-7 5.3. Menu Function Types ..........5-10 5.4. Top-Level Menu ............5-11 5.4.1. IDU-680 PFD Normal Mode Top-Level Menu ..5-11 5.4.2. IDU-680 MFD Normal Mode Top-Level Menu ..5-12 5.4.3. IDU-680 PFD or MFD Essential Mode Top-Level Menu ................5-13 5.4.4.
  • Page 12 First Level (MFD IDU other than #1) Normal Mode ................5-24 5.6.2. MFD Page First-Level Option Descriptions ..5-25 5.6.3. IDU-680 EICAS Page First-Level in Essential Mode ................5-25 5.6.4. EICAS Page First-Level Option Descriptions ..5-27 5.7. EICAS Exceedance Menu .......... 5-27 5.8.
  • Page 13 Heading Bug (HDG) Menu .........5-54 5.14.1. Heading Bug (HDG) Menu (Step-By-Step) ..5-55 5.15. Nearest (NRST) Menu ..........5-55 5.15.1. Nearest (NRST) Menu (Step-By-Step) ....5-58 5.15.2. Nearest (NRST) Menu ILS (Step-By-Step) ..5-58 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 14 5.26. MFD HSI Pointer (PTRS) Menu ......... 5-86 5.26.1. MFD HSI Pointer (PTRS) Menu (Step-By-Step) 5-87 Section 6 Quick Start Tutorial ........... 6-1 Section 7 IFR Procedures ............7-1 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 15 Missed Approach and Departure Path Definition ..7-30 7.9. Loss of Navigation Monitoring ........7-31 7.10. Discontinuities .............7-32 7.11. Selection of an Instrument Procedure ......7-32 7.11.1. Standard Terminal Arrival Route (STAR) (Step-By- Step) ................7-33 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 16 Flight into Terrain when not in Landing Configuration (GPWS Mode 4) ..............8-17 8.10. Excessive Downward Deviation from an ILS Glideslope (GPWS Mode 5) ..............8-19 8.11. 500-Foot Wake-Up Call ..........8-20 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 17 Jeppesen NavData Chart Compatibility .....9-10 9.8. ARINC 424 Path-Terminator Leg Types ....9-11 9.9. Data Logging and Retrieval ........9-16 9.10. Log Files/Delete LOG Files ........9-17 9.10.1. Downloading Screen Capture from Ground Maintenance Pages .............9-17 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 18 Remote BUGs Panel .......... RBP-3 S 1. WX-500 Data ............... S-3 S 1.1. Strike Screen Range ........... S-4 S 1.2. Air Data and Groundspeed ......... S-4 S 1.3. Clock and Options ..........S-4 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 19 AR 3.2. Marker Beacon Receiver .........AR-14 AR 3.3. Marker Beacon Receiver Symbols ....AR-14 AR 4. AR Tune Menu.............AR-15 AR 5. Expanded AR Page ..........AR-21 AR 5.1. ADR7050 COM Transceiver ......AR-24 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 20 MFD Datalink Format (FORMAT) Menu ....D-17 D 2.1. MFD DATALINK Page (Step-By-Step) ....D-18 D 3. Active Flight Plan (ACTV) Menu Options ....D-22 D 4. Information (INFO) Menu .......... D-22 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 21 V 1.3. Video Input Status Display ........V-4 V 2. MFD Video Input Format (FORMAT) Menu ....V-6 V 3. IDU-680 Center Rotary Encoder Controls ....V-8 INDEX GLOSSARY Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 22: Introduction

    Section 1 Introduction Section 1 Introduction Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 23 Section 1 Introduction Revision Record Rev Notes Date Author 1. Change image in Figure 1-3: IDU-680 Nov, Multifunction Display (MFD) 2016 Schmidt 2. Added note regarding initialization on page 2-23. 3. Replaced image in Figure 2-4: MFD with EICAS Essential Mode.
  • Page 24 (PFD) ....1-6 IGURE RIMARY LIGHT ISPLAY 1-3: IDU-680 M (MFD) ....1-7 IGURE ULTIFUNCTION ISPLAY 1-4: IDU-680 R IGURE EMONSTRATOR RAINING PPLICATION 1-5: A ..........1-12 IGURE UDIO AND IDEO CONS Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 25: Introduction

    Contrary to the traditional idea of overloading the pilot with information and options, this Genesys Aerosystems EFIS clearly and concisely presents only necessary information. This reduces pilot workload while greatly decreasing task complexity as it minimizes confusion.

  • Page 26: Figure 1-1: Idu-680 Input Identification

    When this door is lifted, an optical switch initiates the Ground Maintenance mode to gain access to the maintenance program once a USB memory device is inserted. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 27: Figure 1-2: Idu-680 Primary Flight Display (Pfd)

    NOTE: If entering the Ground Maintenance mode with bright light shining directly on the display, shield the light sensor if necessary. Figure 1-2: IDU-680 Primary Flight Display (PFD) IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 28: Run Demonstrator/Training Application

    1) With power off, lift the USB Memory Flash Door. Insert a USB Flash Memory Storage Device in the IDU lower bezel.  2) Power the system on and use (scroll and push to enter) to select RUN DEMONSTRATION/TRAINING APPLICATION. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 29: Efis Training Tool

    The EFIS Training Tool (ETT) is an application entirely based on the EFIS code and is compatible with 32- or 64-bit versions of Microsoft Windows. It serves as a multi-purpose tool for training pilots and IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 30: About This Guide

    IDU display. The audio output capability for the ETT matches the audio functionality in the actual IDU. This training tool simulates the functionalities of the IDU-680, which begins flight in Reno, Nevada at approximately 7900’ MSL. If different ETT startup conditions are required, they may be edited.
  • Page 31 PFD and ND presentation… REVERSIONARY MODES (Section 4) This section provides views of the IDU-680 displays with various sensor failed conditions and resulting symbology as well as examples of various configurations and display formats used with specific tables showing affected functions.
  • Page 32 Miscompare thresholds; EFIS Training Tool accessibility; naming conventions used by the navigation database provider; flight data recorded information format; downloading routes and user waypoints; and sourcing a copy of the Service Difficulty Report form… Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 1-11...

  • Page 33: 1.5.1. Audio And Video Interactive Capabilities

    3 6 T U U 3 6 T If you encounter problems with the operation of your Genesys Aerosystems EFIS, please complete and return the Service Difficulty Report in Section 9 Appendix section directly to: Genesys Aerosystems...

  • Page 34: System Overview

    Section 2 System Overview Section 2 System Overview Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 35: Abbreviations And Acronyms

    2.9....2-68 EMONSTRATOR RAINING ROGRAM 2.9.1. Application Software Air Mode and Ground Mode ................2-68 List of Figures and Tables 2-1: S ............. 2-19 IGURE YSTEM IAGRAM IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 36 .....2-35 ABLE ARNINGS AUTIONS DVISORIES 2-3: A ...........2-62 ABLE NNUNCIATIONS RIORITY 2-4: L ............2-63 ABLE ALUES 2-9: G ........2-64 IGURE ROUND AINTENANCE 2-10: IDU-680 I ......2-66 IGURE NITIALIZATION CREEN Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 37 American National Standards Institute Antenna Waypoint is part of an Instrument Approach Procedure APPR Approach Airport Approach with Vertical Guidance Audio Radio ARINC Aeronautical Radio, Inc. SAE Aerospace Recommended Practice IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 38 Course to Fix (ARINC-424 Leg) Course to Intercept (ARINC-424 Leg) Clear Configuration Management Communications/Navigation/Surveillance Cancel Communication CONT Continue CPLT Co-Pilot Company Project Manager; Computer Processor Module Central Processing Unit Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 39 Decision Height Data Link Distance Measuring Equipment DMIR Designated Manufacturing Inspection Representative RTCA Document Department of Defense Digital Obstruction File Departure Procedure Dead Reckoning or; Defect Report Digital Signal Processing IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 40 "First in, First out" Flight Information Service FIS-B Flight Information Service-Broadcast Flight Level FLTA Forward Looking Terrain Awareness Course from Fix to Manual termination (ARINC-424 Leg) FMEA Fault Mode and Effects Analysis Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 41 Ground Proximity Warning System Grid; Ground Glideslope Hold Terminates at an altitude (ARINC-424 Leg) Holding, Pattern to Fix (ARINC-424 Leg) Altitude or Manual Termination (ARINC-424 Leg) Horizontal Alert Limit Height Above Threshold IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 42 Instrument Flight Rules Instrument Landing System Inner Marker INFO Information INHBT Inhibit inHg Inches of Mercury INIT Initialize Input/Output Initial Point Instrument Procedure with Vertical Guidance International Standard Atmosphere Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 43 Waypoint is part of the missed approach segment of an Instrument Approach Procedure MAGVAR Magnetic Declination (Variation) MAHP Missed Approach Holding Point MAHWP Missed Approach Holding Waypoint (same as MAHP) 2-10 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 44 National Aeronautical Charting Office U.S. National Airspace System NASA National Aeronautics and Space Administration Navigation NAVAID Device or system providing navigational assistance Navigation Display Nondirectional Beacon National Elevation Dataset Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-11...
  • Page 45 -- also refers to the primary IDU with software that only shows primary instrumentation) PFDE Predictive Fault Detection and Exclusion Primary Flight Information Procedure Turn (ARINC-424 Leg) Peripheral Interface Controller Pitch Limit Indicator 2-12 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 46 Precision Arc to Fix (ARINC-424 Leg) RFMS Rotorcraft Flight Manual Supplement Radio Frequency Panel Retractable Gear RG + F Retractable Gear with Defined Landing Flaps Position Radar Height Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-13...
  • Page 47 Analog color television system used in France SECI Software Environment Configuration Index Standard Instrument Departure SIGMET Significant Meteorological Advisory SLCT Select Sub-Miniature version A connector Serial Number Serial Number Information 2-14 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 48 Traffic Advisory (Traffic Function) TACAN Ultra-High Frequency Tactical Air Navigational Aid TAFs Terminal Aerodrome Forecasts Traffic Advisory System; True Airspeed TAWS Terrain Awareness and Warning System Terminal Control Areas Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-15...
  • Page 49 Universal Serial Bus, data storage device USGS United States Geological Survey User Waypoint Universal Time Coordinated Speed beyond which the takeoff should no longer be aborted Takeoff safety speed 2-16 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 50 Never exceed speed Maximum structural cruising speed or maximum speed for normal operations VHF Omnidirectional Radio VORTAC Collocated VOR and TACAN Voice Vertical Protection Level Procedure Speed PROC Rotation speed Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-17...

  • Page 51: System Overview

    XFILL Cross-fill 2.2. System Overview The IDU-680 EFIS is a complete flight and navigation instrumentation system that intuitively provides information to a pilot via computer generated screen displays. The screen displays include three-dimensional, enhanced situational awareness Primary Flight Display (PFD) and Multi-Function Display (MFD). The MFD...

  • Page 52: Functional Integration And Display Redundancy

    *AHRS #2 *IDU #4 Engine Data *Datalink/ *Weather Pilot Co-Pilot ADS-B Radar *Mode S *WX-500 Transponder *Analog *Fuel Flow/ Interface Quantity Note: * = Optional Figure 2-1: System Diagram Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-19...

  • Page 53: Idu Initialization

    The hardware, including file system, IO, and graphics, is initialized. Immediately after graphics initialization, a logo screen with “INITIALIZING” is displayed with the Genesys Aerosystems logo, software version number, and part number. The software version number delineates: (1) major revision number (i.e., “8.0”), and (2) minor revision letter (i.e., “E”).
  • Page 54 IDU decides whether it is booting on the ground or in flight. If booting on the ground, the following actions happen: 1) A logo screen with “TESTING” is displayed. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-21...
  • Page 55 2 minutes has elapsed; b) when the pilot presses any button to escape the startup countdown; or c) when all critical sensors are in normal condition. 2-22 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 56 PFDs to sync with MFDs and allows pilot and copilot sides to sync (as applicable). If any IDU menu is active, intra-system and inter- system synchronization messages are paused. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-23...

  • Page 57: Software Safety Functions

    EICAS page is half-screen, a pilot-selectable multi-function page in the bottom area. If IDUs configured as #3 or #4 are installed, their “Normal” state is pilot-selectable multi-function pages in both areas. 2-24 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 58 Press (R5) to switch any screen between “Normal” and “Essential” states; the legend changes between TO ESSNTL and TO NORMAL to indicate the button action. State change is instantaneous. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-25...

  • Page 59: Menu Philosophy

    A filled triangle next to a menu legend means the button press leads to a further menu level. 2-26 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 60: Avoidance Of Autonomous Behavior

    Data Source Monitors In installations with redundant sensors, the IDUs continuously monitor the sensors to detect disagreements. The following parameters from redundant sensors are compared: 1) Airspeed 2) Altitude Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-27...

  • Page 61: Idu Intra-System Communications

    10) Radar altitude agreement 2.4. General Arrangement The IDU-680 is 7.500”W x 10.250”H x 4.750”D and weighs less than 9.5 lbs. The IDU-680 is composed of two major sub-assemblies mechanically connected by through-bolts, the User Interface Module (UIM) and the Computer Processor Module (CPM). The IDU-680 has the capacity to accommodate “Integrated Peripherals”...
  • Page 62 Section 2 System Overview sensor modules in parallel, each IDU is independent from all other IDUs. In an IFR installation, the software of the primary IDU-680 is configured so only the primary screen Primary Flight Information (PFI) display top half plus Multi-Function display (MFD) bottom half may be displayed (Figure 2-5).

  • Page 63: Eicas Display

    IDU-680s are configured as a primary display of engine information; at least one of the Multi-Function Display areas must show the engine display. Figure 2-6 is an IDU-680 Multi-Function display with the top display area showing the EICAS and bottom area configured to the MAP page.
  • Page 64 Section 2 System Overview Figure 2-7: PFD with EICAS Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-31...

  • Page 65: Color Conventions

    Figure 2-8: MFD with HSI and EICAS 2.6. Color Conventions The Genesys Aerosystems EFIS uses a consistent set of colors for displaying information on display. (Any color representation may not be identical as it appears on the IDU.) WHITE is used for items set by the pilot and held internally...
  • Page 66 VOR #2 and to indicate normal or valid operation (airspeed, altitude tape coloring, status indication, etc.). Examples:  Aircraft ground track  Skyway symbology  Airspeeds in green arc Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-33...

