Page 1 VFR PFD...
Page 3 VFR PFD 091-00028-001 ( ) EFD1000 VFR PDF Pilot’s Guide Page iii...
Page 4 REVISION DESCRIPTION of CHANGE Initial Release Page iv EFD1000 VFR PDF Pilot’s...
Page 5: Table Of Contents
Copyrights, Trademarks and Patents ............ ix 2.1. Controls & Display Orientation ...............2-2 Approvals ..................... x 2.2. Controls ........................2-4 LIMITED WARRANTY Aspen Avionics, Inc..........xi 2.2.1. Left and Right Knobs ..............2-4 2.2.1.1. Left Knob Functions ............2-5 Weather Data Warranty ................. xiv 2.2.1.2.
Page 6 2.3.4.1. Numerical Direction Indicator 4.1.2. Pitot Obstruction Monitor ............4-4 (Magnetic Compass) ............2-30 4.1.3. Heading ....................4-5 Compass Modes: 360º vs. ARC ..........2-30 4.1.4. Free Gyro Mode .................. 4-6 4.1.5. Degraded ADAHRS Performance ..........4-7 Navigation Information ............2-31 Ground Track Marker ..............2-31 4.2.
Page 7 4.4. Navigation Display ....................4-23 4.8. Hazard Awareness ...................4-52 4.4.1. Compass ....................4-24 4.8.1. Lightning Overlay ................4-52 4.4.1.1. 360° Compass Mode ............4-24 4.8.2. Data Link Weather Overlay ............4-54 4.4.1.2. ARC Compass Mode ............4-24 4.8.3. Traffic Overlay ...................4-58 4.4.2. Course Pointer ................4-27 4.8.3.1. Traffic Symbols ..............4-59 4.4.3.
Page 8 6.5. Loss of Aircraft Electrical Power ..............6-9 7.5.3. Analog Converter Unit (ACU) ...........7-12 6.5.1. Overvoltage Protection ..............6-11 7.5.4. Operational Specifications ............7-13 6.6. GPS Failures and RSM Emergency GPS Use ........6-11 7.6. Glossary ........................7-14 6.7. Power Override ....................6-13 7.7. Index ..........................7-18 6.8.
Page 9: Copyrights, Trademarks And Patents
Evolution™, EFD1000 Pro PFD™, EFD1000 MFD™, EFD500 MFD™, Services or any information accessed; 2) loss or damage to your EFD1000™, EFD500™, EFD 1000 VFR, PFD and the Aspen Avionics logo records or data; or 3) your use of, or results achieved from, the Services are trademarks of Aspen Avionics, Inc.
Page 10: Approvals
Revisions page. Specifications and operational details are subject to change without notice when using an earlier or later software version. Please visit the Aspen Avionics web site for the most up-to-date Pilot’s Guide. Installation of the EFD1000 PFD in a type-certificated aircraft must be performed in accordance with the latest revision of the EFD1000 and EFD500 Installation Manual.
Page 11: Limited Warranty Aspen Avionics, Inc
LIMITED WARRANTY Aspen Avionics, Inc. YOUR WARRANTY. Aspen Avionics, Inc. (“Aspen”) warrants Furnish proof sufficient to establish that the item is a to you, the original purchaser, that its Products (if purchased from an Nonconforming Product, and authorized dealer) will comply with applicable specifications (as set Allow Aspen access to all relevant records in order to forth in the owner’s manual) in all material respects and will be free from...
Page 12 Accident, contamination, damage from a foreign object or EXCLUSIVE WARRANTY. THIS WARRANTY IS EXCLUSIVE weather conditions, abuse, misuse, neglect, or negligence, AND IN LIEU OF ALL OTHER WARRANTIES. THE IMPLIED WARRANTY OF MERCHANTABILITY AND IMPLIED WARRANTY OF FITNESS FOR A Exposure of the product or the product’s host medium to any PARTICULAR PURPOSE, AS WELL AS ALL OTHER IMPLIED WARRANTIES computer virus or other intentionally disruptive, destructive, or...
Page 13 EXTENSION OF WARRANTY. No extension of this warranty WARRANTY PROCEDURE. If you require warranty service, will be binding upon Aspen unless set forth in writing and signed by you may contact your local Aspen Authorized Dealer or you may Aspen’s authorized representative. contact Aspen directly as described below.
Page 14: Weather Data Warranty
Weather Data Warranty THE WEATHER DATA SOFTWARE PRODUCT IS PROVIDED “AS IS. ” ALL OTHER LIMITS ON OUR RESPONSIbILITY WARRANTIES, EXPRESSED OR IMPLIED, INCLUDING ANY WARRANTY OF DISCLAIMERS. EXCEPT AS EXPRESSLY PROVIDED HEREIN, MERCHANTABILITY OR FITNESS FOR A PARTICULAR PURPOSE OR OF NON- WE MAKE NO WARRANTY OR REPRESENTATION, EITHER INFRINGEMENT ARE HEREBY EXCLUDED.
Page 15: Xm Wx Satellite Radio Service Agreement
XM WX Satellite Radio Service Agreement Hardware and required monthly subscription sold separately. Subscription fee is consumer only. Other fees and taxes, including a one-time activation fee may apply. All programming fees and weather data are subject to change. XM WX weather data displays and individual product availability vary by hardware equipment.
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Page 17: Conventions
Some of the optional functions with the VFR model are noted in the text. For complete instructions on the EFD1000 MFD and the EFD500 MFD, refer to the Aspen Avionics document number 091-00006-001 EFD1000/500 MFD Pilot’s Guide Terminology The term “PFD”, is used throughout this Pilot’s Guide and refers to the EFD1000 VFR PFD.
Page 18 Term Example Buttons REV Button, Range Buttons, MENU Button Hot Keys / Menu Keys Five keys on the lower right of the display Buttons CDI Navigation Source Select Button (Center Button) Knobs Left (CRS) Knob, Right (HDG) Knob Navigation Display Data Bar Airspeed, attitude, altitude display Table 1...
Page 19: Color Philosophy
Color Philosophy Table 2 provides the general operational philosophy of color usage on the PFD display. COLOR PURPOSE COLOR PURPOSE Used for navigation information or mode data related to Used to indicate flight envelope and system limits, and or provided by the navigation source currently selected for for warning annunciations that require immediate pilot display on the Course Deviation Indicator (CDI) (i.e., navigation GREEN...
Page 20: Warnings, Cautions, And Notes
Warnings, Cautions, and Notes Where applicable warnings, cautions, and notes are used in this manual. Aspen Avionics uses the following icons and definitions (Table 3). Icon Definition Emphasizes a crucial operating or maintenance procedure, which, if not strictly observed, could result in injury to, or death of, personnel or long Warning term health hazards.