  • Page 67: Warning/Caution/Advisory System

    Table 2-2 lists the annunciations provided by the IDU. Displayed with red flag and an aural annunciation repeating until the condition goes away or is acknowledged by the pilot. 2-34 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 68 (V “Overspeed, as appropriate) plus Overspeed” instrument error. No time delay. “Terrain, Terrain cell within TAWS Terrain, Pull FLTA warning envelope. Up, Pull Up” Half second time delay. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-35...
  • Page 69 Only active in dual-ADC installation. Indicates no valid indicated airspeed, Alert Tone pressure altitude, or VSI received from ADC #2 for more than 1 second. No time delay. 2-36 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 70 Only active in dual-ADC installation with neither ADC in failure condition. Indicates pressure altitude Alert Tone difference between ADCs is beyond limits. 10-second time delay. Inhibit for 5 minutes after startup. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-37...
  • Page 71 1) RS-232 TAS System Auxiliary 2) ADS-B System Sensor Failure” 3) WSI Datalink System 4) WX-500 Lightning System 5) Analog Interface System 6) Weather Radar 7) Weather Radar Control Panel 2-38 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 72 Alert Tone ing fan status discrete input indicates the cooling fan is not rotating. 1-minute time delay. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-39...
  • Page 73 2) One of the sensed fuel Fuel Low” tank quantities is below its low fuel caution threshold. 3) Total aircraft fuel is below the pilot-set minimum fuel threshold. 1-minute time delay. 2-40 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 74 10 seconds after unusual attitude mode. Loss of Vertical Navigation caution. No time delay. Inhibited Alert Tone during and for 10 seconds after unusual attitude mode. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-41...
  • Page 75 4°. Groundspeed: If difference between GPS#1 and GPS#2 miscompare is more than 10 kts. 10-second time delay. Inhibited during and for 10 seconds after unusual attitude mode. 2-42 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 76 GPS/SBAS for more than 5 seconds, and dead Alert Tone reckoning not available. No time delay. Inhibited during and for 10 seconds after unusual attitude mode. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-43...
  • Page 77 Only active in dual-ADC installation with neither ADC in failure condition. Indicates indicated airspeed difference Alert Tone between ADCs is beyond limits. Inhibit for 5 minutes after startup. 10-second time delay. 2-44 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 78 TAWS FLTA function Alert Tone from operating. Half second time delay. Inhibited during and for 10 seconds after unusual attitude mode. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-45...
  • Page 79 Alert Tone 1) Attitude (Pitch and Roll) (use Attitude Miscompare logic) 2) Heading (use Heading Miscompare logic) 3) Pressure Altitude (use Altitude Miscompare logic) 2-46 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 80 10) Track (Use GPS/SBAS Mis- compare logic) 11) Groundspeed (Use GPS/SBAS Mis- compare logic) 1-second time delay. Inhibited during and for 10 seconds after unusual attitude mode. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-47...
  • Page 81 2000’ AGL in Air Mode without a valid radar Alert Tone altimeter reading. For ARINC 429, radar altimeter indicates an SSM of failure warning is transmitting. 2-second time delay. 2-48 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 82 Ground Alert Tone Mode. Inhibited when radar altimeter value received from ARINC 429, except when SSM of radar altimeter message indicates failure warning. 2-second time delay. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-49...
  • Page 83 “SSEC2 FAIL” used in dual ADC installations. “SSEC FAIL” used in a single ADC installation. Inhibited is the related ADC is in a failed condition. 1-minute time delay. 2-50 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 84 Indicates both systems are Alert Tone operating from the same EICAS data source for labels where dual sources are setup in the OASIS configuration file. No time delay. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-51...
  • Page 85 Indicates both systems are operating from same radar altimeter source. No time delay. Within GPWS Mode 1 “Sink Rate, caution envelope. Sink Rate” Half second time delay. 2-52 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 86 “Too Low Gear” envelope. Gear, Too Low Gear” Half second time delay. “Too Low Within GPWS Mode 4-3 “Too Low Flaps” envelope. Flaps, Too Low Flaps” Half second time delay. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-53...
  • Page 87 1950. Pitch trim running “Trim in for more than a preset Motion, Trim amount of time in UP in Motion” direction. Amount of time is part of the aircraft limits. 2-54 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 88 150’ from alti- tude of the current or prior VNAV waypoint after cap- ture. Altitude capture de- fined as being within 100’ of altitude. 2-second time delay. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-55...
  • Page 89 Chime upon current GPS/SBAS HPL. Only active in dual-system (pilot and co-pilot) installa- tion. Indicates mismatch of Chime altimeter settings or altimeter modes between systems. 10-second time delay. 2-56 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 90 Shown when the FLTA function is automatically inhibited during normal operation. “NO TAWS” Chime caution and “TAWS IN- HBT” advisory have priority over this message. No time delay. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-57...
  • Page 91 ## is Chime nautical miles left (L) or right (R) of main path. No time delay. GPS/SBAS Automatic Re- quired Navigation Perfor- Chime mance as acquired from navigation database 2-58 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 92 Chime discrete input. No time delay. Only active with TCAS-II system. Indicates system Chime is: (1) in standby or (2) executing functional test in flight. No time delay. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-59...
  • Page 93 Only active in dual-system (pilot and co-pilot) with good inter-system com- munications and crossfill Chime not inhibited. Indicates systems are not synchro- nized and synchronization function is available. No time delay. 2-60 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 94 50% of VSI from Altitude Alert uncaptured selected or Tone VNAV waypoint altitude. Inhibited in approach procedures. No time delay. Sounds chime when Chime countdown timer reaches 00:00:00. No time delay. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-61...
  • Page 95 12) GPWS Mode 4-3 13) GPWS Mode 1 Caution 14) GPWS Mode 2 Caution 15) GPWS Mode 3 16) GPWS Mode 5 Warning 17) GPWS Mode 5 Caution 18) Check Gear 2-62 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 96 CAS messages to be controlled by the EICAS configuration file. Within the data fields of the log file, values are written as follows. Table 2-4: Log File Values Category Value NORMAL ADVISORY CAUTION WARNING Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-63...

  • Page 97: Database And Software Updates

    3 6 T U U 3 6 T correct database. Three types of navigation databases may be used on this EFIS. 2-64 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 98 IDU successfully updated with the latest database by noting the new NavData cycle expiration dates before acknowledging the initialization screen. There is no expiration for the obstruction database. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 2-65...
  • Page 99 RNP values (if applicable). DPs and STARs are retrievable as a procedure (selecting the procedure by name results in loading the appropriate waypoints and legs into the flight plan). 2-66 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 100: Terrain Database Update

    LNAV/VNAV procedure are uniquely identified as such to provide proper approach mode operation. 2.8.3. Terrain Database Update The IDU-680 contains the entire World Terrain Database, which is updated on an as-needed basis and performed as required as described in a service bulletin. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 101: Run Demonstrator/Training Program

    If airspeed is invalid but AGL altitude is valid, Ground Mode is set when AGL altitude is less than 75 feet. c) Under any other circumstance, Air Mode is set by default. 2-68 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 102: Display Symbology

    Section 3 Display Symbology Section 3 Display Symbology Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 103: Section 1 Introduction

    ISPLAY ORMAL APES 3.2.1. IDU-680 PFD Display (Normal Mode) with EICAS (Tapes) ................. 3-11 3.2.2. IDU-680 PFD Display (Basic Mode) (Tapes) ... 3-12 3.3. IDU-680 MFD D ) ....3-14 ISPLAY ORMAL 3.3.1. IDU-680 MFD Display (Essential Mode) (Tapes) ...
  • Page 104 Flight Director Symbology (FD2 Dual Cue) (Tapes) ................3-50 3.5.28. Course Deviation Indicator (Tapes) ....3-51 3.5.29. OBS Setting of CDI ...........3-53 3.5.30. Heading/Roll-Steering Sub-mode .....3-54 3.5.31. Vertical Deviation Indicator .......3-54 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 105 Clock and Groundspeed ........3-70 3.8.2. Fuel Remaining and Fuel Flow Data ....3-70 3.8.3. Waypoint Identifier Column ......3-71 3.8.4. VNAV and VNAV Offset Column ..... 3-71 3.8.5. Path Column ............ 3-72 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 106 3.17.4. Air Data and Groundspeed .......3-90 3.17.5. Clock/Options ...........3-90 3.17.6. Fuel Totalizer/Waypoint Bearing and Distance Functions ................3-90 List of Figures and Tables 3-1: PFD ) .........3-10 IGURE ORMAL APES Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 107 ECISION EIGHT OUND IALS 3-31: A ) ........3-29 IGURE IRSPEED ISPLAY APES 3-32: A ) ........3-30 IGURE IRSPEED REND APES 3-5: A ..........3-30 ABLE IRSPEED IMITS IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 108 FD2 (N ) (T ) ..3-50 IGURE LIGHT IRECTOR ORMAL APES 3-66: F FD2 (B IGURE LIGHT IRECTOR ASIC ODE WITHOUT OMPASS ND) (T ) ..........3-51 ETECTED ON APES Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 109 3-18: A ..........3-78 ABLE IRSPACE EPICTION 3-95: A ......... 3-79 IGURE ATA AND ROUNDSPEED 3-96: A ......3-81 IGURE NALOG AVIGATION YMBOLOGY 3-97: B ............... 3-82 IGURE ORDERS IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 110 WITH ARKER EACON ISPLAYED APES 3-107: HSI D ...3-90 IGURE ISPLAY ATA AND ROUNDSPEED 3-108: HSI C ............3-90 IGURE LOCK 3-109: HSI F IGURE OTALIZER AYPOINT EARING UNCTIONS ....................3-90 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 111: Introduction

    Section 3 Display Symbology 3.1. Introduction In an IFR installation, the software of the primary IDU-680 is configured so only the primary screen (Primary Flight Information in top half and Multifunction Display in bottom half) is displayed. The software is configured on all other IDU-680 displays so any screen display may be shown at any time.

  • Page 112: Pfd Display (Normal Mode) With Eicas (Tapes)

    Section 3 Display Symbology 3.2.1. IDU-680 PFD Display (Normal Mode) with EICAS (Tapes) Figure 3-2: PFD in Normal Mode with EICAS (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-11...

  • Page 113: Pfd Display (Basic Mode) (Tapes)

    1) Atmospheric perspective 5) Flight Path Marker 2) Airspeed Trend 6) Airport runways 3) Terrain rendering 7) Highway in the Sky 4) Obstruction rendering 8) Bank Scale Declutter 3-12 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 114 2) Airspeed trend 8) Mini MAP 3) Terrain rendering 9) Mini TRFC 4) Obstruction rendering 10) Turn IND 5) Flight Path Marker 11) Bank Scale Declutter 6) Airport runways Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-13...

  • Page 115: Mfd Display (Normal Mode)

    Section 3 Display Symbology 3.3. IDU-680 MFD Display (Normal Mode) Figure 3-5: MFD in Normal Mode with MAP Page Displayed on Top and Bottom 3-14 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 116: Mfd Display (Essential Mode) (Tapes)

    Section 3 Display Symbology 3.3.1. IDU-680 MFD Display (Essential Mode) (Tapes) Figure 3-6: MFD in Essential Mode with EICAS (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-15...

  • Page 117: Mfd In Normal Mode

    (with further Without further levels) or hollow triangle (without menu levels further levels) pointing to the associated button. Figure 3-8: Menu Functions 3-16 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 118: Selecting Baro

    (inHg) or millibars (mbar) value in the lower right corner.  Scroll clockwise to increase or counter clockwise to decrease  QNH. Push to enter the new value. Figure 3-10: Selecting BARO (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-17...
  • Page 119 QNH: Barometric setting resulting in the altimeter displaying altitude above mean sea level at the reporting station. Figure 3-11: Altimeter Setting (Tapes) 3-18 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 120: Selected Altitude Sub-Mode (Target Altitude) (Tapes)

    When not vertically integrated with an autopilot, the target altitude bug setting annunciation is white, and the target altitude bug is filled-white at all times. Figure 3-14: Target Altitude Bug (Not Vertically Integrated) (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-19...

  • Page 121: Vnav Sub-Mode

    “parked” in the direction of the difference with half of the associated bug visible as seen in Figure 3-16. 3-20 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 122: Altitude Display (Vnav Tile)

    Other objects in the background, including terrain, obstructions, traffic, and runways, are presented conformally as if seen directly in front of the aircraft while looking outside. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-21...

  • Page 123: Minimum Altitude

    When a minimum altitude is set, descending from above to below causes an aural annunciation of “Minimums, Minimums” and the minimum altitude to turn amber (yellow) and begin to flash. 3-22 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 124: Altitude Display (Round Dials)

    When the ADC sensor fails, a black circle with red “X” is shown instead of the altitude readout, dial, and pointer. Figure 3-21: Altitude Display (Round Dials) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-23...
  • Page 125 The resolution is one meter like the target altitude bug setting. The altimeter setting displays exactly as described in § 3.4.1. Figure 3-22: Metric Altitude (Round Dials) 3-24 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 126: Vertical Speed Indicator (Tapes)

    FPM. Figure 3-24: VSI Bug (Tapes) The vertical speed bug is used either as a visual reference or, when vertically integrated with an autopilot (either fully integrated or Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-25...

  • Page 127: Vertical Speed Indicator (Round Dials)

    (Analog) AGL Indicator. These are mutually exclusive of each other and driven by whichever AGL altitude source is used for a TAWS system but not displayed when source is invalid. 3-26 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 128: Analog Agl Indication (Tapes Only)

    The circular tape has a radial line at its end and disappears above 1000’ AGL. Figure 3-28: Analog AGL Indication Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-27...
  • Page 129 20’  30’  40’  50’   60’  70’  80’  90’ 100’  200’  300’  400’  500’   1000’ 3-28 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 130: Decision Height (Tapes)

    80-130 measurement units. During an ADC failure, a red “X” is displayed in place of the airspeed scale. Figure 3-31: Airspeed Display (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-29...
  • Page 131 1) If in Air Mode, a red low-speed awareness area from the bottom of the scale to V . The airspeed readout is red in this area. 3-30 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 132 A red high-speed awareness area from the lower of V to the top of the scale. The airspeed readout is red in this area. Aircraft Aircraft Figure 3-33: Airspeed Scale FAR Part 23 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-31...
  • Page 133 The airspeed readout is red in this area. The airspeed scale for Part 25 airplanes have additional specific airspeed markings as follows: 3-32 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 134 6) If enabled (V extension speed marker at V On Ground In Flight with V or No V 1.2 x V 1.1 x V Figure 3-34: Airspeed Scale FAR Part 25 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-33...

  • Page 135: Airspeed Display (Round Dials)

    The V , and V symbols automatically declutter when the respective value is exceeded by 40 knots or when above 2000 feet AGL. 3-34 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 136: Airspeed Display (With Efis-Coupled) (Tapes)

    (Y-axis) G-force (slip indicator is the white rectangular part of the heading pointer). Figure 3-39: Slip/Skid Indicator (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-35...
  • Page 137 (not necessarily the safest) direction of turn to 3-36 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 138: 3.5.13. Pitch Scale

    AHRS in DG Mode (Round Dials) Heading detected No heading detected in bottom area in bottom area Figure 3-43: Heading in Bottom Area (Round Dials) 3.5.13. Pitch Scale Figure 3-44: Pitch Scale (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-37...

  • Page 139: Pitch Limit Indicator (Tapes)

    1-G V or V airplanes 1-G V corrected for G-loading where V or V corrected calculated by dividing the pilot-input V for G-loading 1.23. 3-38 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 140: G-Force And Fast/Slow Indicator (Tapes)

    If the G-limits have been exceeded, a Ground Maintenance Function option is available to reset exceedance on the ground only. Figure 3-49: RESET G Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-39...

  • Page 141: G-Force Indicator (Round Dials)

    Figure 3-51: G-Force Indicator (Round Dials) 3.5.17. Landing Gear Indication (Tapes and Round Dials) Basic Mode Normal Mode Figure 3-52: Landing Gear Indication 3-40 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 142: Unusual Attitude Mode (Tapes)

    12) If in Zoom mode FOV, PFD 6) Atmospheric perspective reverts to normal FOV 7) Analog and Digital AGL 13) Runways indication Figure 3-53: Unusual Attitude Mode (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-41...

  • Page 143: Pfd Background (Tapes Only)

    Figure 3-54: PFD Terrain and Obstructions (Tapes) 3-42 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 144 Shades of olive when at Amber and red are or below 100 feet less used for normal display TAWS than aircraft altitude. The of terrain. slope between adjacent Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-43...
  • Page 145 DO NOT USE THIS EFIS FOR TERRAIN-FOLLOWING FLIGHT. DO NOT ATTEMPT TO NAVIGATE USING THE TERRAIN DEPICTION. ALWAYS ADHERE TO PUBLISHED NAVIGATIONAL INSTRUMENT PROCEDURES AND NAVIGATIONAL CHARTS IN ALL FLIGHT CONDITIONS. 3-44 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 146 PFD display as vertical amber (yellow) lines. Obstructions are conformal in both location and size and only shown in conjunction with terrain regardless of Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-45...

  • Page 147: Flight Path Marker (Velocity Vector) Basic Mode (Tapes)

    The flight path marker appears at a location on the background to coincide with the aircraft’s actual flight path as projected upon the outside world. The 3-46 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 148 Flight path marker movement is dampened by reference to aircraft pitch and heading so as not to deviate from pitch or heading at a rate greater than 1°/sec. Figure 3-57: Flight Path Marker Ghost (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-47...

  • Page 149: Bank Angle Scale (Tapes)

    This allows the pilot to fly a standard rate turn and incorporates a standard “balance ball” display. Figure 3-60: Turn Rate Indicator (Round Dials) 3-48 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 150: 3.5.24. Timer Indication

    PFD (Figure 3-62). Figure 3-62: Marker Beacons (Tapes) 3.5.26. Flight Director Symbology (FD1 Single Cue) (Tapes) Figure 3-63: Flight Director FD1 Single Cue (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-49...

  • Page 151: Flight Director Symbology (Fd2 Dual Cue) (Tapes)

    Figure 3-64: Flight Director FD1 (Basic Mode with Compass Rose Detected on ND) (Tapes) 3.5.27. Flight Director Symbology (FD2 Dual Cue) (Tapes) Figure 3-65: Flight Director FD2 (Normal Mode) (Tapes) 3-50 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 152: Course Deviation Indicator (Tapes)

    Table 3-11: CDI Behavior and Color CDI Pointer and Condition Color or Behavior Full Scale Deflection Flash When Slaved to GPS/SBAS Scale is appropriate FSD value for mode of flight: Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-51...
  • Page 153 Amber (Yellow) (with GPS Loss of Navigation) Normal conditions Magenta In sources other than FMS Angular scale annunciation Navigation source is Localizer Reverse sensing (Course error exceeds 105°) 3-52 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 154: 3.5.29. Obs Setting Of Cdi

    CDI as follows: 1) NAV: FMS1 4) NAV: LOC1 2) NAV: FMS2 5) NAV: BC1 (annunciated instead of LOC1 when 3) NAV: VOR1 course error exceeds 105°) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-53...

  • Page 155: 3.5.30. Heading/Roll-Steering Sub-Mode

    The vertical deviation indicator only appears when the source of vertical navigation is valid, and the source of vertical navigation is FMS (either LPV or VNAV modes). Figure 3-68: Vertical Deviation Indicator (Tapes) 3-54 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 156 VNAV waypoint (i.e., taking into account VNAV offsets); and 3) If on the final approach segment, the aircraft is within a 35° lateral wedge of the azimuth reference Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-55...
  • Page 157 4) GS1 or GS2: Glideslope receiver #1 or #2 as indicated. Pilot follows guidance to published Barometric DH. Figure 3-69: Vertical Deviation Indicator Color during GPS/SBAS LON or VLON (Tapes) 3-56 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 158 VDI for LNAV/VNAV and LPV approaches (Figure 3-70). Figure 3-70: EFIS Coupled Vertically with Glideslope Mode Engaged (Tapes) 3.5.33. Highway in the Sky/Skyway (Tapes only) Coupled Uncoupled Figure 3-71: Highway in the Sky Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-57...
  • Page 159 The active waypoint symbol disappears in Unusual Attitude Mode and turns amber (yellow) in the event of GPS Loss of Navigation caution. 3-58 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 160 3.5.35. Mini Map (Tapes only) Figure 3-73: Mini Map VOR #1 VOR #2 Figure 3-74: Mini Map VOR Symbology Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-59...
  • Page 161 3.5.36. Runways (Tapes only) Figure 3-75: Runways The PFD displays airport runways in a 3-D manner. Immediately upon a system startup on the ground, runways for the nearest airport 3-60 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 162 Runway markings Medium gray Landing portion of the Taking into Light gray selected runway. account displaced threshold data. Runway markings for Lighter gray the selected runway than light gray. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-61...
  • Page 163 The Navigation Display is presented in a variety of formats: 1) Moving Map 6) Datalink 2) Conventional HSI 7) WX RDR 3) Navigation Log 8) Video 4) Strikes 9) EICAS 5) Traffic 10) Radio page 3-62 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 164 FAR 23 with V With V Figure 3-77: Ownship Symbology Airplane w/o M Airplane with M Figure 3-78: Ownship Symbols 3.7.2. Basic Moving Map Figure 3-79: Basic Moving Map Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-63...
  • Page 165 Section 3 Display Symbology 3.7.3. Moving Map with Instrument Approach Figure 3-80: Moving Map with Instrument Approach 3.7.4. North-Up Arc Mode Figure 3-81: North-Up Arc Mode 3-64 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 166 Heading-Up Centered Mode Figure 3-83: Heading-Up Centered Mode 3.7.7. Waypoint Symbology The ND displays navigation symbology in its correct relationship to the ownship symbol and includes the following symbols. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-65...
  • Page 167 North discrete input. When the HSI NAV source (FMS, VOR1, or VOR2) fails, a red “X” is displayed in place of the HSI deviations. Figure 3-84: Conventional HSI/PTR Format 3-66 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 168 See Section 7 IFR Procedures for description of the following heading modes with the AHRS and EFIS: 1) ADAHRS Slaved—EFIS Magnetic North 2) ADAHRS Slaved—EFIS True North 3) ADAHRS Free/”DG”—EFIS Magnetic North 4) ADAHRS Free/”DG”—EFIS True North Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-67...
  • Page 169 Range and time to waypoint are based on flight plan route if active waypoint is not the last waypoint. Otherwise, range and time are based on a direct geodetic path. 3-68 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 170 Local Offset Time Figure 3-87: Clock Options Table 3-17: Clock/Options Feature Options Notes Zulu Zulu or Local Shown in hh:mm:ss and Time or synchronized with the GPS/SBAS Local constellation. Offset Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-69...
  • Page 171 The following are displayed in the upper right corner of the NAV Log: 1) Fuel Remaining: If either fuel level or fuel flow is available, current fuel remaining is displayed digitally in fuel units. 3-70 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 172 Glidepath Intercept point. VNAV altitudes and offsets from the navigation database or manually entered are white; those computed automatically are gray. VNAV and VNAV Offset column elements align with Waypoint Identifier Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-71...
  • Page 173 Distance column elements are offset from Waypoint Identifier column elements to indicate distance information applies to the leg between waypoints. 3-72 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 174 1) Path data (dashes) 4) ETA data (dashes) 2) Distance data (dashes) 5) Fuel remaining data (dashes) 3) ETE data (dashes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-73...
  • Page 175 Altitude is captured and shown as a green arc located ahead of the aircraft after passing the Top-of-Descent, along the lubber line. The arc marks the bottom-of-descent or top-of-climb point. 3-74 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 176 OBS mode, skyway boxes, and mini-map). The active flight plan path’s active leg/manual course and active waypoint are magenta but turn amber (yellow) in the event of a GPS Loss of Navigation caution. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-75...
  • Page 177 Consequently, when the range ring shows a distance of 5NM, the   directional scale is 10NM. Scroll to set the overall map scale ranges to .5, 1, 2.5, 5, 10, 25, 50, 100, and 200NM as appropriate. 3-76 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 178 The ND displays navigation data in correct relationship to the ownship symbol with navigation data symbols, including airport symbols, NDBs, and user waypoints. High altitude and low altitude airways may be shown. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-77...
  • Page 179 1, 2, and 3. 2) VORs: Manually or automatically decluttered. In automatic declutter mode, VORs are shown in levels 1, 2, 3, 4, and 5. 3-78 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 180 1) Wind: Information consists of the following readouts: a) Direction in degrees; b) Speed in knots; c) Crosswind component in knots; and d) Graphical wind vector arrow oriented to correspond to the ND orientation. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-79...
  • Page 181 If the DME channel is in hold mode, “H” is shown above the distance readout. If a bearing or distance are not valid, the respective field is filled with dashes. 3-80 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 182 Figure 3-96: Analog Navigation Symbology 3.15.3. Borders National and United States state borders are drawn if selected at all map scales. They are white if the ND background includes terrain. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-81...
  • Page 183 Table 3-19: Terrain Display on Navigation Display Color Relationship to Aircraft Altitude Based on Aircraft Altitude Color Notes # Terrain when at or below 100 Shades of Olive feet less than aircraft altitude 3-82 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 184 Note #3: Areas of water and takes precedence over other colors. Figure 3-98: Obstructions Obstructions are displayed on the ND in correct relationship to the ownship symbol using color to show relationship to aircraft altitude. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-83...
  • Page 185 Depicted in amber than 500 below aircraft Within 500’ but below Depicted in light red aircraft At or above aircraft Depicted in deep red altitude Figure 3-99: Terrain/Obstructions 3-84 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 186 (°) symbol. Otherwise, a stylized True North ) symbol is used. When panning, the nearest displayed airport, VOR, NDB, or fix within the inner range ring is highlighted with a Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-85...
  • Page 187 When selected, the ND displays conventional HSI symbology, including a selected course needle, a lateral deviation indicator, and a “TO-FROM” indicator. When the HSI is slaved to GPS/SBAS 3-86 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 188 [green]) navigation symbology with an RMI pointer format overlaid upon the HSI. When the signal is invalid, the associated pointer is not shown. When the signal is valid for VOR1 and VOR2, a bearing Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-87...
  • Page 189 This prevents a weak DME signal from disengaging the DME hold mode. When a DME channel is in hold mode, the tuned DME frequency is amber (yellow) over the associated VOR pointer in the bearing/distance display. 3-88 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 190 PFD and ND HSI display (Figure 3-106) with appropriate coloring markings. Only during a built-in-test, more than one marker beacon may be active. Marker beacons are disabled when NAV source is FMS. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 3-89...
  • Page 191 Fuel totalizer, waypoint bearing, and waypoint distance are displayed in lower right corner of the HSI as specified in § 3.7.10. Figure 3-109: HSI Fuel Totalizer/Waypoint Bearing Functions 3-90 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 192 Section 4 Reversionary Modes Section 4 Reversionary Modes Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 193 PFD Failure Mode 3 (Normal Mode) (Round dials) ................. 4-26 4.5.2. MFD Failure Mode 3 (Normal Mode) ....4-27 4.6. PFD F 4 (N ) (T ) ..4-28 AILURE ORMAL APES IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 194 ) GPS, ADC IGURE AILURE ORMAL AHRS N ) ...............4-14 ORMAL APES 4-3: PFD F 0 (N ) GPS, ADC IGURE AILURE ORMAL AHRS N ) ............4-15 ORMAL OUND IALS Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 195 , ADC N ) ........4-35 AILED ORMAL APES 4-24: PFD F 6 (N ) ADC AHRS IGURE AILURE ORMAL , GPS/SBAS N ) .......... 4-36 AILED ORMAL APES IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 196 4-30: MFD F 7 (N ) GPS/SBAS, IGURE AILURE ORMAL AHRS F ...............4-42 AILED 4-31: MFD F 7 (E ) GPS/SBAS, IGURE AILURE SSENTIAL AHRS F ) ..........4-43 AILED APES Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 197: Reversionary Modes

    To use this section, review the following table and notes to determine what feature or function is affected by one or more of the three sensors failed conditions. Examples follow with the IDU-680 displays in various configurations with a table breaking down the affected functions.
  • Page 198 Heading Indicator Horizon Mini-Map Pitch Limit Indicator Pitch Scale Highway in the Sky Terrain/Obstructions Clock Functions Waterline Symbol Waypoint Symbol Waypoint Brg/Dist Traffic Traffic Thumbnail Speed Trend Dynamic Stall Speed Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 199 Output Functions Air/Ground Output Autopilot EFIS Valid TAWS Alarm Output Transmit Enabled Warning Light Output Caution Light Output Mstr. Caut. Light Output MDA/DH Output Altitude Capture Output IAS Switch Output IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 200 Flight Path Marker grayed after one minute to indicate degraded operation. Note 15: Highway in the Sky removed after one minute. Note 16: See IDU SCC Card and Limits Requirements for activation requirements. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 201: Oat Sensor Failure Mode

    To accommodate this, MFDs must have the ability to sense when the PFD has failed and take 4-10 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 202: Eicas Screen Single-Action Reversion

    EICAS on an alternate IDU with a single action to mitigate the hazards associated with losing the primary display of EICAS. This occurs on the IDU-680 in the following manner. Press TO NORMAL/TO ESSNTL (R5) to alternate between Normal and Essential Modes on all displays.
  • Page 203 Fault detects a position failure that cannot be excluded within time-to-alert when integrity is provided by FDE; e) HPL > HAL on the final approach segment. Genesys Aerosystems EFIS does not transition to DR Navigation at this stage. A GPS Navigation solution is still presented; and Where HPL >...
  • Page 204 GPS failure results in the EFIS operating in “dead reckoning” mode. The EFIS continues to provide navigational position, groundspeed, and ground track information, based upon the last known wind, current air data, and heading. The IDU-680 PFD and MFD are affected as follows. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 205: Pfd Failure Mode 0 (Normal Mode) (Tapes)

    Section 4 Reversionary Modes 4.2. PFD Failure Mode 0 (Normal Mode) (Tapes) Figure 4-2: PFD Failure Mode 0 (Normal Mode) GPS, ADC and AHRS Normal (Tapes) 4-14 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 206: Pfd Failure Mode 0 (Normal Mode) (Round Dials)

    Section 4 Reversionary Modes 4.2.1. PFD Failure Mode 0 (Normal Mode) (Round Dials) Figure 4-3: PFD Failure Mode 0 (Normal Mode) GPS, ADC and AHRS Normal (Round Dials) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-15...

  • Page 207: Mfd Failure Mode 0 (Normal Mode)

    Section 4 Reversionary Modes 4.2.2. MFD Failure Mode 0 (Normal Mode) Figure 4-4: MFD Failure Mode 0 (Normal Mode) GPS, ADC and AHRS Normal 4-16 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 208: Pfd Failure Mode 1 (Normal Mode) (Tapes)

    Section 4 Reversionary Modes 4.3. PFD Failure Mode 1 (Normal Mode) (Tapes) Figure 4-5: PFD Failure Mode 1 (Normal Mode) GPS/SBAS Failed, (Full Sensor Status Flag) ADC and AHRS Normal (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-17...

  • Page 209: Pfd Failure Mode 1 (Essential Mode) (Tapes)

    Section 4 Reversionary Modes 4.3.1. PFD Failure Mode 1 (Essential Mode) (Tapes) Figure 4-6: PFD Failure Mode 1 (Essential Mode) GPS/SBAS Failed, ADC and AHRS Normal (Tapes) 4-18 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 210: Pfd Failure Mode 1 (Essential Mode) (Round Dials)

    Section 4 Reversionary Modes 4.3.2. PFD Failure Mode 1 (Essential Mode) (Round Dials) Figure 4-7: PFD Failure Mode 1 (Essential Mode) GPS/SBAS Failed, ADC and AHRS Normal (Round Dials) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-19...

  • Page 211: Mfd Failure Mode 1 (Normal Mode)

    Section 4 Reversionary Modes 4.3.3. MFD Failure Mode 1 (Normal Mode) Figure 4-8: MFD Failure Mode 1 (Normal Mode) GPS/SBAS Failed, (Full Sensor Status Flag) ADC and AHRS Normal 4-20 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 212: Pfd Failure Mode 2 (Normal Mode) (Tapes)

    Section 4 Reversionary Modes 4.4. PFD Failure Mode 2 (Normal Mode) (Tapes) Figure 4-9: PFD Mode 2 (Normal Mode) ADC Failed, GPS/SBAS and AHRS Normal (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-21...

  • Page 213: Pfd Failure Mode 2 (Normal Mode) (Round Dials)

    Section 4 Reversionary Modes 4.4.1. PFD Failure Mode 2 (Normal Mode) (Round Dials) Figure 4-10: PFD Mode 2 (Normal Mode) ADC Failed, GPS/SBAS and AHRS Normal (Round Dials) 4-22 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 214: Mfd Failure Mode 2 (Normal Mode)

    Section 4 Reversionary Modes 4.4.2. MFD Failure Mode 2 (Normal Mode) Figure 4-11: MFD Failure Mode 2, (Normal Mode) ADC Failed, GPS/SBAS and AHRS Normal Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-23...

  • Page 215: Mfd Failure Mode 2 (Essential Mode) (Tapes)

    Section 4 Reversionary Modes 4.4.3. MFD Failure Mode 2 (Essential Mode) (Tapes) Figure 4-12: MFD Failure Mode 2 (Essential Mode) ADC Failed, GPS/SBAS and AHRS Normal (Tapes) 4-24 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 216: Pfd Failure Mode 3 (Normal Mode) (Tapes)

    Section 4 Reversionary Modes 4.5. PFD Failure Mode 3 (Normal Mode) (Tapes) Figure 4-13: PFD Failure Mode 3 (Normal Mode) AHRS Failed, GPS/SBAS and ADC Normal (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-25...