Page 21: Example Graphics
While the PFD is reasonably intuitive and easy to use, some familiarity with EFD 1000 VFR Electronic Flight Instrument Systems (EFIS) is required. Aspen Avionics strongly recommends that new users of the PFD get some dual instruction from an experienced instrument CFI, and spend some time becoming familiar with the VFR PFD.
Page 22: Information Covered In This Pilot's Guide
Information Covered in this Pilot’s Guide This Pilot’s Guide covers all the features and options available in the EFD 1000 VFR . VFR PFD Options: - ACU (Analog converter unit) used to connect auto pilots, analog nav sources, legacy GPS. NOTE The VFR PFD supports the display of flight plan and - EHA (Evolution hazard awareness) Includes XM weather, traffic, lightning...
Page 23: Welcome And Introduction
Chapter 1 Welcome and Introduction Welcome to Aspen Avionics’ Evolution Flight Display (EFD) System, the most flexible, expandable, and upgradable Electronic Flight Instrument System (EFIS) available for general aviation aircraft. Designed to replace traditional mechanical primary flight instruments—in whole or in part, all at once, or in phases.
Page 24 The center of the EFD System is the EFD 1000 Primary Flight Display (PFD), which replaces the traditional mechanical Attitude Indicator (AI) and Directional Gyro (DG), (Figure 1-2). Course Deviation Indicator or Horizontal Situation Indicator (HSI) The PFD is available in three models—the EFD 1000 Pilot, EFD1000 VFR and the EFD 1000 Pro.
Page 25 NOTE NOTE Please spend some time with your aircraft flight manual supplement and avionics With multiple EFD installations, an independent, installer to understand exactly how your PFD is installed and configured in your standby attitude indicator must be within the pilot’ s particular aircraft, to understand the features and capabilities available to you, and to primary maximum field of view.
Page 26: System Overview
1.1. System Overview Pitot Static The PFD system typically consists of four components: Existing Aircraft Existing Aircraft EFD 1000 Display Unit (PFD) Pitot Line Static Line Configuration Module (CM) Remote Sensor Module (RSM) Aircraft Power Analog Converter Unit (ACU) EFD1000 VFR PFD Remote Sensor The ACU converts older analog signals and interfaces to the...
Page 27: Primary Flight Display Unit (Pfd)
1.1.1. Primary Flight Display Unit (PFD) Pitot & Static System Connections The Primary Flight Display Unit (PFD) is a digital system that consists of a high resolution, six-inch diagonal color LCD display, user controls, photocell, and micro SD data card slot. The three-inch diameter, four-inch deep can on the back of the display contains a non-removable electronics module that includes: • A Sensor Board with solid-state Attitude and Heading Reference System (AHRS) and 44-pin D-Sub for Electrical Connections...
Page 28: Configuration Module (Cm)
1.1.2. Configuration Module (CM) The Configuration Module (Figure 1-7), contains an EEPROM device that retains system configuration and calibration data and provides two primary functions: • Retains aircraft-specific configuration information, calibration data, and user settings, allowing the PFD to be swapped for service purposes without re-entering Figure 1-7 or re-calibrating the installation Configuration Module (CM)
Page 29: Remote Sensor Module (Rsm)
1.1.4. Remote Sensor Module (RSM) The Remote Sensor Module (RSM) (Figure 1-9), is an integral part of the EFD1000 system and works together with the display unit sensors as part of the AHRS and ADC. The RSM looks and mounts like a GPS antenna and is mounted on the exterior of the fuselage, typically aft of the cabin.
Page 30: Evolution Databases
1.1.6. Evolution Databases The EFD 1000 VFR PFD doesn’t require a data base. The Evolution MFD includes two separate databases loaded on a microSD card; one from Jeppesen and one from Seattle Avionics Software. • The Jeppesen database consists of NavData®, Obstacle, Cultural, and Terrain data. • The Seattle Avionics database features Instrument Approach Procedure (IAP) charts, Departure charts, Standard Terminal Arrival Route (STAR) charts, and airport diagrams.
Page 31: Controls And Display
Chapter 2 Controls and Display The VFR PFD is a flat-panel LCD primary flight instrument that presents the pilot with all of the information from the traditional six-pack of mechanical instruments: Airspeed, Attitude, Altitude, Turn Coordinator, Heading Indicator and Vertical Speed Indicator (VSI). Modern technology and standard EFIS symbology enable the consolidation of all six instruments into a single display, tightening the pilot’s instrument scan and reducing pilot workload.
Page 32: Controls & Display Orientation
2.1. Controls & Display Orientation ATTITUDE DISPLAY Attitude Display CONTROLS Aircraft Reference Symbol Reversion and Power Button Range Buttons Roll Pointer Menu Button Slip/Skid Indicator 1/2 Hot Key Menu 1 of 2 2/2 Hot Key Menu 2 of 2 1, 5 Altitude Tape LTNG –...
Page 33 DATA BAR Vertical Speed Tape True Airspeed (TAS) or Mach number Barometric Pressure Setting Field Wind Direction and Speed Wind Direction Arrow Outside Air Temperature (OAT) Ground Speed Selected CDI Navigation Source NAVIGATION DISPLAY Selected CDI Navigation Source Information Block Navigation Display Left Knob State Ownship Symbol...
Page 34: Controls
2.2. Controls The primary means for the pilot to control the PFD are the two knobs and center button at the bottom of the display. The knobs control setting CRS and HDG, and additional bugs and altitude settings. The lower center buttons control selection of navigation sources for the CDI.
Page 35: Left Knob Functions
2.2.1.1. Left Knob Functions NOTE The Left Knob is used to set the Course (CRS) and Airspeed Bug (IAS). Course (CRS) is the default setting for the Left Knob. When the CDI navigation source is selected to a GPS receiver and the Auto Course is enabled in the Menu, Refer to Table 2-1 and Figure 2-2 the course is set automatically by the GPS and is not pilot-adjustable (see Section 4.4.6).
Page 36: Sync Function
SYNC Function 2.2.1.3. Knob SYNC Function Press the Knob until its state shows the value you want to set in magenta. Press and hold the Knob for approximately one (1) second to SYNC the field’s value according to the rules shown in Table 2-2. After 10 seconds of inaction, the knob reverts to its home state (CRS or HDG), and the labels and field turn to cyan (inactive).
Page 37 Left Knob SYNC Action Set to the current indicated airspeed. Course Pointer points to the VOR. CRS value is the reciprocal of the current VOR VOR navigation radial. The deviation bar centers with a “TO” indication. Course Pointer points to the active GPS waypoint.