  • Page 217: Pfd Failure Mode 3 (Normal Mode) (Round Dials)

    Section 4 Reversionary Modes 4.5.1. PFD Failure Mode 3 (Normal Mode) (Round dials) Figure 4-14: PFD Failure Mode 3 (Normal Mode) AHRS Failed, GPS/SBAS and ADC Normal (Round Dials) 4-26 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 218: Mfd Failure Mode 3 (Normal Mode)

    Section 4 Reversionary Modes 4.5.2. MFD Failure Mode 3 (Normal Mode) Figure 4-15: MFD Failure Mode 3 (Normal Mode) AHRS Failed, GPS/SBAS and ADC Normal Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-27...

  • Page 219: Pfd Failure Mode 4 (Normal Mode) (Tapes)

    Section 4 Reversionary Modes 4.6. PFD Failure Mode 4 (Normal Mode) (Tapes) Figure 4-16: PFD Failure Mode 4 (Normal Mode) GPS/SBAS and ADC Failed, AHRS Normal (Tapes) 4-28 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 220: Pfd Failure Mode 4 (Normal Mode) (Round Dials)

    Section 4 Reversionary Modes 4.6.1. PFD Failure Mode 4 (Normal Mode) (Round Dials) Figure 4-17: PFD Failure Mode 4 (Normal Mode) GPS/SBAS and ADC Failed, AHRS Normal (Round Dials) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-29...

  • Page 221: Mfd Failure Mode 4 (Normal Mode)

    Section 4 Reversionary Modes 4.6.2. MFD Failure Mode 4 (Normal Mode) Figure 4-18: MFD Failure Mode 4 (Normal Mode) GPS/SBAS and ADC Failed, AHRS Normal 4-30 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 222: Mfd Failure Mode 4 (Essential Mode) (Tapes)

    Section 4 Reversionary Modes 4.6.3. MFD Failure Mode 4 (Essential Mode) (Tapes) Figure 4-19: MFD Failure Mode 4 (Essential Mode) GPS/SBAS and ADC Failed, AHRS Normal (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-31...

  • Page 223: Pfd Failure Mode 5 (Normal Mode) (Tapes)

    Section 4 Reversionary Modes 4.7. PFD Failure Mode 5 (Normal Mode) (Tapes) Figure 4-20: PFD Failure Mode 5 (Normal Mode) GPS/SBAS and AHRS Failed, ADC Normal (Tapes) 4-32 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 224: Pfd Failure Mode 5 (Normal Mode) (Round Dials)

    Section 4 Reversionary Modes 4.7.1. PFD Failure Mode 5 (Normal Mode) (Round Dials) Figure 4-21: PFD Failure Mode 5 (Normal Mode) GPS/SBAS and AHRS Failed, ADC Normal (Round Dials) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-33...

  • Page 225: Mfd Failure Mode 5 (Normal Mode)

    Section 4 Reversionary Modes 4.7.2. MFD Failure Mode 5 (Normal Mode) Figure 4-22: MFD Failure Mode 5 (Normal Mode) GPS/SBAS and AHRS Failed, ADC Normal 4-34 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 226: Mfd Failure Mode 5 (Essential Mode) (Tapes)

    Section 4 Reversionary Modes 4.7.3. MFD Failure Mode 5 (Essential Mode) (Tapes) Figure 4-23: MFD Failure Mode 5 (Essential Mode) GPS/SBAS and AHRS Failed, ADC Normal (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-35...

  • Page 227: Pfd Failure Mode 6 (Normal Mode) (Tapes)

    Section 4 Reversionary Modes 4.8. PFD Failure Mode 6 (Normal Mode) (Tapes) Figure 4-24: PFD Failure Mode 6 (Normal Mode) ADC and AHRS Failed, GPS/SBAS Normal (Tapes) 4-36 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 228: Pfd Failure Mode 6 (Normal Mode) (Round Dials)

    Section 4 Reversionary Modes 4.8.1. PFD Failure Mode 6 (Normal Mode) (Round Dials) Figure 4-25: PFD Failure Mode 6 (Normal Mode) ADC and AHRS Failed, GPS/SBAS Normal (Round Dials) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-37...

  • Page 229: Mfd Failure Mode 6 (Normal Mode)

    Section 4 Reversionary Modes 4.8.2. MFD Failure Mode 6 (Normal Mode) Figure 4-26: MFD Failure Mode 6 (Normal Mode) ADC and AHRS Failed, GPS/SBAS Normal 4-38 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 230: Mfd Failure Mode 6 (Essential Mode) (Tapes)

    Section 4 Reversionary Modes 4.8.3. MFD Failure Mode 6 (Essential Mode) (Tapes) Figure 4-27: MFD Failure Mode 6 (Essential Mode) ADC and AHRS Failed, GPS/SBAS Normal (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-39...

  • Page 231: Pfd Failure Mode 7 (Normal Mode) (Tapes)

    Section 4 Reversionary Modes 4.9. PFD Failure Mode 7 (Normal Mode) (Tapes) Figure 4-28: PFD Failure Mode 7 (Normal Mode) GPS/SBAS, ADC and AHRS Failed (Tapes) 4-40 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 232: Pfd Failure Mode 7 (Normal Mode) (Round Dials)

    Section 4 Reversionary Modes 4.9.1. PFD Failure Mode 7 (Normal Mode) (Round Dials) Figure 4-29: PFD Failure Mode 7 (Normal Mode) GPS/SBAS, ADC and AHRS Failed (Round Dials) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-41...

  • Page 233: Mfd Failure Mode 7 (Normal Mode)

    Section 4 Reversionary Modes 4.9.2. MFD Failure Mode 7 (Normal Mode) Figure 4-30: MFD Failure Mode 7 (Normal Mode) GPS/SBAS, ADC and AHRS Failed 4-42 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 234: Mfd Failure Mode 7 (Essential Mode) (Tapes)

    Section 4 Reversionary Modes 4.9.3. MFD Failure Mode 7 (Essential Mode) (Tapes) Figure 4-31: MFD Failure Mode 7 (Essential Mode) GPS/SBAS, ADC and AHRS Failed (Tapes) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 4-43...
  • Page 235 Section 5 Menu Functions and Procedures Section 5 Menu Functions and Step- By-Step Procedures Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 236 5.3..........5-10 UNCTION YPES 5.4............5-11 EVEL 5.4.1. IDU-680 PFD Normal Mode Top-Level Menu .. 5-11 5.4.2. IDU-680 MFD Normal Mode Top-Level Menu . 5-12 5.4.3. IDU-680 PFD or MFD Essential Mode Top-Level Menu ................. 5-13 5.4.4. Top-Level Menu Option Descriptions ....5-13 ...
  • Page 237 5.10.17. RAIM Prediction (Step-By-Step) .......5-40 5.11. (ACTV) M ......5-42 CTIVE LIGHT 5.11.1. Active Flight Plan (ACTV) Menu Options ..5-43 5.11.2. Active Flight Plan (ACTV) Menu Options (Step-By- Step) ................5-47 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 238 5.20.1. PFD Declutter (DCLTR) Menu (Step-By-Step) 5-72 5.21. PFD A ..........5-72 LTIMETER 5.21.1. PFD Altimeter Menu (Step-By-Step) ....5-74 5.22. MFD F (FAULTS) M ....... 5-75 AULT ISPLAY IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 239 5-10: EICAS E ........5-27 IGURE XCEEDANCE 5-11: E CAS M ..........5-27 IGURE XPAND 5-12: IDU-680 I ..IGURE NPUT ONTROLS FOR OWER EVEL ENUS ....................5-28 5-13: F ..........5-29 IGURE LIGHT Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 240 IGURE 5-32: MFD S ........5-82 IGURE YMBOL ECLUTTER 5-33: MFD ND P (FORMAT) M ..... 5-84 IGURE ORMAT 5-34: MFD HSI P (PTRS) M ......5-87 IGURE OINTER IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 241: Menu Functions

     encoders ( , and ). The encoder in the lower left corner of the IDU-680 is only used for adjusting screen and button brightness and cannot be used for menu functions. It is always labeled DIM.   ...
  • Page 242 Otherwise, they are only synchronized onside. These parameters are FMS parameters and allow the pilot and co-pilot FMSs to be operated independently when crosslink is inhibited. Active Flight Plan Parameters IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 243 Menu parameters The following menu parameters are independent between displays. These are used to support non-PFD display options to give the pilot maximum MFD operating flexibility. Note that some Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 244: Menu Function Types

    680 MFD areas 5.3. Menu Function Types On the IDU-680, only soft menu functions are used (even at the top- level) and are annunciated in a dedicated, blacked-out area in the screen margins. Soft menu function tiles indicate further menu levels with a filled triangle (with further levels) or hollow triangle (without further levels) pointing to the associated button.

  • Page 245: Top-Level Menu

    Section 5 Menu Functions and Procedures 5.4. Top-Level Menu On the IDU-680, the top-level menu consists of soft menu options along with option labels for the rotary encoders. 5.4.1. IDU-680 PFD Normal Mode Top-Level Menu Flight Plan Menu First Level Menu...

  • Page 246: Mfd Normal Mode Top-Level Menu

    · Turn (EICAS Page on Bottom Area) – Scroll CAS box (if applicable) AR Tune Menu (only if Audio/ Radio devices configured) Figure 5-3: IDU-680 MFD Normal Mode Top-Level Menu 5-12 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 247: Idu-680 Pfd Or Mfd Essential Mode Top-Level Menu

    Radio devices configured) CAS box (if applicable) Heading Bug Menu Altitude Select Menu ALT SEL Figure 5-4: IDU-680 PFD or MFD Essential Mode Top-Level Menu 5.4.4. Top-Level Menu Option Descriptions 1) FPL (L1): Flight plan menu. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 248: 11) #3 Encoder

    CCW to decrease scale). c) On an MFD (IDUs other than #1) operating in Normal Mode, if the top area is showing a video page, scroll the encoder 5-14 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 249 4) On a PFD or MFD operating in Normal Mode, if the bottom area is showing an Audio/Radio page, scroll the encoder to change the selected Audio/Radio device Volume and or Mute function if applicable. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-15...

  • Page 250: Top-Level Menu Automatic Pop-Up Function

    Press to deactivate heading bug sub-mode and resume guidance to active flight plan path. 5-16 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 251 VNAV appears when VNAV guidance is valid, selected altitude sub-mode is active, and the system is integrated with an analog autopilot. Press to deactivate selected altitude sub-mode and resume Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-17...
  • Page 252 Note 1: Designated buttons used when the function is tied to a page in the top area. Note 2: Designated buttons used when the function is tied to a page in the bottom area or is “Transmit Enabled.” 5-18 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 253: First Page (Pfd)

    Figure 5-5: First Page PFD The top area of IDU #1 is fixed to the PFD page. Select Essential Mode on other IDUs to show the PFD page in the top area. IDU-680 PFD page first-level options are shown adjacent to the top eight pushbuttons.

  • Page 254: First Level (Pfd Idu#1) Normal Mode

    (“EXCD” with filled AR Tune Menu (only if Audio/ pointer) Radio devices configured) Expand CAS menu. Only EXPAND CAS.. shown if message count exceeds 11 Figure 5-6: First Level PFD 5-20 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 255: Pfd Page First-Level Option Descriptions

    Crossfill is enabled by releasing (OFF) this switch. The location and number of crossfill inhibit switches in a cockpit varies by installation. Usually a single crossfill switch Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-21...

  • Page 256: First Level (Mfd)

    2) SOURCE (L2): Activates PFD source selection menu option. 3) DESIG (L3): Creates a user waypoint at current aircraft location. In addition, if pressed on an IDU-680 with an ND page operating in panning mode, creates a user waypoint at the panning location.
  • Page 257 AR Tune Menu (only if Audio/ Radio devices configured) Expand CAS menu. Only EXPAND CAS.. shown if message count exceeds 11 Figure 5-7: First Level MFD Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-23...

  • Page 258: First Level (Mfd Idu Other Than #1) Normal Mode

    AR Tune Menu (only if Audio/ pointer) Radio devices configured) Expand CAS menu. Only EXPAND CAS.. shown if message count exceeds 11 Figure 5-8: First Level (MFD IDU other than #1) Normal Mode 5-24 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 259: Mfd Page First-Level Option Descriptions

    11 active CAS messages. 5.6.3. IDU-680 EICAS Page First-Level in Essential Mode The bottom area of the IDU-680 shows the EICAS page. In Normal Mode on IDUs other than #1, the EICAS page may be shown in the Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 260 Section 5 Menu Functions and Procedures top area (a full-screen EICAS page using both the top and bottom areas is considered a top area page). IDU-680 EICAS page first- level options are shown adjacent to the area in which the EICAS page resides.

  • Page 261: Eicas Page First-Level Option Descriptions

    EXPAND CAS.. count exceeds 11. In the Expand CAS  menu, is dedicated to scroll the CAS display box. SCROLL CAS Figure 5-11: Expand CAS Menu Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-27...

  • Page 262: Expand Cas Menu

    4) This example indicates there is one message above and four below. 5.9. Lower-Level Menus (Below First-Level)    Figure 5-12: IDU-680 Input Controls for Lower-Level Menus 5-28 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 263: Flight Plan (Fpl) Menu

    Section 5 Menu Functions and Procedures The pushbuttons and rotary encoders on IDU-680, which control the top-level and first-level menus, called lower-level menus, are described in this section. In the following diagrams, button and encoder numbers are interpreted according to the following view.

  • Page 264: 5.10.2. Pfd Page Shown On Idu

    IDUs controls and disables the menu operations described in this document (other than the automatic IDU-680 EICAS page reversions described above). Normal menu operation and IDU control function are restored upon: 1) Exiting the Flight Planner page; or 2) Automatic reversion of the IDU to the PFD or Essential Mode.

  • Page 265: To Create An Overfly User Waypoint (Step-By-Step)

    2) Scroll  to desired flight plan and push to enter. 5.10.6. Flight Plan (FPL) Menu Create-Edit (Step-By-Step) 1) Press FPL (L1).  2) Scroll to CREATE- EDIT.. and push to enter. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-31...

  • Page 266: Flight Plan (Fpl) Menu Selection (Step-By-Step)

    “KBDR” appears as the first waypoint, continue with adding more waypoints. 3) If necessary, scroll up to KBDR. 4) Press INFO (L7) and view information about selected waypoint. 5-32 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 267: Flight Plan (Fpl) Creation (Step-By-Step)

    FLIGHT PLAN and push to enter.  4) Scroll to desired saved flight plan and push to enter. 5) Press EXIT (R1) if no other action is necessary. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-33...

  • Page 268: Edit Flight Plan (Step-By-Step)

    7) Press EXIT (R1), if no other action is necessary. 5.10.11. Reverse Flight Plan (Step-By-Step) 1) Press FPL (L1).  2) Scroll to CREATE- EDIT.. and push to enter. 5-34 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 269: Delete Flight Plan (Step-By-Step)

    EXIT (R1). 5.10.13. Create User Waypoint (LAT-LON) (Step-By- Step) User waypoints may be created with three methods: 1) Latitude and Longitude 3) Overfly (Designate) 2) Radial and Distance Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-35...
  • Page 270 In Flight: Preloaded with “OFF” value. If desired, specify the approach bearing to the user waypoint in degrees 1°- 360°. “OFF” value disables VFR approaches to the user waypoint. 5-36 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 271 If multiple results appear from the search, a selection list appears. INFO (R6) appears to verify each waypoint information. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-37...

  • Page 272: Edit User Waypoint (Step-By-Step)

    BACK (L1) and continue to the end of all character spaces. 6) If necessary, select another USR WPT to edit or press EXIT (R1) to save changes. 5-38 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 273: Delete User Waypoint (Step-By-Step)

    2) Open a flight plan which uses the user waypoint 3) Delete the existing waypoint from the flight plan 4) Save and exit 5) Reload the flight plan if it was in use. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-39...