Page 38: Using The Knobs (Example)
2.2.1.4. Using the Knobs (Example) How to Set the Heading Bug (HDG) Rotate the Right Knob to the desired heading value, shown both by the position of the Heading Bug and the numeric value in the Selected Heading Field (Figure 2-5). The HDG label, Heading Bug and the Selected Heading Field appears in magenta After 10 seconds of inactivity, the knob defaults to HDG.
Page 39: Cdi Navigation Source Select Button
2.2.2.1. CDI Navigation Source Select Button NOTE The CDI Nav Source Select Button is the center button (Figure 2-7). It selects which of the available navigation sources will couple to the CDI, which in turn couples to When GPS is selected as the CDI’ s nav source, but no the autopilot (if available).
Page 40: Hot Keys
2.2.3. Hot Keys NOTE The five keys along the lower right side of the PFD function as either single-action When configured with the Evolution Hazard Awareness Hot Keys for frequently used commands or as Menu Keys when the Menu has been option, there are two levels of Hot Keys controlled activated.
Page 41 HOT KEY DESCRIPTION OPTIONS Hot Key Menu 1 of 2 Hot Key Menu selection Hot Key Menu 2 of 2 Minimums displayed and Enables and displays, or Altitude Alerter enabled disables and hides, Minimums (see Section 4.2.3.4.) Alerter 1, 2 Minimums alerter disabled 360°...
Page 42 HOT KEY DESCRIPTION OPTIONS Hot Key Menu 2 of 2 Hot Key Menu selection Hot Key Menu 1 of 2 LTNG Data Link Lightning Overlay on Toggles between Lightning STRK WX-500 Strike Overlay on LTNG Overlay options (see Section CELL WX-500 Cell Overlay on 4.8.1.) LTNG...
Page 43: Menu
2.2.4. Menu The MENU button is used to access the EFD1000 PFD’s Menu to change options, and also to change the PFD’s display brightness. 2.2.4.1. Using the Menus Press the MENU button to activate the Menu (Ref. 3). The current menu page name is shown on the bottom center of the Navigation Display.
Page 44 Each Menu Page has up to five selectable options, each adjacent to one of the five Hot Keys which double as Menu Keys when the Menu is active (Item 1 of Figure 2-17 and Table 2-4). After navigating to the Menu Page containing the option you want to change, press the Menu Key adjacent to that option label, which initiates the Menu’s Edit mode.
Page 45 The MENU text will display in one of the four colors listed and described in Table 2-4. Figure 2-18 DISPLAY Menu Text - Editable DESCRIPTION DISPLAY TEXT WHITE Figure 2-18 Editable option Figure 2-19 MAGENTA Editable option enabled Figure 2-19 Menu Text - Enabled for Editing GREEN Status Only...
Page 46 Edit Main Menu Items NOTE Press the MENU Button. Navigate to the desired Menu Page. Pressing the Right Knob returns to Navigation mode Press the Menu Key of the desired option. The Menu label turns magenta, and and allows selection of other menu options on different the EDIT VALUE label displays above the Right Knob (Figure 2-23).
Page 47: Display Lighting
2.2.4.2. Display Lighting When the MENU button is pressed and the Menu is active, the Left Knob can be used to adjust the PFD display brightness. By default, the LCD brightness operates in AUTO mode, and is adjusted based on photocell sensing of ambient lighting conditions.
Page 48: Range Buttons
2.2.5. Range Buttons When the MAP is enabled, the RNG (Range) Button is used to zoom the map in or out. Press the RNG (+) Button to increase map range. Press the RNG (-) Button to decrease map range. Additionally, an Auto Range control feature is available. Pressing and holding either the RNG (+) or (-) Button will cause the map range to scale continuously to its maximum or minimum range, respectively.
Page 49: Display
2.3. Display The PFD replaces the existing Attitude Indicator and DG in the center of the primary flight instrument cluster. Like the instruments it replaces, the top half presents an Attitude Display and the bottom half contains a Navigation Display (Figure 2-26). Between the two halves is the Data Bar.
Page 50: Cleaning The Display Screen
The PFD generally follows standard display conventions for Electronic Flight Instrument Systems (EFIS), so a pilot with some experience and familiarity with other EFIS PFDs will usually transition quickly to using the EFD1000. Pilots for whom the EFD1000 PFD is their first real exposure to EFIS and glass cockpit flying, however, should get some transition training from a certified flight instructor (CFI) with EFIS experience.
Page 51: Attitude Display
2.3.2. Attitude Display The Attitude Display includes an Attitude Director Indicator (ADI) (when connected to a compatible autopilot), an Airspeed tape, an Altimeter tape, an Altitude Alerter, Radio Altitude, approach minimums annunciations, and approach course and glide slope indicators (Table 2-6 and Figure 2-27), (see Chapter 4, Reference Guide for more details).
Page 52 ATTITUDE DISPLAY Attitude Display Aircraft Reference Symbol Roll Pointer Slip/Skid Indicator Altitude Tape Airspeed Tape Selected Altitude Field Selected Airspeed Field Altitude Alerter Airspeed Bug Numerical Altitude Value, Numerical Airspeed Value, Airspeed Altitude Drum/Pointer Drum/Pointer Altitude Trend Vector Altitude Bug Figure 2-27 Table 2-6 Attitude Display Components...
Page 53: Attitude Director Indicator (Adi)
2.3.2.1. Attitude Director Indicator (ADI) The Attitude Director Indicator (ADI) features a conventional blue (sky) over brown (ground) background, with a white horizon line dividing the two areas. A triangular Aircraft Reference Symbol (Ref. 17) is in a fixed position and shows aircraft attitude relative to the horizon.
Page 54: Airspeed Tape And Bug
2.3.2.2. Airspeed Tape and Bug Airspeed is indicated by a moving airspeed tape against a fixed position airspeed pointer, shown on the left-hand side of the Attitude Display (Figure 2-30). A numerical, rolling drum readout indicating airspeed values to the closest one knot or mile per hour is provided adjacent to the fixed pointer.
Page 55: 2.A. Mach Number Display For Mmo Aircraft
The pilot can set a target airspeed using the Left Knob (see Section 4.2.2.1.). The target airspeed is shown on the Airspeed Tape as an Airspeed Bug with its setting displayed numerically above the Airspeed Tape (Figure 4-10 and Figure 4-11). The Airspeed Bug and numerical value are for visual reference only, to help the pilot maintain a target airspeed;...
Page 56 (Figure 2-31). A numerical rolling drum readout indicating altitude values to the closest 20 feet is provided adjacent to the fixed pointer. When climbing or descending, a magenta Altitude Trend Vector displays above or below the altitude pointer, indicating the altitude that will be reached in six seconds if the current rate of climb or descent is maintained.
Page 57: Data Bar
2.3.3. Data Bar The Data Bar visually separates the upper and lower halves of the PFD display. When available, True Airspeed (TAS) or Mach Number, GPS Ground Speed (GS), Outside Air Figure 2-34 Data Bar Components Temperature (OAT), Wind Vector arrow, Wind Direction, Wind Speed, and Barometric Pressure Setting are presented in the Data Bar (Table 2-7 and Figure 2-34).
Page 58: Navigation Display
2.3.4. Navigation Display The lower half of the PFD is the Navigation Display (Table 2-8 and Figure 2-35), which shows a wide range of navigation information and flight data, including: • Course Pointer and Heading Bug. • 360° and ARC Compass rose display modes. • Numeric displays of current magnetic heading, selected heading (HDG), and selected course (CRS).
Page 59 NAVIGATION DISPLAY Navigation Display Ownship Symbol Course Pointer Rate of Turn Indicator Ground Track Marker Select CDI Navigation Source Numerical Direction Indicator Selected CDI Navigation Source Information Block Selected Course (CRS) Field Left Knob State Selected Heading (HDG) Field Right Knob State Heading Bug Hot Ket Legend Navigation Display Range...
Page 60: Numerical Direction Indicator (Magnetic Compass)
2.3.4.1. Numerical Direction Indicator (Magnetic Compass) The center of the Navigation Display is the Numerical Direction Indicator. Like a magnetic compass, the NDI always shows the current magnetic heading of the aircraft. This NDI compensates both for the turning and acceleration errors exhibited by wet compasses and for precession errors found in common Directional Gyros.
Page 61: Navigation Information
Navigation Information Regardless of Compass Mode setting, the current magnetic heading is always shown at the top center of the Navigation Display (Figure 2-2, No. 50 and Figure 2-38). The HDG Bug setting is shown in the Selected Heading Field (Figure 2-2, No. 52). This field Figure 2-38 is always visible even if the HDG Bug itself is only partially visible in ARC Compass Mode.
Page 62: Deviation Off-Scale Indication
2.3.4.3. Course Deviation Indicator (CDI) In the 360º Compass Mode, the Course Pointer and CDI displays an arrowhead pointing to the selected course, and a movable center diamond indicating course deviation against a scale of two dots to either side of the center. A TO/FROM/LOC indication is shown to the left of the course deviation scale.
Page 63: Rate Of Turn Indicator
Auto Course Select is indicated by an inverse A on a green background, adjacent to both the numerical CRS value and the CRS Left Knob State. (Figure 2-44 and Figure 2-45). Figure 2-44 Auto Course Indication on CRS Field If the GPS navigator enters the OBS or HOLD mode, Auto Course Select is automatically disabled on the EFD1000 VFR PFD until the GPS navigator resumes waypoint sequencing.
Page 64: Situational Awareness Map
of up to ±9,990 fpm. A white triangle caps the tape whenever rates exceed ±2,000 fpm (Figure 2-48). The Vertical Speed Numerical Value will be dashed whenever the vertical speed exceeds +/- 10,000 fpm. In the ARC Compass Mode, only the Vertical Speed Numerical Value is presented.
Page 65 The map display range is controlled by the RNG Button (Figure 2-2, Ref. 2), enabling the pilot to zoom in or out on the map. Automatic declutter logic changes the map features displayed depending on the selected map range. The current range and declutter level map settings are shown in the lower left-hand corner of the navigation display (Figure 2-49).
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Page 67: Flying The Vfr Pfd
Chapter 3 Flying the PFD This chapter provides an overview of flying the PFD on a cross-country flight, explaining how to access and change the necessary settings of the PFD. Refer to Chapter 4 for detailed step-by-step instructions for all PFD functionality.
Page 68 FEATURE SETTING FEATURE SETTING Barometric Selected Pressure Allows for BARO Set as desired Altitude (BARO) Hot adjustment Map RNG Left and Right No EFD 1000 (Range) Set as desired Buttons VFR functionality Buttons Barometric Navigation Pressure Adjustable Source Select Select as desired Setting Field (Middle Button)
Page 69: Quick Controls Overview
3.1. Quick Controls Overview Chapter 2 explains the PFD controls in detail. The following is a quick summary: Knobs (See Chapter 2, Section 2.2.1. for details) The Left or Right Knob each has a Home State, to which it returns after 10 seconds of inactivity.
Page 70 Navigation Source Buttons • Buttons at the bottom of the display couple the available navigation sources to the CDI. The Center Button - CDI Navigation Source Select Button (Figure 2-2, Ref. • 11) selects the nav source to couple to the CDI and to drive the autopilot (if installed).
Page 71: Example Flight Scenario
3.2. Example Flight Scenario This section will walk you through using the PFD on a flight from Albuquerque International Sunport (KABQ) to Reno/Tahoe International Airport (KRNO), flying NOTE Victor airways. This scenario uses one pilot’s technique for setting up the navigation The tasks and procedures you will use in your airplane instruments, but there are many other valid possibilities.
Page 72: Pre-Departure (Startup)
3.2.1. Pre-Departure (Startup) Once the pre-flight inspections and checklists are complete, start the engines and turn on the PFD Master switch. When power is applied to the PFD, the bezel backlighting illuminates and within a few seconds the PFD splash screen displays while it initializes and the AHRS data is validated (Figure 3-2).
Page 73 Turn the Avionics Master ON. Until the navigation radios are operational, the CDI Navigation Source annunciations on the PFD is slashed as invalid (Figure 3-4), and the GPS1, GPS2 caution annunciations on the left (Figure 3-5), and INTEG caution annunciated on the right edge of the display. The CDI Navigation Source Select will default to VLOC1 the first time the PFD is turned on.
Page 74 Once the radios are available, we listen to the ATIS and learn that the local altimeter setting is 30.15 and that Runway 8 is in use for departures. WARNING First set the standby altimeter to 30.15, and then set the PFD barometric pressure Whenever there is a new altimeter setting, set both the setting.
Page 75 Next, since we’ll be departing from Runway 8, we set our Heading Bug to runway heading, 080°. Set the Heading Bug Press the Right Knob until HDG displays above the knob and the HDG field is enabled for editing, both rendered in magenta (Figure 3-8). The Heading Bug will also be rendered in magenta, and a dashed magenta line will extend from the ownship symbol to the Heading Bug to make it easier to see the bug position.
Page 76 Select GPS1 as the CDI Navigation Source. Because we have enabled Auto Course Select, the Course Pointer automatically slews to 261º (the initial course from the airport to the first fix on the LARGO2 departure, ABQ VOR). Select the CDI Navigation Source •...