  • Page 274: Raim Prediction (Step-By-Step)

    PREDICTION and push to enter. SEE NOTE BELOW. 4) If another RAIM Prediction is necessary, press START OVER (R6) to start again or press EXIT (R1) to exit. 5-40 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 275 “OK” or “XX” for ETA ± in 5-minute increments. Once a prediction is complete, START OVER (R6) appears for the pilot to perform another prediction without having to exit the RAIM Prediction screen. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-41...

  • Page 276: Active Flight Plan (Actv) Menu

    Runway List * Insert selected Insert selected Insert selected STAR approach Figure 5-14: Active Flight Plan Main Menu See Section 7 IFR Procedures for Active Flight Plan description. 5-42 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 277 Various options appear at the same menu level as the nav log selection list. These options allow various modifications to be made to the active flight plan as follows: Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-43...
  • Page 278 If there is no result from the search, the pilot is re-prompted to enter an 5-44 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 279 If there are no results (i.e., no user waypoints within 240NM), NO RESULTS is displayed. Otherwise, a Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-45...
  • Page 280 The tile also does not appear when the highlighted waypoint is suppressed or when the highlighted position is one position past the end of the active flight plan. 5-46 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 281: Active Flight Plan (Actv) Menu Options (Step-By-Step)

    2) Press ACTV (L2) to view active flight plan.  3) Scroll to desired waypoint. Push to enter.  4) As one option, push to enter a VNAV setting. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-47...

  • Page 282: Active Flight Plan (Actv) Options Nrst Menu Option (Step-By-Step)

    NRST VOR (L3), NRST NDB (L4), NRST FIX (R2), NRST USR (R3), or AIRWAY (R4) to view  applicable list. Scroll to desired selection. Push to insert into active flight plan. 5-48 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 283: Information (Info) Menu

    If there are multiple results from the search, a selection list with matching identifiers is presented to allow the pilot to select the desired Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-49...
  • Page 284 WX LGND (L2) appears to allow the display of an airport graphical METAR legend and EXPND WX (L3) appears to allow the display of textual METAR and TAF data for the airport. 5-50 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 285: Information (Info) Menu (Step-By-Step)

    (depending upon HSI source) to the inbound course or, if the inbound course cannot be determined, to aircraft heading. When HSI source is FMS, OBS AUTO/OBS MAN (R4) toggles between automatic and manual OBS settings. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-51...
  • Page 286 0.10NM and 15NM as follows: 1) 0.01NM increments between RNP 0.10 and RNP 0.3 2) 0.1NM increments between RNP 0.3 and RNP 2 3) 1NM increments between RNP 2 and RNP 15 5-52 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 287: Omnibearing Selector (Obs) Menu (Step-By-Step)

    OBS MANUAL (R4). 3) When the OBS is set to FMS, VLOC1 or VLOC2,  scroll to select new OBS course. 4) To select Manual RNP press OBS (L4). Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-53...

  • Page 288: Heading Bug (Hdg) Menu

    The heading bug menu allows the pilot to set the heading bug in increments of 1°, synchronize the heading bug to current heading, or turn off the heading bug. 5-54 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 289: Heading Bug (Hdg) Menu (Step-By-Step)

    The selection lists for airports contains only airports with runway length greater than or equal to the minimum runway length setting when the system was configured during installation. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-55...
  • Page 290 It is up to the pilot to swap frequencies to the active position in the applicable radio. If Garmin SL-30/40 radios are enabled in the EFIS limits, only TO COM (R2) and TO NAV (R2) appear. 5-56 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 291 If there are two NAV radios installed, the default sensor for the selecting side controls which source is used. The source for the other side does not change. 6) Connected NAV radios are remote tuned to ILS frequency. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-57...

  • Page 292: Nearest (Nrst) Menu (Step-By-Step)

    The selection must be an ILS.  4) Scroll to desired airport and ILS approach. Push to select and enter.  5) Push to confirm and activate ILS. 5-58 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 293: Direct Menu

    * Or nearest airport if no active waypoint Single Match? INFO.. Match List Create and activate new flight plan from present position to selected waypoint Figure 5-21: Direct Menu Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-59...

  • Page 294: Direct Menu (Step-By-Step)

     4) Or scroll to begin entering new identifier. 5) After creating new  identifier, scroll to the end and push to enter 5-60 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 295: Time (Time) Menu

    Shortcut buttons to quickly add or decrement by five-minute increments are provided at this level. After entering a start time, the pilot may either start the Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-61...

  • Page 296: Time (Time) Menu (Step-By-Step)

    UTC OFFSET... Push to enter.  7) Scroll to desired offset value. Push to enter. 8) Local time now appears where Zulu time was previously. 5-62 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 297: Pfd Source (Source) Menu

    Selects #2 EICAS Sensors and EICAS2 (g) Only available if selected AHRS is a CFS/ Deselects #1 EICAS Sensors Genesys ADAHRS that is in DG mode and GPS1 Selects GPS1 and Deselects AHRS slew discrete inputs for the selected GPS2 AHRS are not configured.

  • Page 298: Pfd Page First-Level Source Selection (Step-By-Step)

    1 knot indicated airspeed. On the low end, airspeed bug settings are no less than 60KIAS and no greater than V 5-64 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 299 VSI, turning the VSI bug off, or setting the VSI bug in increments of 100 feet per minute. NOTE: The airspeed bug and VSI bug are mutually exclusive, and therefore, selecting one turns off the other. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-65...
  • Page 300 Enter angle Press – Set selected altitude Turn – Change climb angle in 0.1° increments VNAV CDA.. Press – Set selected angle Figure 5-25: PFD Bug (BUGS) Menu 5-66 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 301: Pfd Bug (Bugs) Menu (Step-By-Step)

    5.19.1. PFD Bug (BUGS) Menu (Step-By-Step) 1) Press MENU (R1) then BUGS (R2) to enter the Bugs menu, or use Remote Bugs Panel if equipped as referenced in RBP appendix. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-67...
  • Page 302 PFI area below the FPM or next to analog AGL display. 9) If VNAV CDA (R4) is  selected, scroll select DCND.. or CLIMB.. and push to enter. 5-68 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 303 V speed and push to enter. , and V symbols automatically declutter, when respective value is exceeded by 40 knots or when above 2000 feet AGL. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-69...

  • Page 304: Pfd Declutter (Dcltr) Menu

    Normal PFD Overlay Turning both off disables terrain Note that “SVS TAWS” is labeled “SVS ADVNCD” when TAWS is Accept changes not enabled. Figure 5-27: PFD Declutter (DCLTR) Menu 5-70 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 305 (i.e., it is not possible to turn both off), because the display of the flight directors when integrated with the Intelliflight 1950 is controlled through the mode control panel. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-71...

  • Page 306: Pfd Declutter (Dcltr) Menu (Step-By-Step)

    The following definitions: a) QFE: Barometric setting resulting in the altimeter displaying height above a reference elevation (e.g., airport or runway threshold). 5-72 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 307 * Displayed if current transition altitude is Turn – Change altitude in not 18,000 ft 1000 ft increments Enter altitude Press – Set selected altitude Figure 5-28: PFD Altimeter Menu Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-73...

  • Page 308: Pfd Altimeter Menu (Step-By-Step)

    QNH and push to enter. 3) Crosscheck proper QNH under altitude indication. 4) Press BARO (R2) again and STD (R4) to reset  QNH to 29.92. Push to enter. 5-74 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 309: Mfd Fault Display (Faults) Menu

    1) GPS/SBAS loss of navigation due to absence of power (GPS PWR.) 2) GPS/SBAS loss of navigation due to probable equipment failure (GPS EQPMNT.) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-75...
  • Page 310 12) GPS/SBAS loss of navigation due to insufficient number of SBAS HEALTHY satellites (SBAS HLTH.) a) An Attitude or Range Fault Condition exists. b) A Control Fault Condition exists. 5-76 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 311 (WXR FAULT X) reflects any one of the following conditions is true: a) A Cooling Fault Condition exists. b) For weather radar types ARINC 708-6 or Collins 800/840, a Display or Control Bus Fault Condition exists. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-77...

  • Page 312: Pfd Or Mfd Fault Display (Faults) Menu (Step-By-Step)

    5.22.1. PFD or MFD Fault Display (FAULTS) Menu (Step-By- Step) 1) Press MENU (R1) then FAULTS (L5) to view the faults menu on PFD. 2) View status of GPS and equipment parameters. 5-78 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 313: Mfd Fuel Totalizer Quantity Setting (Set Fuel) Menu

    5.24. MFD Page (PAGE) Menu PAGE menu allows the pilot to select which MFD page to display: 1) MAP: Shows the ND page. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-79...
  • Page 314 AUDIO/RADIO defined. Text for tile page comes from OASIS page name parameter. (h) IDU-680 only, shown if Audio Radio devices are configured Figure 5-31: MFD Page (PAGE) 5-80 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 315: Mfd Page (Page) Menu (Step-By-Step)

    Push and scroll HSI. Push to enter in the bottom area. 5.24.2. MFD NAV LOG ND Page (Step-By-Step)   1) Push and scroll to NAV LOG. Push to enter. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-81...

  • Page 316: Mfd Nd Page Ormat (Format) Menu

    Figure 5-32: MFD Symbol Declutter 5) Turning on VFR airports also turns on large airports and IFR airports. Turning on IFR airports also turns on large airports. 5-82 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 317 (if WX-500 option is enabled); m) display of terrain; n) display of traffic (if traffic option is enabled); and o) display of weather radar (if weather radar option is enabled). Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-83...
  • Page 318 Press – Switch to PFD (e) Shown if optional weather Right Turn – Increase range radar installed. Left Turn – Decrease range Figure 5-33: MFD ND Page Format (FORMAT) Menu 5-84 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 319: Mfd Nd Page Format (Step-By-Step)

    PAN ON and push to enter. 7) To turn off pan mode, either press PN OFF (L5) or MENU (R1) and  FORMAT (R8). Scroll to PAN OFF and push to enter. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-85...

  • Page 320: Adding Lat/Lon To Mfd Nd Page

    Upon selecting the HSI pointers menu when in the HSI page, an option list appears for the pilot to individually select: 1) display of ADF1 pointer (if ADF symbology is enabled); 5-86 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 321: Mfd Hsi Pointer (Ptrs) Menu (Step-By-Step)

    2) Scroll to either PTR ADF, PTR NAV1 or PTR NAV2 and push to place check mark, then press EXIT (R1) or scroll to DONE and push to enter. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 5-87...
  • Page 322 Section 6 Quick Start Tutorial Section 6 Quick Start Tutorial Quick Reference Guide (DOC 64-000097-080E) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 323 For the purpose of flight planning, etc., press any button override this countdown. The encoders at the bottom bezel    numbered 1-3 from the right.  Scroll adjust heading bug setting. IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 324 A direct route to the active waypoint is activated and appears as magenta tethered balloon on the PFI area. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 325 Meter is located below the airspeed indicator. FMS/VLOC CDI is located on the bottom. The VSI is located below the altimeter. Analog navigation symbology on MFD HSI shown on top area. IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 326 PFD on the top view and EICAS on the bottom view. On the MFD, press (R5) to change displays to EICAS page (if enabled) on top and bottom view. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 327 Section 6 Quick Start Tutorial When EICAS is not enabled, press (R5) to restore MFD on top and bottom areas. IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 328 5) Edit waypoint and press SAVE (R8) and push or press EXIT (R1) to exit Flight Planner. Create a User Waypoint on PFD or MFD 1) Press MENU (R1). 2) Press DESIG (L3). Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 329 OBS SYNC (R3) and push to enter. 4) If HSI source is NAV VLOC1 (L3) or NAV VLOC2 (L4) scroll  to desired course (OBS:XXX° (XXX°)) and push to enter. IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 330 Change Runway on IFR Approach on PFD or MFD 1) Press ACTV (L2).  2) Scroll to destination airport and push to enter. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 331 3) When the pilot and co-pilot systems are not synchronized, press MENU (R1) then XFILL SYNC (L1) to synchronize the pilot and co-pilot active flight plan parameters to the other system from where the button press occurred. 6-10 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 332 Section 7 IFR Procedures Section 7 IFR Procedures Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 333 VTF VFR Approach .......... 7-30 7.8. 7-30 ISSED PPROACH AND EPARTURE EFINITION 7.9....... 7-31 OSS OF AVIGATION ONITORING 7.10............7-32 ISCONTINUITIES 7.11....7-32 ELECTION OF AN NSTRUMENT ROCEDURE IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 334 OURSE PPROACH 7-14: RNAV (GPS) I LPV M IGURE NSTRUMENT PPROACH TO INIMA ....................7-45 7-15: NRST ILS I ......7-48 IGURE NSTRUMENT PPROACH 7-16: VOR/DME I ......7-51 IGURE NSTRUMENT PPROACH Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 335: Active Flight Plan

    To add a waypoint to the end of the active flight plan, scroll through each waypoint of the flight plan to one position past the end. If not, the application makes the selected waypoint active. Otherwise, an option list is presented. IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 336 NO RADIUS: Force the turn radius at the waypoint to be zero. This forces the inbound course and outbound course to go directly to and from the waypoint regardless of the amount of course change required. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 337 STAR is created. Activating a STAR automatically deletes any pre-existing STAR. If there is a pre- existing approach (IFR or VFR) to the airport, the STAR waypoints are inserted prior to the approach waypoints. IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 338: Ifr Procedures

    7.3. Overview of Approaches This Genesys Aerosystems EFIS provides 3-D GPS precision and non-precision instrument approach guidance using a system integral TSO C146c BETA 3 GPS receiver. With GPS and augmented GPS with SBAS (Satellite Based Augmentation System) commonly referred to as WAAS (Wide Area Augmentation System).
  • Page 339 LNAV procedures due to the narrower obstacle clearance surface. The Genesys Aerosystems EFIS guides the pilot through every step of the approach procedure with Highway in the Sky 3-D symbology. The system defines a desired flight path based upon the active flight plan.

  • Page 340: Highway In The Sky (Skyway)

    When the active route is in view, up to five boxes are shown with the dimensions being a constant 400 feet wide (±200 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 341 ACTV menu. VNAV altitudes for waypoints without a navigation database or manually input VNAV altitude are computed using “look-ahead” rules. When “look-ahead” finds a further VNAV altitude constraint 7-10 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 342 Climb guidance is depicted in Figure 7-2, Figure 7-3, and Figure 7-4. Level-Off Point VNAV Altitude Active Depicted Waypoint Flight Path Dynamic Climb Angle Figure 7-2: Highway in the Sky (Aircraft Referenced) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-11...
  • Page 343 VNAV altitude. On the final approach segment of an IFR approach, descent angle and VNAV waypoint are defined as follows. 7-12 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 344 The climb paradigm compensates for an aircraft's ability to climb more steeply than specified and warns of being below a desired climb gradient when Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-13...

  • Page 345: Waypoint Sequencing

    Radius for turning segments (other than DME arc or Radius to a Fix segments) is calculated with the parameter speed determined as follows: 7-14 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 346: Fly-Over Waypoints

    These waypoints are type Fly-Over with Defined Entry Heading: 1) Exit from holding pattern; 2) Exit from procedure turn; 3) Entry into holding pattern; Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-15...

  • Page 347: Fly-By Waypoints

    Manual Termination, etc. (See Section 9 Appendix for table of ARINC-424 Path-Terminator Leg Types.) 7.3.4. Fly-By Waypoints These waypoints are type Fly-Over with Defined Exit Heading: 1) Entry into procedure turn; and 7-16 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 348 Leg, WGS-84 geodesic or arc path Fly-By Fly-By Arc or from entry to exit turns. Radius to a Fix 1st half of fly-by turn at exit waypoint. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-17...
  • Page 349 WGS-84 geodesic or arc path Fly-By Entry from entry to exit turns. Heading 1st half of fly-by turn at exit waypoint. Turn from entry heading after Fly-Over Fly-Over entry waypoint. Defined Defined 7-18 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 350 Defined Defined Pattern is the heading required to get Entry Entry to entry of inbound turn. Heading Heading WGS-84 geodesic path to entry of inbound turn. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-19...