Page 77 Select Map Declutter Level NOTE The Map Declutter function can be found in the 360 MAP SETTINGS page or in the ARC The Basemap symbols and flight plan legs rendered MAP SETTINGS page of the MENU (Figure 3-13). The Map Declutter Icon is located for each of the map’...
Page 78 Change the Map Range • Press the RNG (Range) Buttons (Figure 3-14) UP (+) to increase the range, or DOWN (-) to decrease the range, until the desired range is shown (Figures 3-15 and 3-16). Figure 3-14 Range Button Ownship Symbol Current Range Figure 3-15...
Page 79 ADS-B Aspen will soon be offering a range of ADS-B receivers and transceivers to meet the pending ADS-B mandate, January 1, 2020. When connected to the EFD 1000 VFR PFD these options enable ADS-B weather and traffic hazards to be overlaid on the Navigation Display. Evolution Hazard Awareness (EHA) Aspen’s Evolution Hazard Awareness (EHA) option allows the EWR50 XM WX Data Link Weather Receiver, WX500 Stormscope®, and Traffic system to be connected to the PFD.
Page 80 Display the Data Link Weather Display the 2/2 Hot Key Menu. Press the NXRD Hot Key to turn Data Link Weather on (label turns inverse green Figure 3-17). Display the Lightning Overlay Display the 2/2 Hot Key Menu. Press the LTNG Hot Key until the desired overlay is selected (LTNG, STRK, or CELL).
Page 81 NOTE Setting the Altitude Alerter provides visual to help the pilot capture and maintain target altitudes. When set to a new altitude, the Alerter will illuminate a yellow flag adjacent to the target altitude display; 15 seconds (or 200 feet) before the aircraft will reach the target altitude (based on current rate of climb or descent).
Page 82 Our normal climb speed is 120 KIAS, so we set the Airspeed Bug as a reminder. To do so, we press the Left Knob twice, until it shows IAS in magenta above the knob. Then turn the knob until 120 shows in the Selected Airspeed Field. Set the Airspeed Bug Figure 3-24 Press the Left Knob until IAS displays above the Left Knob and the Selected...
Page 83: Departure
3.2.2. Departure As we start the takeoff roll, we note the airspeed on the PFD comes “alive” at 20 KIAS. All indications are normal, so we continue the takeoff, rotate at 80 KIAS. As we run out of Figure 3-27 usable runway to land, we bring the gear up, and soon we’re over the end of the 13,800 ft.
Page 84 Auto Course Select has already set our Course Pointer to the 255º course from ABQ to ZUN and a 220º heading sets us up for a nice intercept. We pitch a little higher to climb at 115 KIAS through 8,000 for traffic, then lower the nose to maintain our target airspeed of 120 KIAS by reference to the Airspeed Bug.
Page 85: Enroute
3.2.3. Enroute Albuquerque Center gives us a new altimeter setting of 30.11. We set 30.11 on the standby altimeter and then on the PFD. • Press the BARO Hot Key and rotate the Right Knob to set 30.11. • Press the BARO Hot Key, or any knob, button/key to exit. Soon, the CDI comes “alive”...
Page 86 With GPS Steering (GPSS), a compatible GPS navigator (in this case, a Garmin 430W) drives the autopilot directly via the autopilot’s HDG mode, telling it how to bank to stay centered on course. GPSS can drive the autopilot far more accurately than the NAV mode (which is based on course deviation indications) because the GPS always knows the ground track and how to adjust to maintain that track, implicitly accounting for changing wind conditions.
Page 87: Conclusion
Display the Lightning Overlay Display the 2/2 Hot Key Menu. Press the LTNG Hot Key until the STRK label is shown in green next to the Hot Key (Figure 3-35). The STRK mode annunciation appears in the lower left-hand corner of the Navigation Display, showing a yellow X for Strike mode, and a strike rate of 6 (moderate lightning activity) (Figure 3-36).
Page 88 CAUTION The Garmin 400/500 series navigators continue to output GPS Steering commands to follow the GPS flight plan even when the CDI source is set to VLOC. The PFD permits GPSS to be enabled even when VLOC is selected as the CDI navigation source. Whenever the GPSS is on and the autopilot is in the HDG mode, the autopilot will fly the GPS flight plan.
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Page 91: Chapter 4 Reference Guide
Chapter 4 Reference Guide The PFD is a panel-mounted Electronic Flight Instrument System (EFIS) that presents the pilot with displays of attitude, altitude, indicated airspeed, heading, rate of turn, slip/skid, and navigation course deviation information. The system also displays supplemental flight data, such as winds, TAS, OAT, groundspeed, moving maps, pilot-selectable indices (bugs), and various annunciations to increase situational awareness and enhance flight safety.
Page 92: Air Data, Attitude And Heading Reference System (Adahrs)
4.1. Air Data, Attitude and Heading Reference System (ADAHRS) One of the many benefits of glass cockpit systems like the Aspen Evolution system is that they replace old, less-reliable mechanical instruments and sensors with electronic equivalents. For aircraft primary flight instruments, spinning metal gyros are replaced with electronic gyros and accelerometers, and mechanical air data instruments (airspeed indicator, altimeter, and VSI) are replaced by electronic sensors to measure static and ram air pressures.
Page 93: Attitude
4.1.1. Attitude The Aspen ADAHRS attitude solution uses inputs from its internal three-axis accelerometers, rate gyros, and magnetometers, supplemented by ram and static air pressure inputs from the aircraft pitot-static system. Failures or incorrect input from any of these sensors (such as might occur if the pitot tube or static system become blocked) will affect the attitude solution.
Page 94: Pitot Obstruction Monitor
4.1.2. Pitot Obstruction Monitor Most light aircraft have only a single pitot and static system available for flight instrument use. As such, a common pitot and static input is shared between the PFD and analog standby instruments. Should one or both of these pitot and static lines become blocked, both the PFD and any standby airspeed and altitude indicators could display erroneous airspeed and altitude information.
Page 95: Heading
In summary, loss or degradation of the PFD attitude solution is unlikely if the pilot assures the proper operation of the pitot-static system. If the pitot or static system becomes blocked, an ADAHRS internal sensor fails, or a CROSS CHECK ATTITUDE indication is frequent or persists, the attitude indication on the PFD should be considered to be compromised.
Page 96: Free Gyro Mode
Just like other compass systems, the accuracy of the fluxgate is affected by its location on the airframe. Ferrous metal structures, electrical fields produced by motors, pumps, wiring, magnets in cabin speakers and other airframe-related sources of interference either constant or momentary (i.e. operating an electric trim motor, windshield heat, pumps, etc) can all affect the accuracy of the compass.
Page 97: Degraded Adahrs Performance
Two minutes after detection, a FREE GYRO MODE annunciation will be presented across the Navigation display, indicating the heading system no longer can be aligned with magnetic north. Some precession of the heading is possible, especially during abrupt maneuvers. If the condition persists for four more minutes (six minutes total) the attitude and heading indicators will be removed and replaced with red X indications. ...
Page 98: Attitude Display
4.2. Attitude Display 4.2.1. Attitude Indicator The Attitude Indicator consists of an aircraft reference symbol on a blue (sky) and brown (ground) background. The white horizon line separates the sky from the ground and extends to the edge of the display. The Roll Scale curves over the top of the Attitude Indicator while the Pitch Scale extends vertically in the middle.
Page 99: Roll Scale
4.2.1.1. Roll Scale The Roll Scale is displayed at the top of the Attitude Indicator and comprises a moving scale set against a fixed, white, triangle roll pointer. Tick marks are displayed at 0º, 10º, 20º, 30º, 45º, and 60º of roll. The 45º marks are triangles. 4.2.1.2.
Page 100: Airspeed Indicator
4.2.2. Airspeed Indicator The Airspeed Indicator comprises a moving tape, airspeed bug, and numerical airspeed value (drum). Textual Vspeeds, color Speed Bands, and Speed Markers are also rendered on the moving tape (Figure 4-7). Selected Airspeed Field Color Speed Bands Textual Vspeeds Initial Flap Extension Speed Marker Airspeed Tape...
Page 101 Indicated airspeed is displayed in knots, miles per hour or Mach number, set at installation, with tick marks rendered on the Airspeed tape every ten (10) units. Speed Bands and Speed Markers are configured during installation and cannot be changed or removed by the pilot.
Page 102: Selected Airspeed
4.2.2.1. Selected Airspeed The Selected Airspeed Field value and associated Airspeed Bug are shown on the Airspeed Tape. The Selected Airspeed Field value is shown at the top of the Airspeed Tape. The Airspeed Bug is displayed next to the Airspeed Tape when the Selected Airspeed value is within the visible range of the tape.
Page 103: Airspeed Display
4.2.2.2. Airspeed Display NOTE In some configurations, such as a stand-alone PFD, the airspeed tape can be turned off at the pilot’s discretion to facilitate screen declutter. This setting will be retained when The Altitude Tape can also be turned off for screen the PFD system is turned off then powered on again.
Page 104: Mach Number Display For Mmo Aircraft
4.2.2.3. MACH Number Display for Mmo Aircraft For Mmo aircraft, the PFD can show aircraft Mach number in the Data Bar with a display resolution of 0.01 Mach. The Mach number (configured during initial installation) can be displayed for either altitude or speed transition.
Page 105: Altimeter
4.2.3. Altimeter The altimeter comprises an Altitude Bug, Numerical Altitude Value (drum), Altitude Tape, Altitude Trend Vector, MINIMUMS annunciation, Selected Altitude Field value, Decision Height Annunciation, Altitude Alerter and an aural tone (when configured) DH (Figure 4-14). Altitude Alerter Altitude Tape MINIMUMS Annunciation/ Selected Altitude Field Selected MINIMUMS Field...
Page 106: Barometric Units Of Measure
An adjacent, magenta Altitude Trend Vector predicts the anticipated altitude, in the next six seconds, if the current rate of climb or decent is maintained. Like the VSI, there is a slight lag in the indication. If the ribbon meets or exceeds the display limit, the vertical trend is large. The Altitude Trend Vector does not display when the altitude remains constant.
Page 107: Selected Altitude Field
Set the Barometric Pressure Press the BARO Hot Key. The BARO label above the Right Knob and Barometric Pressure Setting Field appear in magenta (Figure 4-21). Rotate the Right Knob to change the value of the Barometric Pressure Setting Field. Press the BARO Hot Key or any knob, button/key to exit. If no action is taken, after 10 seconds of inactivity, the label, and field are rendered in cyan.
Page 108: Altitude Level-Off And Deviation Alert
4.2.3.3. Altitude Level-Off and Deviation Alert NOTE The Altitude (level-off ) Alert is ARMED and rendered on-screen as a yellow alert flag next to the Selected Altitude value when the aircraft altitude transitions to within 200 Rotating the knob quickly will change the altitude feet or 15 seconds of reaching the selected altitude (Figure 4-23).
Page 109: Altitude Display
4.2.3.6. Altitude Display NOTE In some configurations, such as a stand-alone PFD, the altitude tape can be turned off, at the pilot’s discretion, to facilitate screen declutter. Both Airspeed and Altitude tapes A typical PFD only installation sets the tapes display are affected by this action.
Page 110: Data Bar
4.3. Data Bar The Data Bar presents True Airspeed (TAS) or the Mach number, GPS Ground Speed (GS), Outside Air Temperature (OAT), Wind Direction, Wind Speed, and Barometric Pressure Setting, as shown in Figure 4-36. The Data Bar is always present on the display. Invalid or out-of-range Data Bar values are dashed.
Page 111: Ground Speed
Select the Transition Setting Press the MENU Button and rotate the Right Knob to the GENERAL SETTINGS C page. Press the MACH DSPL Hot Key and rotate the Right Knob to the desired Altitude or Speed setting. Press the MENU Button to exit. 4.3.2.
Page 112: Wind Speed, Direction, And Arrow (When Enabled)
Figure 4-38 4.3.4. Wind Speed, Direction, and Arrow (when enabled) Wind Direction Arrow The Wind Speed, Direction, and Direction Arrow are displayed in the lower right portion of the Data Bar. The Wind Speed has a range of 10–999 knots or mph, using the same unit of measure as the Airspeed Indicator.
Page 113: Navigation Display
4.4. Navigation Display The Navigation Display of the PFD, combines a Direction Indicator with a Course Deviation Indicator (CDI) (Figure 4-39). The Direction Indicator comprises a compass, numerical direction indication, heading bug, Ground Track Marker (when GPS ground track information is available), rate of turn indicator, and aircraft ownship symbol.
Page 114: Compass
All Magnetic Headings are displayed in degrees. The value range is from 001° - 360°, always displayed in three digits, and use leading zeros when applicable. The Magnetic North is expressed as 360°. 4.4.1. Compass The PFD offers two Compass Modes: 360°, CDI, and ARC CDI. The Compass Mode is 360. The aircraft’s heading is always expressed degrees magnetic.
Page 115 The ARC CDI Compass Mode uses a fixed CDI, resembling a contemporary GPS navigation deviation display. The ARC CDI Compass Mode is intended to maximize the lower display area for map and flight plan data (Figure 4-42). Figure 4-42 ARC CDI Compass Mode Page 4-25 091-00028-001 ( ) EFD1000 VFR PFD Pilot’s Guide...