  • Page 351: Direct-To

    Where the selected “To” fix is in the active flight plan, the required transition is created as follows: 1) A phantom waypoint is created at the current aircraft location. 7-20 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 352: Magnetic Course

    True North with drift free heading. The preferred way to operate in areas where navigation is done relative to True North. (See Section 9 Appendix for limitations on Earth’s magnetic flux horizontal field.) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-21...

  • Page 353: Gps Altitude

    An exception to this occurs where the parallel offset ends. In 7-22 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 354 A parallel offset entry waypoint (“PTK+”) is shown in Figure 7-8. Figure 7-8: Parallel Offset PTK+ Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-23...
  • Page 355 Figure 7-9: Parallel Offset PTK- 7-24 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 356: Default Gps/Sbas Navigation Modes

    VTF IFR Approach has been selected; and VTF Approach (LNAV, within 30NM of the active runway*; and LNAV/VNAV, LP or LPV) FAWP is active waypoint*; and Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-25...
  • Page 357 30NM of the departure airport, arrival airport, or runway. Not in Departure, Approach, nor Terminal Enroute Modes. 7-26 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 358: Gps/Sbas Cdi Scale

    7.7. Approach Type Selection The IDU selects the approach type (LNAV, LNAV/VNAV, LP, or LPV) when entering approach mode with the following order of precedence and prerequisites: Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-27...
  • Page 359 If a Final Approach Segment data block exists, it passes CRC check; and d) Horizontal alert limit of 556m (.3NM) is predicted to be supported. 7-28 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 360: Approach Path Definition

    IDU indicates a VTF IFR approach has been selected (mode annunciation “VECTORS”) to indicate guidance is not relative to a published approach path, and TERPS clearances are not assured. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-29...

  • Page 361: Vtf Vfr Approach

    MAWP. If a missed approach is not initiated prior to crossing the MAWP, the IDU switches to FROM mode at the MAWP and continues on the same course. 7-30 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 362: Loss Of Navigation Monitoring

    3) 1NM increments between RNP 2 and RNP 15 The aircraft is equipped for these individual levels of RNP, but may not be capable due to limited satellite coverage. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-31...

  • Page 363: Discontinuities

    1) STAR 2) ILS Instrument Approach 3) LOC BC Instrument Approach 4) RNAV GPS Instrument Approach to LPV minima 5) NRST ILS Instrument Approach 6) VOR DME Instrument Approach 7-32 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 364 Figure 7-11: Standard Terminal Arrival Route (STAR) If the selected waypoint is an airport with a published STAR, this option is available from a selection list of available STARs, Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-33...
  • Page 365 8) Once a VNAV altitude has been entered for any waypoint within the STAR, subsequent waypoints follow with altitude, bearing, distance, and ETE/ETA values. 9) View STAR on MAP page. 7-34 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 366 SARDI intersection on course left turns with 5- mile legs. 12) Course guidance and turn anticipation are provided on PFD with HITS boxes, which connect waypoints throughout the procedure. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-35...
  • Page 367 All approach operations typically begin with the same basic steps. This example selects the ILS or LOC RWY 34 at Westchester County (HPN). Figure 7-12: ILS Instrument Approach 7-36 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 368 ATC clears to descent to 3000’.  to select 3000’ Scroll and observe VNAV (L6) appear for quick return to VNAV profile. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-37...
  • Page 369 FAF when ATC issues clearance for the approach. 10) Inside the FAF with indicating automatic waypoint sequencing is suspended until ARM (L6) is pressed. 7-38 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 370 VOC1 and glideslope appearing on both top and bottom areas. 12) MFD with EICAS shown on top in NORMAL mode with MAP on bottom area for orientation purposes. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-39...
  • Page 371 13) Over the middle marker and just below DH and below the glideslope. 14) During the missed approach with automatic navigation source switched to FMS1 and 0.3NM FSD. 7-40 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 372 Section 7 IFR Procedures 7.11.3. LOC Back Course Instrument Approach (Step-By-Step) Figure 7-13: LOC Back Course Approach Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-41...
  • Page 373 MENU (R1), BUGS (R2),  MINS (R3), scroll MIN ALT.., and push to  enter. Scroll to set desired minimum altitude and push to enter or use RBP if equipped. 7-42 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 374 105° beyond the front course bearing of 120°, HSI indicates a BC1 120° setting. Back course sensing is automatic with reversal of CDI presentation for natural tracking guidance. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-43...
  • Page 375 MAWP or press MISS (L5) at any time. 12) During the missed approach procedure, the navigation source automatically switches to FMS guidance. 7-44 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 376 Section 7 IFR Procedures 7.11.4. RNAV (GPS) Instrument Approach to LPV Minima (Step- By-Step) Figure 7-14: RNAV (GPS) Instrument Approach to LPV Minima Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-45...
  • Page 377 Top of Descent point within instrument approach procedure. 6) Active leg magenta line and next leg in white. 7) Inside FAF, press ARM (L6) prior to step down FIX, HOLUS. 7-46 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 378 LPV vertical profile based on GPS/SBAS. 10) Obstructions appear on PFD and MAP page. 11) Flight path marker lined up on the active runway on glidepath approaching minimums. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-47...
  • Page 379 Section 7 IFR Procedures 7.11.5. NRST ILS Instrument Approach (Step-By-Step) Figure 7-15: NRST ILS Instrument Approach 7-48 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 380 5) HSI source is switched as follows: ILS frequency is automatically transmitted to NAV#1 in standby position. 6) EFIS changes to LOC1, and VDI indicates source of glideslope GS1. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-49...
  • Page 381 FMS1. Dashed magenta and white lines lead the flight to the holding waypoint.  10) Scroll to scale the MAP for desired view of published missed approach procedure. 7-50 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 382 Section 7 IFR Procedures 7.11.6. VOR/DME Instrument Approach (Step-By-Step) Figure 7-16: VOR/DME Instrument Approach Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-51...
  • Page 383  5) Scroll to view procedure with desired MAP scale. 6) Minimums are set to 420’ as the aircraft tracks along final approach course from LADDY. 7-52 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 384 MAP is not armed, and auto waypoint sequencing is not suspended due to stepdown fix ahead. 8) PFD shows auto waypoint sequencing is suspended after passing stepdown fix GOLDY. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 7-53...
  • Page 385 If the lateral integrity limit is exceeded on an LP approach, a missed approach is necessary, since the lateral alarm limit may not be reset while the approach is active. 7-54 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 386 Section 8 Terrain Awareness Warning System Section 8 Terrain Awareness Warning System All Airplane TAWS Classes Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 387 External Sensors and Switches ....... 8-20 8.13. TAWS Basic Parameter Determination ....8-22 8.14. TAWS Automatic Inhibit Functions (Normal Operation) .................. 8-26 8.14.1. TAWS Automatic Inhibit Functions (Abnormal Operation) ................8-27 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 388 8-14: PFD SVS TAWS O ........8-31 IGURE PTION 8-15: PFD SVS TAWS O ..8-32 IGURE PTION AND BSTRUCTIONS 8-16: PFD O ........8-33 IGURE BSTRUCTION AUTION 8-17: PFD O .........8-34 IGURE BSTRUCTION ARNING Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 389: Taws B (Terrain Awareness And Warning System)

    (GPWS Mode 5): Alerts when an excessive downward glideslope deviation is detected on the final approach segment of an ILS approach. 9) 500 foot Wake-up Call: A single aural callout when descending through 500 feet AGL. IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 390: Terrain Display

    The display of terrain on the PFD and ND are described in Sections 3 Display Symbology and 5 Menu Functions and Step-By-Step Procedures of this pilot guide where applicable. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 391 Forward Looking Terrain Alert Function Figure 8-2: FLTA INHBT FLTA function uses the following to alert to hazardous terrain or obstructions within a search envelope in front of the aircraft: IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 392: Flta Modes

    (this is near the liftoff point). Departure Mode ends upon climbing through 1500 feet above or traveling more than 6NM from the reference point. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 393 3500’ 3500’ Enroute Mode Enroute Enroute Mode Mode 1900’ Terminal FLTA Terminal Mode proach Inhibit proach Mode Mode Mode 15NM 15NM Reference Point Figure 8-4: FLTA INHBT Mode Areas IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 394 Class C: 200 feet Terminal Mode Class A & B: 300 feet Descending RTC: Class C: 200 feet Approach Mode 100 feet Descending RTC: Departure Mode 100 feet Descending RTC: Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 395 RTC value used by the system. The increase in descending flight RTC is based upon a three-second pilot reaction time and VSI leading according to the level-off rule parameter. 8-10 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 396 TAWS Inhibit is not enabled. TAWS Inhibit prevents terrain from being automatically enabled on the navigation display. In addition, when an FLTA warning is initiated or upgraded, an automatic popup mode is engaged as follows: Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 8-11...
  • Page 397 Premature Descent Alert (PDA) Function Function applies to this airplane TAWS and uses the following: 1) GPS/SBAS navigation database 2) GPS/SBAS navigation mode 3) Aircraft position 4) Aircraft altitude 8-12 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 398 AGL altitude to alert when the rate of descent is hazardously high as compared to height above terrain. GPWS Mode 1 has a caution and a warning threshold. When below the thresholds, a GPWS Mode 1 warning is generated. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 8-13...
  • Page 399 There are two Mode 2 envelopes: Mode 2A which is active when not in landing configuration, and Mode 2B which is active when in landing configuration. Envelope selection is determined as follows. 8-14 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 400 AGL Rate (KIAS) (fpm) 66% × < 220 Caution 6000 > 3900 6000 + Threshold 220 to 50 × ( Airspeed − 220 ) > 300 10,000 AGL Rate Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 8-15...

  • Page 401: Sink Rate After Takeoff Or Missed Approach

    (as determined by the GPS/SBAS) with distance to the active runway threshold increasing. GPWS Mode 3 is disarmed upon climbing through 700 feet AGL traveling more 8-16 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 402: (Gpws Mode 4)

    Mode 4B which gives cautions when landing gear or flaps are in other than landing configuration. Applicability of Mode 4 envelopes to aircraft types are as follows. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 8-17...
  • Page 403 ≥182.5 High-Speed 800 or 8 × ( KIAS − 120 ) < 138.75 Low-Speed Lesser of: ≥ 138.75 High-Speed 800 or 8 × ( KIAS − 120 ) 8-18 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 404: Excessive Downward Deviation From An Ils Glideslope

    1.3 + 1.4% × 2 + 1% × ] Dots ] Dots ( 150 − AGL Altitude ) ( 150 − AGL Altitude ) 1.3 Dots 2 Dots Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 8-19...
  • Page 405 TAWS and connects directly to the EFIS IDU. 3) ILS Receiver. Glideslope receiver is the source of glideslope deviation for the TAWS. 8-20 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 406  Audio Cancel Switch         Radar Altimeter     Flap Position Sensor Glideslope     Deactivate Switch Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 8-21...
  • Page 407 1) If either the pilot or co- pilot system is operating in QNH mode, the QNH barometric setting is used (on-side barometric setting preferred); or 8-22 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 408 1) If the aircraft is in TERMINAL, DEPARTURE, IFR APPROACH, or VFR APPROACH mode and an active runway exists, reporting station elevation is the elevation of the active runway threshold. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 8-23...
  • Page 409 Terrain Data Terrain To be considered valid, the Database following must apply: 1) Aircraft position is valid; 8-24 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 410 GPS/SBAS vertical speed providing the VFOM is less than or equal to 106 feet. Terrain Closure Smoothed Due to multiple sources for Rate first derivative altitude, there are multiple Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 8-25...

  • Page 411: Taws Automatic Inhibit Functions (Normal Operation)

    1000’ AGL. This form of inhibiting prevents nuisance alarms on missed approach when the glideslope receiver detects glideslope sidelobes. 8-26 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 412: Taws Automatic Inhibit Functions

    System Sensor/Database Failures. System sensor failures, non- installation of optional sensors, database failures, and combinations thereof affect TAWS as follows. Table 8-12: TAWS Automatic Inhibit Functions GPWS Mode Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 8-27...
  • Page 413 PFD and ND. 3) GPS/SBAS (V) = VFOM > 106’. 4) GPS/SBAS = GPS/SBAS (H) + GPS/SBAS (V). Indication is loss of terrain display on PFD and ND. 8-28 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 414 Figure 8-13 through Figure 8-17 show all possible scenarios including “None” where the aircraft pierces the TAWS FLTA Terrain envelope, and SVS TAWS is enabled for the safest possible Warning Alert condition. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 8-29...
  • Page 415 Section 8 Terrain Awareness Warning System Figure 8-13: PFD SVS BASIC Option 8-30 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 416 Section 8 Terrain Awareness Warning System TAWS FLTA Caution Terrain: Amber (Yellow) TAWS FLTA Caution Warning: Red Figure 8-14: PFD SVS TAWS Option Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 8-31...
  • Page 417 Section 8 Terrain Awareness Warning System Obstruction above aircraft Obstruction below aircraft Figure 8-15: PFD SVS TAWS Option and Obstructions 8-32 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 418 Section 8 Terrain Awareness Warning System Obstruction within TAWS FLTA Caution envelope with aural annunciation “Caution Obstruction, Caution Obstruction.” Obstruction symbols flash. Figure 8-16: PFD Obstruction Caution Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 8-33...
  • Page 419 Section 8 Terrain Awareness Warning System Obstruction within TAWS FLTA warning envelope with aural annunciation “Warning Obstruction, Warning Obstruction.” Obstruction symbols flash. Figure 8-17: PFD Obstruction Warning 8-34 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 420 Section 9 Appendix Section 9 Appendix Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 421 Download Routes and User Waypoints ... 9-18 9.11.3. Upload Routes and User Waypoints ....9-18 9.11.4. Delete Routes and User Waypoints ....9-18 9.12. EFIS T (ETT) ........9-19 RAINING IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 422 ABLE EGULATORY EFERENCE 9-3: A ............9-8 ABLE IRSPEED RROR 9-4: A ......9-9 ABLE IRSPEED EGULATORY EFERENCE 9-5: P ............9-11 ABLE ERMINATORS 9-2: VFR W ............9-18 IGURE AYPOINT Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 423: Appendix

    9.2. Operating Tips With the Genesys Aerosystems EFIS installed and certified in all categories of certified aircraft, numerous tips and suggestions are available for obtaining the maximum performance and benefit from this system. Additional operating tips are available with future releases of this publication.

  • Page 424: Altimeter Settings

    9.4. Magnetic vs. True North Modes of Operation There are two modes for the AHRS: Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 425 Magnetic North. Wind is displayed referenced to Magnetic North. 2) True North mode: GPS Track is used as-is and reflects True North. When AHRS is in Slaved mode, heading from AHRS is IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 426: Altitude Miscompare Threshold

    20,000’ 50’ 30,000’ 75’ 40,000’ 100’ 50,000’ 125’ Allowable installed system error is added on top of instrument error and these values are derived from the regulations as follows. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 427: Airspeed Miscompare Threshold

    SAE AS8002A Table 3 as follows. Table 9-3: Airspeed Error Calibrated Airspeed Allowed Error 50 knots 5 knots 80 knots 3 knots 100 knots 2 knots 120 knots 2 knots IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 428 For Climbing Flight (VSI > 250 feet per minute): – 10): 10 knots Starting from (V 14 CFR § Do not perform a comparison if either value is 29.1323 – 10) below (V For Other Flight Regimes: Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)

  • Page 429: Jeppesen Navdata Chart Compatibility

    They are not a substitute for current aeronautical charts. www.Jeppesen.com for the latest information on coding instrument procedures, naming conventions, altitudes within the database, and aeronautical information compatibility. 9-10 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...

  • Page 430: Arinc 424 Path-Terminator Leg Types

    (Course is flown making adjustment for wind) Course to Leg defines a specified course to a specific DM Distance, Distance which is from a specific database DME Navaid. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 9-11...
  • Page 431 Course to Leg defines a course to a Radial specified radial from a specific database VOR Navaid. Direct to Fix Course from Fix to Altitude 9-12 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 432 Distance DME Distance from a DME (Different Navaid. Fix) Course from Fix to Manual termination Terminates at an altitude Terminates at the fix after one orbit Manual termination Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 9-13...
  • Page 433 Leg defines a course reversal Turn starting at a specific fix, includes Outbound Leg followed by 180 degree turn to intercept the next leg. Precision Arc to Fix 9-14 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 434 DME Distance Distance from a specific database DME Navaid. Heading to Leg defines a specified heading Intercept to intercept the subsequent leg at an unspecified position. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 9-15...

  • Page 435: Data Logging And Retrieval

    VOR Navaid. 9.9. Data Logging and Retrieval The Genesys Aerosystems EFIS logs all data associated with a flight, including all flight instrument and navigation data. This data may be downloaded for review after flight. Data from the last five flights or 20 hours are logged at a one-second interval.

  • Page 436: Log Files/Delete Log Files

    “VP.” These may be found on VFR charts and should be loaded in the FMS prior to flight to ensure they are available in the database, and the INFO checked for proper location. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 9-17...
  • Page 437 USER.DAT, from the IDU. Use this option to delete contents of the route directory when corrupted routes cause the IDU to continually reboot. 9-18 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 438 2) Ensure the USB with required files is properly connected. 3) Try again after reboot. 4) Press any button to continue. 5) Try a different USB external drive. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 9-19...
  • Page 439 Error Code: Route: Duration of Flight: Conditions: Remarks: (Include time, altimeter Setting, OAT, ALT, TAS, GS, Heading, track, position, flight segment, pilot action, system response, is problem repeatable?). 9-20 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 440 Section 9 Appendix 9.15. Certification Basis The following TSOs are considered applicable to the IDU-680 (depending upon the features of the installed software). Document Number Document Title Mark 33 Digital Information Transfer ARINC 429-16 System (DITS) Traffic Alert and Collision Avoidance...
  • Page 441 Section 9 Appendix 9.16. Environmental Requirements The IDU-680 meets the requirements of RTCA/DO-160F as defined below. Test Category Sec. Condition Cat. Notes Description 4.0 Temperature Equipment intended for +75°C for and Altitude installation in non- Short-Time pressurized and non- Operating controlled temperature High Temp.
  • Page 442 13.0 Fungus Demonstrate whether By Analysis Resistance equipment material is adversely affected by fungi growth. 14.0 Salt Fog Equipment is subjected to a corrosive atmosphere Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 9-23...
  • Page 443 Conducted) environments and to show frequencies compliance with the to be interim HIRF rules. 100V/m 21.0 Emission of Equipment in areas where Radio apertures are EM 9-24 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 444 26.0 Fire, Non-metallic equipment, By Analysis Flammability component parts, sub- assemblies installed in pressurized or non- pressurized zones and non-fire zones with largest dimension greater than 50 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) 9-25...
  • Page 445 Traffic Traffic Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 446 TIS-B T ......T-8 IGURE RAFFIC YMBOLS T-4: C ............T-9 ABLE LOCK PTIONS T-7: MFD T (FORMAT) M ....T-10 IGURE RAFFIC ORMAT T-5: M ........... T-11 ABLE YNCHRONIZATION IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 447 Table T-1: Traffic Rendering Rules Type Traffic Distance Results OT and PA Traffic Beyond 6 NM Not displayed TCAS-I, TCAS-II, TAS Within 200’ of ground Not Displayed or TIS-A Sensor Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 448 Traffic within +2,700 and -9,900 feet of aircraft BELOW altitude is displayed. Traffic within -2,700 and +2,700 feet of aircraft NORMAL altitude is displayed. All received traffic is displayed; no altitude filtering is performed. IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 449 North or True North depending upon the status of the True North discrete input. When the AHRS is in DG Mode, “DG” appears to the right of the ownship symbol. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 450 A digital heading readout and pointer aligned with the longitudinal axis of the ownship symbol appears on the compass rose boundary circle. Compass rose symbols are as specified in Section 3 Display IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 451 The traffic screen displays airport runways in correct relationship and scale to the ownship symbol. When traffic source is ADS-B, traffic vectors and aircraft identification data are shown. The traffic vector is a line connecting Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 452 Degraded Position Traffic with Track Information: Other Traffic Proximate Traffic Advisory Advisory (Flashing) Degraded Position Traffic without Track Information: Other Traffic Proximate Traffic Advisory Advisory (Flashing) Figure T-6: ADS-B and TIS-B Traffic Symbols IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 453 4) ADS-B Traffic Vector Length: When display of ADS-B traffic vector symbols is selected, length of traffic vector is annunciated as “VECT ##” where “##” is the traffic vector length in minutes. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 454 5) TREND VECTOR: When TCAS flag is TIS-B, used to select the traffic trend vector length in minutes. OFF (R4) appears at this level to quickly turn off the traffic trend vector. T-10 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 455 680 MFD areas as specified in the notes. MFD Selected Page Independent between top and bottom 680 MFD areas. Note that this parameter is Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) T-11...
  • Page 456 Independent between top and bottom 680 MFD areas T 5. MFD Fault Display (FAULTS) Menu If the traffic option is enabled, loss of communications with the traffic sensor (TRFC). T-12 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 457 Remote Bugs Panel (RBP) Remote Bugs Panel (RBP) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) RBP-1...
  • Page 458 EMOTE ANEL List of Figures and Tables RBP-1: R ........RBP-3 IGURE EMOTE ANEL RBP-1: R (RBP) ......RBP-4 ABLE EMOTE ANEL RBP-2: M ........RBP-6 ABLE YNCHRONIZATION RBP-2 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 459 The design of this RBP promotes the ease of operation while minimizing pilot workload complexity. The HDG and ALT encoders behave similarly as do the same encoders on the IDU-680 where they appear during most screen configurations. During initialization, the RBP always begins with the GENESYS RBP displayed on the Main and Option display screens.
  • Page 460 Set climb angle Encoder Angle Set climb angle to 3 degrees setting Increment or Set descent Multifunction Descent decrement angle to 3 Encoder Angle Set descent degrees angle setting RBP-4 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 461 Button or off) Toggle Minimum Option “---“ minimum Altitude Button altitude bug (on or off) Scroll through “Set” options. Function Arrow Buttons Press both Scroll arrow buttons simultaneously Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) RBP-5...
  • Page 462 VNAV Climb Angle VNAV Descent Angle Used when “Dual Decision Decision Height Setting Height Flag” is false. Heading Bug Minimum Altitude Bug Value VLOC OBS Settings RBP-6 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 463 MFD Selected Page Independent between top and bottom 680 MFD areas. Note that this parameter is transmitted to all other IDUs to support weather radar vertical profile mode selection. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) RBP-7...
  • Page 464 MFD Map Function Declutter Independent between top Settings and bottom 680 MFD areas MFD Show ETA Flag MFD Map NavData Symbol Declutter Settings Independent between top and bottom 680 MFD areas RBP-8 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 465 WX-500 Lightning Strikes WX-500 Lightning Strikes Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 466 AYPOINT EARING ISTANCE IN OWER ..............S-6 IGHT ORNER S-6: F . S-7 IGURE OTALIZER AYPOINT EARING AND ISTANCE S-7: MFD S (FORMAT) M ....S-7 IGURE TRIKE ORMAT IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 467 True North discrete input. When the AHRS is in the DG mode, a “DG” indication appears to the right of the ownship symbol. Strike Screen Display ND Lightning Display Figure S-1: Lightning Symbols Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 468 Clock with Zulu Time Figure S-3: Clock and Options Table S-2: Clock/Options Feature Options Notes = Automatic declutter mode Declutter DCLTR A Mode DCLTR M = Manual declutter mode IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 469 Strike rate increases are displayed immediately upon calculation while decreases in strike rate are damped. Activating the strike clear function resets the strike rate to zero. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 470 “TRAFFIC” with an overlying red “X.” When traffic is enabled, the status of traffic altitude filtering is displayed as follows: a) AUTO = “TRF AUTO” IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 471 (shown if cell is current mode) CELL MODE Switch to cell mode STRK TEST (shown if strike is current mode) Activate WX-500 pilot initiated test function Figure S-7: MFD Strike Format (FORMAT) Menu Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 472 PAGE menu allows the pilot to select which MFD page to display: STRIKES: Shows the Strike page. S 4. MFD Fault Display (FAULTS) Menu If the WX-500 option is enabled, loss of communications with the WX-500 (WX-500). IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 473 Audio/Radio Management Audio/Radio Management Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-1...
  • Page 474 RN3320 Nav Receiver ........AR-28 AR 5.5. Radio Frequencies Panel ......AR-29 AR 6........AR-30 EVICE PECIFIC AILURES AR 6.1. TX Indicator ........... AR-31 AR 6.2. AMU50 ............AR-31 AR-2 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 475 ONLY AR-14: ARINC 716 VHF COM T (8.33 C ABLE RANSCEIVER APABLE ) * ................AR-27 ONLY AR-18: RN3320 N ........AR-28 IGURE ECEIVER AR-15: RN3320 N ........AR-28 ABLE ECEIVER Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-3...
  • Page 476 ABLE OMMON YMBOLS AR-20: VHF T IGURE RANSCEIVER RANSMIT ELECTION NDICATOR ..................AR-31 AR-17: M ........AR-31 ABLE YNCHRONIZATION AR-18: T ..ABLE EVEL UNCTION ESCRIPTIONS ..................AR-34 AR-4 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 477 -- such as STBY frequency/codes, TX indicator when there is no TX feedback, or Marker Beacon Receiver High/Low sensitivity modes. When used for an analog bar indication, light gray is used in low-light conditions. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-5...
  • Page 478 Line Select: Each device is pilot-selectable indicated by a gray rectangle drawn around the line for that device. Figure AR-2: Device Label Line Select AR-6 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 479 The level bar indicates a varying range of attributes, commonly volume. The white rectangle is filled with a color as defined in Table AR-1 proportionately increasing from left to right, representing the magnitude of its value. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-7...
  • Page 480 AR 2.2.5. Selected Line Highlight Figure AR-4: Selected Line Highlighted AR-8 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 481 VHF NAV Receiver When VHF navigation receivers are interfaced for management from the audio/radio page, the AR page line for the device is displayed in the following manner. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-9...
  • Page 482 AR 2.5. ADF Receiver When ADF receivers are interfaced for management from the audio/radio page, the AR page line for the device is displayed in the following manner. AR-10 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 483 When a transponder is interfaced for management from the audio/radio page, the AR page line for the device is displayed in the following manner. AR 2.6.1. Transponder Symbols Figure AR-8: Transponder Symbols Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-11...
  • Page 484 DME Receiver DME receiver parameters are established through interfaces with VHF navigation receivers. When a DME receiver device is interfaced, the DME receiver is displayed as an Audio-Only Device. AR-12 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 485 Threshold or filter level of Voice operated microphone before sound is switch allowed to be heard on the intercom system VOX or volume level bar Volume communications over Volume level intercom system Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-13...
  • Page 486 When interfaced for receiver sensitivity switching through the EFIS, the Word “HIGH” or “LOW” appears to represent the configured Marker Beacon receiver. Figure AR-11: Marker Beacon Receiver Symbols AR-14 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 487 TX (L5) enabled, enables inhibited. transmitting on selected Transmissions go transmitter. Enabling through the default (only one device at a emergency- time) unmutes the Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-15...
  • Page 488 When selected line is When audio an intercom with Pilot controller fails, PLT PLT ISO (L5) Isolation mode, toggles ISO (L5) is Pilot Isolation mode of inhibited. the intercom. AR-16 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 489 ACTV and STBY frequencies, channels, or codes. When selected line is If audio controller SPLIT TX an intercom, toggles fails, appearance (R7) split transmit mode. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-17...
  • Page 490 KHZ ( frequency by 25 kHz .x75, .x80, .x85 and from 0 to 975 kHz. .x90. When selected line is a If selected device VHF COM transceiver fails, appearance AR-18 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 491 When selected line is a For BXP6402 transponder, scroll to transponder, change the transponder operating modes (in  MODE ( operating mode. order) are STBY, GRD, ON, and ALT. If transponder fails, Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-19...
  • Page 492 If native volume no audio controller is control through the AR-20 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 493 · COM: “MHZ” · NAV: “KHZ” · NAV: “VOL” or “VOL/MUTE” · NAV: “MHZ” · ATC: “MODE” · ATC: “CODE” · ALL: “ADJ” Figure AR-13: Expanded Control Page Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-21...
  • Page 494 EMERG (R8) inserts the emergency code (7700) into the standby EMERG (R8) code position and emergency frequency (121.500) into the standby frequency positions for the VHF Com transceivers. AR-22 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 495 Appears when a Functionality depends line other than on the line selected.  ADJ ( the first line is Scroll CW or CCW for selected. desired input. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-23...
  • Page 496 Scroll amplification In light magenta to increment Fourth applied to the until confirmed of or CCW to transmitting then level bar filled decrement microphone with light green level AR-24 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 497 AUDIO MODE Setting of audio filter to allow for better voice or Morse code Second  Scroll to toggle signals to be heard. VOICE and Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-25...
  • Page 498 Transponder status  mode. Scroll  mode and code changes respectively.  Scroll to toggle METERS or Second ALTITUDE  Scroll to increment or Third decrement (per-digit) the preset AR-26 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 499 Table AR-14: ARINC 716 VHF COM Transceiver (8.33 Capable only) * Line Notes Name and Control Function Number (if applicable) First COM1 or COM2 COM1 and COM2 status Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-27...
  • Page 500 ; KHZ/MUTE AUDIO MODE Setting of audio filter to allow for better voice or Second  Scroll to toggle Morse code signals to be VOICE and NONE. Light heard AR-28 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 501 Displays Frequency is when light magenta VHF COM actively until confirmed Transceiver transmitting then light green. Receive Device is actively receiving. Split RFP display Transmit excludes Split Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-29...
  • Page 502 AR Page display. When an audio controller fails, only the devices with audio control through those other devices’ interfaces and connected to audio controller slots that are heard when failed display a volume level bar. AR-30 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 503 Audio-Radio device parameters The following menu parameters are independent between displays. These are used to support non-PFD display options to give the pilot maximum MFD operating flexibility. Note that some Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-31...
  • Page 504 (CW rotation) or decrement (CCW rotation) the STBY frequency by 25 kHz from 0 to 975 kHz. When the selected line is a VHF Com Transceiver in 8.33 AR-32 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 505 (CCW rotation) the volume level. When an audio controller is configured and not failed, push to toggle muting. If the selected device fails, VOL/MUTE is inhibited. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-33...
  • Page 506 ADF, BFO, and REC. If ADF receiver fails, MODE appearance and operation are inhibited. 4) When showing AR page, VFR appears when selected line is a transponder and places VFR code AR-34 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 507 If transponder fails, IDENT appearance and operation are inhibited. 1) When showing any page, RADIO appears. Press to enable the radio page for control of audio and frequency control. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-35...