Page 116 Select Compass Type Press the 360/ARC Hot Key (Figure 4-46) to alternately select either the 360° or ARC Compass Mode. The Navigation Display changes and the Hot Key label reflects the currently selected Compass Mode (Figures 4-47 and 4-48). Figure 4-47 Figure 4-48 Figure 4-46 ARC CDI Compass Mode...
Page 117: Course Pointer
4.4.2. Course Pointer For all Compass Modes, the arrowhead of the Course Pointer aligns with the corresponding value on the compass scale regardless of the aircraft heading. The ARC CDI Course Pointer is described in Table 4-2. COMPASS DESCRIPTION Figure 4-50 Stub Course Arrowhead, The Course Pointer is shown as a stub arrow or tail whenever the CRS value ARC CDI Compass Mode...
Page 118: To/From Indicator
4.4.3. TO/FROM Indicator Each of the Compass Modes has a TO/FROM indicator. The TO/FROM indicator shows whether the aircraft is heading toward a waypoint or radio navaid, or from a waypoint or radio navaid. For each Compass Mode, the TO/FROM indication is slightly different, as described in Table 4-3.
Page 119: Course Deviation Indicator And Scale
4.4.4. Course Deviation Indicator and Scale Selected course deviation is depicted by a Course Deviation Indicator and Scale. Deviation is indicated by positioning the Course Deviation Indicator on the Scale corresponding to the lateral deviation value. Course Deviation Indicator Figure 4-59 Course Deviation Indicator, DI Compass Mode Course Deviation Scale...
Page 120: Cdi Navigation Source
4.4.5. CDI Navigation Source When the PFD powers up, the default Selected CDI Navigation Source is the last source selected. The pilot can select from any of the installed navigation sources using the Middle Button. The PFD supports navigation information display from VHF Omni- directional Radio Range (VOR) navaids, and Global Positioning Systems (GPS).
Page 121 Pointer and autopilot will react immediately to the flight plan change. NOTE There are many radio configurations available. Your authorized Aspen Avionics Dealer can explain the Figure 4-63 CDI Source selection and Information configuration used on your aircraft. Page 4-31 091-00028-001 ( ) EFD1000 VFR PFD Pilot’s Guide...
Page 122 Whenever the CDI Navigation Source’s data is valid, a CDI Source Information Block for the selected source is shown in the upper left corner of the Navigation Display, as shown in Figure 4-64 and described in Table 4-4. Radio Mode Information Block Label GPS1 or GPS2 VOR1 or VOR2...
Page 123 When available, the bearing and distance to station is displayed on the third line of the information block in the format dddº/nnnn or dddº/nn.n, where ddd is the bearing in degrees and nnnn or nn.n is the distance in nautical miles (e.g., 360º/1103 or 322º/3.2, shown in Figure 4-64).
Page 124: Auto Course
4.4.6. Auto Course The pilot can either use the Auto Course (AUTOCRS) or manually set a CRS value. By default, AUTOCRS is enabled. When the selected CDI Navigation Source is a connected GPS receiver and AUTOCRS is enabled, CRS is not adjustable (current course value is automatically slewed and controlled by the desired track from the GPS).
Page 125: Cdi Selected Course
Disable Auto Course Press the MENU Button. Rotate the Right Knob to the GENERAL SETTINGS A page (Figure 4-72). Press the AUTOCRS Menu Key. The Menu label turns magenta, and the EDIT VALUE label displays above the Right Knob (Figure 4-73). Rotate the Right Knob to select DISABLE (Figure 4-74).
Page 126: Heading Bug
4.4.9. Heading Bug The PFD offers a pilot-selectable Heading Bug. The Heading Bug symbol is positioned on the compass scale according to the Selected Heading Field value (HDG) set by the pilot (Figure 4-82). When the Selected HDG Field value is outside the visible compass scale range in the ARC Compass mode, only a portion of the Heading Bug is shown at the edge of the Figure 4-82 compass arc, closest to the HDG value (Figure 4-83).
Page 127: Aircraft Heading Display
4.4.10. Aircraft Heading Display The aircraft heading is displayed in degrees magnetic (Figure 4-85). If the aircraft’s heading is unavailable or invalid, all heading and navigation information, Figure 4-85 including the CDI and bearing pointers (if previously displayed), is removed and Direction of Flight replaced with a single red X covering the entire lower display area, along with the Numerical Display...
Page 128: Basemap Overlays
4.4.12. Basemap Overlays The Basemap comprises symbols depicting the location of flight plan waypoints and legs, airports, VORs, DMEs, NDBs, and intersections. The Basemap is always oriented with magnetic heading up and centered so that the current aircraft position coincides with the aircraft’s Ownship Symbol.
Page 129: Basemap Declutter And Range
4.4.12.1. Basemap Declutter and Range To turn the Basemap on or off, the pilot selects one of the declutter levels as described in Section 5.2. The default map declutter level is Level 4. The map range corresponds to the outside radius of the compass scale, 2, 3, 5, 10, 15, 20, 30, 40, 60, 80, 100, or 200 nautical miles from the aircraft Ownship Symbol.
Page 130 The PFD has an Auto Range feature that automatically scales the range (to the closest range setting) to fit the Aircraft Ownship and the active waypoint within the Navigation Display, e.g., if the active waypoint is 84 miles away, Auto Range will select a 100nm range (the closest range setting is 100nm).
Page 131: Flight Plan
Auto Range is only available when a flight plan is active. Since Auto Range uses the distance between the present position and the next active waypoint to compute the appropriate map range, if the currently Selected CDI Navigation Source does not have a valid flight plan, then Auto Range is not selectable.
Page 132: Ground Track Marker
When a GPS source’s position data are invalid or no longer available, an amber annunciation, GPS1, GPS2, or RSM GPS, is shown in the lower left corner of the Navigation Display to indicate which has failed (Figure 4-99). 4.4.13. Ground Track Marker When configured with a GPS that provides ground track data, a Ground Track Marker is displayed on the compass scale to indicate the aircraft’...
Page 133: Vertical Speed Indicator
4.6. Vertical Speed Indicator When the 360° Compass Mode is selected, the Vertical Speed Indicator (VSI) is rendered on the right side of the Navigation Display, showing a numerical and graphical representations of vertical speed. The VSI shows the change in pressure altitude over time.
Page 134: Autopilot Integration
4.7. Autopilot Integration NOTE The PFD can connect with many different legacy autopilot systems that are typically Refer to the autopilot AFMS for information on the found in general aviation aircraft. Autopilot integration is limited to heading and operation of the autopilot. navigation modes.