  • Page 508 1) When showing AR page, SWAP appears when selected line is a device with ACTV and STBY frequencies, channels, or codes and toggles ACTV and STBY frequencies, AR-36 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 509 Note 1: Used when the function is tied to a page in the top area. Note 2: Used when the function is tied to a page in the bottom area or tied to being “Transmit Enabled.” Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) AR-37...
  • Page 510 Datalink Datalink Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 511 RECIPITATION D-3: D ....D-8 IGURE ATALINK INDS AND EMPERATURE LOFT D-4: D ....D-9 IGURE ATALINK YMBOLOGY WNSHIP YMBOL D-5: WSI D ........ D-9 IGURE ATALINK CREEN EGEND IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 512 ........D-16 IGURE OUNDARY IRCLE YMBOL D-10: MFD D (FORMAT) M .... D-18 IGURE ATALINK ORMAT D-10: M ........D-19 ABLE YNCHRONIZATION D-11: T D-20 ABLE EVEL UNCTION ESCRIPTIONS Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 513 Graphical METAR Data subscription. Derived from Textual METAR data using EFIS algorithm. NEXRAD Graphical METAR AIRMET Figure D-1: Datalink Symbology NOTE: Up to 300 Temporary Flight Restrictions may be displayed. IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 514 Table D-3: Datalink NEXRAD Echo Tops Amplifying Severe Weather Condition Color Text “HAIL” Possible Hail Light Cyan “HAIL+” Confirmed Hail Light Cyan “MESO” Mesocyclonic (Rotation Detected) “TRNDO” Tornadic Magenta Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 515 VFR and MVFR GMETARS are decluttered 1,600 NM Graphical METARs are also displayed in the menu system “nearest airport,” “nearest weather,” and “info” functions. Figure D-2: NRST Airport INFO IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 516 1) Lightning ground strikes: In correct relationship to the ownship symbol as an amber (yellow), small cross symbol. 2) Convective SIGMET: As magenta line segments showing the boundary of the area in correct relationship to the ownship Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 517 Temp Units in the EFIS Limits) and a graphical arrow indicating wind direction. When winds and temperature aloft data are displayed, soft tiles are present to change the data altitude. Figure D-3: Datalink Winds and Temperature Aloft IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 518 Airplane with V Airplane FAR 23 with V Figure D-4: Datalink Symbology Ownship Symbol D 1.2. Datalink Screen Legend Figure D-5: WSI Datalink Screen Legend Figure D-6: ADS-B Datalink Screen Legend Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 519 “TFR” with an overlying red “X.” 4) Datalink Weather Status: When status of NEXRAD radar, graphical METARs, and lightning ground strike data are displayed as follows. Figure D-7: Clock/Timers/Options D-10 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 520 NEXRAD not downlinked within last 10 minutes but ## is age in minutes. downlinked within last 75 NEXRAD Radar shown on minutes and selected for display. display (weather radar, if Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) D-11...
  • Page 521 5 minutes but (yellow) where ## is age in downlinked within last 10 minutes. minutes and selected for Graphical METARs shown on display. “Show Full Sensor display. Status Flag” enabled. D-12 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 522 Lightning Ground Strikes display. shown on display. “LTNG ##” drawn in green Lightning Ground Strikes downlinked within last 5 where ## is age in minutes. minutes and deselected from Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) D-13...
  • Page 523 Lightning Ground Strikes not downlinked within last 75 “LTNG XX” overlaid with red minutes (timed-out). “Show “X” Full Sensor Status Flag” enabled. Lightning Ground Strikes not shown on display. D-14 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 524 A white triangular heading pointer aligned with the longitudinal axis of the ownship symbol appears on the boundary circle with a green diamond-shaped track pointer aligned with the aircraft’s track across Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) D-15...
  • Page 525 When there is an active waypoint and the GPS/SBAS OBS setting is manual, the manual course through the waypoint is shown as a pointer centered on the waypoint. The pointer matches the lateral D-16 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 526 3) AMET-SMET: Only available when an AIRMET or SIGMET is within the Datalink page viewable area. Allows the pilot to view the text for the displayed AIRMETs and SIGMETs. While Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) D-17...
  • Page 527 Accept changes available Figure D-10: MFD Datalink Format (FORMAT) Menu D 2.1. MFD DATALINK Page (Step-By-Step)   1) Push and scroll to DATALINK and push to enter. D-18 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 528 PFD consistent in the case of PFD reversion. The onside characteristic means that individual pilots can still adjust their PFD settings to their preference. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) D-19...
  • Page 529 Aloft grid level. UP does not appear when highest grid level is displayed. 2) When showing Datalink Page with: (a) pan mode enabled; (b) information for nearest highlighted waypoint being D-20 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 530 Refer to the INFO Menu requirements for the amount and type of information presented. DOWN has precedence over INFO/HIDE. When showing the Datalink Page with Pan Mode, EAST appears. Press to shift Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) D-21...
  • Page 531 (ADSB MAINT) and an indication of whether the Conflict Situational Awareness algorithm is working (ADSB CSA). ADS-B datalink is mutually exclusive with WSI datalink. D 6. MFD Page (PAGE) Menu DATALINK: Shows the Datalink page. D-22 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 532 Weather Radar Weather Radar Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) WX-1...
  • Page 533 ........WX-9 ABLE PPLICABILITY WX-4: RDR 2100 M ......WX-9 ABLE NNUNCIATION WX-8: MFD WX RDR F (FORMAT) M ..WX-12 IGURE ORMAT WX-5: M ........WX-13 ABLE YNCHRONIZATION WX-2 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 534 In a horizontal depiction, the weather screen uses an arced format with the ownship symbol centered in the bottom of the display with the weather area depicted as an arc ahead of the ownship symbol. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) WX-3...
  • Page 535 WX-4 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 536 The value of the track line in whole degrees left or right of aircraft heading is displayed adjacent to the outer end of the track line. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) WX-5...
  • Page 537 The weather radar screen displays airport runways when the weather radar screen is showing horizontal depiction. Figure WX-5: Radar Active Flight Plan WX-6 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 538 055 and 171 bits 27-29 as 010b. Fourth-Level Weather or Third- Level Ground Returns. With an 100b Magenta RDR-2000 or RDR-2100 weather radar type, this color alternates between MAGENTA and BLACK Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) WX-7...
  • Page 539 1) Zulu Time or LCL Time: As specified in Section 3 Display Symbology; 2) Timer: As specified in Section 3 Display Symbology; 3) Weather Radar Mode Annunciation: As in Table WX-3. WX-8 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 540 Weather radar mode is not standby or forced standby; and Weather radar indicates stabilization is off. TGT ALERT Weather radar mode annunciation is not overlaid with a red “X”; (Target Alert) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) WX-9...
  • Page 541 1) Mode annunciation is not overlaid with a red “X”; 2) Mode is not standby or forced standby; 3) Radar is in vertical profile submode (profile depiction). WX-10 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 542 Vertical profile. Vertical Profile option appears in the selection box only when the selected weather radar mode is not OFF or STBY. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) WX-11...
  • Page 543 RDR-2100. c) TRACK: Change the track in increments of 1 degree. d) ROLL TRIM: Change the roll trim in increments of 4 degree. WX-12 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 544 VSI Bug Setting Crosslink Synchronization Status Audio-Radio device parameters G-Force Limit Parameters The following menu parameters are synchronized across all displays when crosslink is enabled. Otherwise, they are only Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) WX-13...
  • Page 545 MFD Map Function Declutter Independent between top and Settings bottom 680 MFD areas MFD Show ETA Flag WX-14 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 546 (WXR RCP X) indicates either loss of communication or a failure status using the same test as invalid data SSM for output labels 270, 271, 273, or 275. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) WX-15...
  • Page 547 Video Video Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 548 ABLE IDEO NPUT ONTROLS V-4: C MFD P ..V-8 IGURE ENTER OTARY NCODER ONTROLS V-2: M ..........V-8 ABLE YNCHRONIZATION V-3: T .. V-10 ABLE EVEL UNCTION ESCRIPTIONS IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 549 When pan mode is active, controls are present to allow moving the portion displayed up, down, left, and right. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 550 Exiting Pan Mode removes pan mode controls and mini-map, if any. V 1.3. Video Input Status Display Figure V-2: Video Status When selected, the following are optionally displayed in the upper right corner of the Video Input display: IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 551 6) Hue: Chroma hue is displayed as HUE nnn% where nnn is the hue setting as a percentage of the maximum value. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 552 Press -- Set Selected Hue Figure V-3: MFD Video Input Format (FORMAT) Menu Upon selecting the MFD format menu when in the Video Input page, an option list appears with the following options. IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 553 DCLTR which video input d) CTRST: (Current contrast status settings are setting) displayed. e) SAT: (Current chroma saturation setting) HUE: (Current chroma hue setting) Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 554 Video V 3. IDU-680 Center Rotary Encoder Controls On the IDU-680, upon selecting the MFD format menu when in the  Video Input page, becomes a dedicated brightness control, and  becomes a dedicated contrast control. Scroll these controls to activate the BRT or CTRST menus.
  • Page 555 680 MFD areas. Note that map scale is transmitted onside to support weather radar range selection. MFD Map Function Declutter Independent between top Settings and bottom 680 MFD areas Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 556 Note 1: Used when the function is tied to a page in the top area. Note 2: Used when the function is tied to a page in the bottom area or is “Transmit Enabled.” V-10 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 557 Altitude Aircraft Selected (ASEL) ............2-5 Capture Predictor ..............3-74 Display ................3-21 to 23 Minimum ..........3-22 to 23, 5-8, RBP-5 to 6 Miscompare Threshold ............. 9-7 to 8 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 558 Brown ................2-34, 3-83 BUGS ..........1-8, 5-22, 5-64 to 69, 7-7, 7-42 Button/Menu Functions ......1-5, 3-16, 5-1, 5-7, 5-10, 8-5 CENTER/ARC ..............5-82, S-8 Clock/Timers ............... S-4 to 6 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 559 Decision Height (DEC HT) ..2-6, 2-56, 3-27 to 29, 5-8 to 9, 5-68, ................RBP-5 to 7, WX-13 DELETE ............5-35, 5-39, 5-46, 6-8 Demonstrator ............... 1-7 to 8, 2-68 Density Altitude ..............3-80, 4-8 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 560 Exceedance Menu ..............5-27 OVRL ................5-71 to 72 Encoder Functions ..............3-17 Enroute ........2-42, 3-52, 3-79, 7-24 to 27, 8-7 to 10 Estimated Time Enroute (ETE) ........... 2-7, 3-73 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 561 .. AR-36, D-16, D-19, D-22, RBP-7, S-5, T-7, T-11, V-9, WX-6, ..................WX-14 Create ..................6-7 CREATE-EDIT............5-31 to 40, 6-7 Delete ..................5-35 Edit ..................5-34 EDIT WHICH FPL ..............5-34 FPL............2-8, 5-13, 5-29 to 40, 6-7 Limits ..................5-29 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 562 ..........D-16 to 17, RBP-4 to 5, S-5, T-7 to 9 ALMANAC ................5-76 Altitude ..................7-22 FDE ..................5-76 HPL ..................5-76 LOI ..................5-76 PWR ..................5-75 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 563 IAP ................2-9, 7-15, 7-29 IAS ............. 1-8, 2-9, 3-30, 4-8, 5-64 to 68 IDU-680 ..1-5 to 10, 2-18, 2-28 to 30, 2-66 to 67, 3-10 to 16, 4-6, ....4-11 to 13, 5-7, 5-10 to 13, 5-19, 5-22, 5-25, 5-28 to 30, ............
  • Page 564 LPV ...... 2-10, 2-67, 3-54 to 57, 7-8 to 9, 7-24 to 28, 7-32, ..................7-45 to 47 Approach .............. 2-58, 7-24 to 25 Magnetic Course ................ 7-21 Map ........... 3-60, 4-7, 5-71, WX-9, WX-14 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 565 Mode 1 ..2-36, 2-52, 2-62, 4-6, 4-17 to 20, 8-4 to 5, 8-13 to 14 Mode 2 ..2-36, 2-42, 2-62, 4-6, 4-21 to 24, 8-4 to 5, 8-14 to 16 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 566 ................3-46, 8-33 to 8-34 OFF ..5-16 to 17, 5-21 to 22, 5-25, 5-36, 5-44, 5-57, 5-61 to 62, ..... 5-68, 5-77, 5-85, D-17 to 20, S-8, T-10, WX-9 to 15 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 567 Declutter ............3-48, 5-70 to 72, 8-29 Essential Mode ................. 6-5 Normal Mode ..............2-23, 5-11 Symbology ..............3-21 to 22 with EICAS ................2-31 Pitch Scale ..............3-37 to 38, 4-7 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 568 RNAV ..........2-14, 7-7 to 8, 7-16, 7-32, 7-45 DPs ..................2-66 Runway (RW) ..2-14, 2-67, 3-61, 4-7, 5-9, 5-50, 6-9 to 10, 8-26, ................. D-19, T-11, WX-14 SAVE ..............5-33 to 34, 5-44, 6-7 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 569 Terrain Rendering ............. 8-11 to 12 Too Low ................2-53, 8-18 Top of Descent (TOD) ......2-16, 3-55, 3-74 to 75, 7-46 Top-Level Menu ............ 5-11 to 16, AR-32 Automatic Pop-Up ..............5-16 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 570 ........7-21, 7-51, 9-12, 9-16, AR-6, RBP-4 to 5 DME ..................7-32 VTF ..............2-18, 3-52, 7-25 to 30 WAAS ..............2-18, 7-7 to 8, 9-21 Warnings, Cautions, and Advisories ......1-9, 2-35, 9-5 Water ..................3-83 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 571 OVERFLY ............... 5-47, 7-5 Overfly User ................5-31 Phantom ..................7-16 Pointer ................4-7 to 8 Routes and User ..............9-18 Sequencing ................7-14 USER WPT .......... 5-22, 5-31, 5-36 to 39, 6-7 Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 572 IDU-680 EFIS Software Version 8.0E WGS-84 ..............2-66, 7-17 to 22 Wind ..............3-79 to 80, 4-8, 9-6 WX-RDR ..................5-80 XFILL SYNC ..............5-21, 6-10 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 573 Usually measured in degrees (°). Barometric Altimetry – Measurement of altitude based on the atmosphere (pressure and temperature). Barometric Correction – Display and altitude correction for local barometric pressure. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 574 Discrete – A logic input or output that identifies a condition or status of or for an ancillary system. Discretes are defined by the operating software or settings programmed specifically for the aircraft. IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 575 PFD. Flight Path Marker (Velocity Vector) – Display of aircraft’s actual flight path, showing where the aircraft is going as opposed to where the aircraft is pointed. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing)
  • Page 576 EFIS desired heading and the actual aircraft heading. The EFIS desired heading is either the pilot-selected IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 577 GPS-based flight plan. Hectopascal (hPa) – International System of Units (SI) unit measure of pressure, equals one millibar (mbar). HeliSAS – Genesys Aerosystems’ helicopter autopilot and stability augmentation system. Horizontal Situation Indicator (Selectable Function) – Display of VOR or localizer and glideslope deviation when selected for display on the PFD.
  • Page 578 Navigation mode signals are the course error output and the left- right deviation signals. Course error output is based on the difference between the EFIS selected course (OBS) and the IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 579 (limits) file. Q-Routes – Published RNAV routes, including Q-Routes and T- Routes, can be flight planned for use by the Genesys EFIS, subject to any limitations or requirements noted on enroute charts, in applicable Advisory Circulars, or by NOTAM. RNAV routes are depicted in blue on aeronautical charts and are identified by the letter “Q”...
  • Page 580 AHRS in the same manner as the ball in a mechanical slip indicator. IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 581 Routes are depicted on Enroute Low Altitude Charts and considered to include the same attributes of Low Altitude Airways in the Genesys Aerosystems EFIS Declutter menus. Talker – IDU providing data to external sensors and generating aural alerts. IDUs depend upon intra-system communications to determine which IDU on a side takes over “Talker”...
  • Page 582 Waterline – Indication of the aircraft’s longitudinal axis or waterline (attitude). Wide Area Augmentation System (WAAS) – Developed by Federal Aviation Administration to provide accurate positioning part of the Satellite Based Augmentation System (SBAS). Other G-10 IDU-680 EFIS Software Version 8.0E (Fixed Wing) Rev A Nov, 2016...
  • Page 583 Wind Information – Display of wind direction, wind speed, and cross wind component. Zulu Clock, Timers – Display of Zulu time (based on GPS data) and pilot-selected timer. Rev A Nov, 2016 IDU-680 EFIS Software Version 8.0E (Fixed Wing) G-11...
  • Page 584 C o p y r i g h t © 2 0 1 6 G e n e s y s A e r o s y s t e ms . A l l r i g h t s r e s e r v e d . I D U - 6 8 0 V e r s i o n 8 .

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