Page 135: Gps Steering (Gpss)
4.7.1. GPS Steering (GPSS) WARNING GPS Steering represents a modern approach to flying between flight plan waypoints, and offers many advantages of over traditional methods of flying direct course lines GPS Steering is a powerful automation tool that between waypoints. can substantially reduce pilot workload.
Page 136 The PFD translates GPS Steering commands received over a digital data bus into a signal that is compatible with the autopilot Heading channel. Thus, by selecting GPSS NOTE on the PFD and the Heading mode of the autopilot, the autopilot is able to fly GPSS commands.
Page 137 When GPSS is enabled, and the autopilot is in HDG mode, the autopilot will follow the steering commands from the GPS. A GPSS enabled state will be indicated on the PFD in two locations: 1) the GPSS legend adjacent to the GPSS Hot Key will be shown in inverse green;...
Page 138 With GPSS enabled on the PFD and the autopilot in HDG mode, the GPSS will steer NOTE the autopilot laterally through the flight plan using GPS, even after the GNS-430 CDI automatically switches to VLOC, and the PFD navigation source similarly switches Refer to the autopilot systems Aircraft Flight Manual to VLOC.
Page 139: Typical Autopilot Operations
4.7.3. Typical Autopilot Operations Whenever the PFD’s installed configuration includes connections to GPS, VLOC, and autopilot systems, it acts as a data conduit between the navigators and the autopilot. This enables any compatible navigator to be coupled to the autopilot. EFD 1000 VFR provides no vertical auto pilot guidance and is not intended to be coupled with a multi axis auto pilot.
Page 140 HDG Mode Operation – Heading Bug Steering NOTE Set the PFD Heading Bug to the desired heading (Section 4.4.9). Verify that GPSS is not selected. When GPSS is enabled, the Heading Bug is not coupled Select the autopilot’s Heading (HDG) mode. to the autopilot.
Page 141 NAV Mode Operation – GPS Navigation NOTE With a valid flight plan programmed and active in the GPS, use the CDI Source Select button to couple the GPS to the PFD (see Section 4.4.5.). Not all autopilots operate in the manner described If AUTOCRS is disabled, set the Course Pointer to the desired course (CRS) (see here for intercepting courses.
Page 142: Hazard Awareness
ADS-B Weather and Traffic Aspen will soon be offering a range of ADS-B receivers and transceivers to meet the pending ADS-B mandate, January 1, 2020. When connected to the EFD 1000 VFR PFD these options enable ADS-B weather and traffic hazards to be overlaid on the Navigation Display. 4.8.
Page 143 Display Annunciation Description NOTE Symbol WX-500 Lightning Symbols and rate annunciation are Data Link Lightning Symbols display as cyan lighting symbols removed from the Basemap for ranges less than 20nm. at full intensity for 5 minutes after information is received. Figure 4-116 Lightning Time Annunciation displays in LTNG...
Page 144: Data Link Weather Overlay
Display Lightning Select the 2/2 Hot Key Menu. Press the LTNG Hot Key to select the desired option. The LTNG Hot Key label turns inverse green when enabled. Each press of the Hot Key cycles through the available options; LTNG, STRK, CELL, or LTNG disabled. (STRK is selected in Figure 4-122).
Page 145 NEXRAD coverage displays using the following methodology: NOTE • If US Precipitation Type is unavailable and US NEXRAD Radar is available, the US weather depiction is displayed as rain. Areas of no coverage are gray. If the aircraft is on the • If US Precipitation Type is available and US NEXRAD Radar is unavailable, the US ground before data is received, or in an area of no weather depiction is not displayed.
Page 146 When the Data Link Weather is enabled, an age annunciation is shown in the lower left corner of the Navigation Display (Figure 4-126). The age annunciation indicates the elapsed time in minutes since the information was generated. Each weather product has an age limit and is usually updated at the update frequency indicated in Table 4-6.
Page 147 The data age (except Puerto Rico NEXRAD) will display in Amber whenever the data link receiver has failed or stops reporting. When the expiration time has been reached and no updates have been received, the age annunciation is shown with a red slash and all data are removed from the Navigation Display.
Page 148: Traffic Overlay
4.8.3. Traffic Overlay The TRFC Hot Key enables the traffic display overlaid on the Navigation Display when the PFD is configured with one of the following traffic sensors: • Avidyne TAS 600/610/620 (TAS) • Bendix/King KMH 880 (TAS) • Bendix/King KTA 870 (TAS) • Garmin GTX 330 (TIS) • RYAN 9900BX (TAS) • SKYWATCH SKY 497 (TAS)
Page 149: Traffic Symbols
4.8.3.1. Traffic Symbols The PFD will display traffic symbols prioritized in the order received from the configured traffic sensor. The PFD includes three threat levels using TCAS symbology; Traffic Advisory (amber circle), Proximity Advisory (cyan diamond), and Other Traffic (hollow cyan diamond). All traffic symbols within the current display range and the Traffic Advisory Other Traffic selected altitude filter are shown relative to the Ownship Symbol (Figure 4-128).
Page 150 The PFD displays traffic information from the sensor with the threat level assigned by the sensor. The sensor and type of traffic system defines the threat data, range, bearing, altitude, and altitude trend. Each traffic symbol is positioned at a location representing the relative range and bearing to the Ownship Symbol.
Page 151: Traffic Altitude Filter
When a traffic symbol and the Ownship Symbol partially or completely overlap, the NOTE traffic symbol and data block will overlay the ownship symbol. The altitude filters listed in Table 4-8 are referenced to 4.8.3.2. Traffic Altitude Filter your aircraft and the PFD altitudes. The traffic sensor There are five Altitude Filters available: Off, Normal, Unrestricted, Above, and Below configured with the PFD may have different (i.e., lower) (Table 4-6).
Page 152: Traffic Unavailable
4.8.3.3. Traffic Unavailable When the TAS (Traffic Advisory System) sensor’s status is STANDBY, TEST or FAIL: • an Invalid Traffic Sensor annunciation (Figure 4-131) is displayed and the Traffic symbols are removed from view Figure 4-131 Traffic Sensor Invalid When the traffic interface is a TIS (Traffic Information Service) and the Traffic data is: • Unavailable –...
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Page 155: Customizing The Pfd
Chapter 5 Customizing the PFD 5.1. Menu Overview The following tables and figures provide a brief overview of each menu page and its menu options. KEY DESCRIPTION OPTIONS Displays Airspeed and DISABLE or ENABLE Altitude Tapes Figure 5-1 Radio Altitude DISABLE or ENABLE GENERAL SETTINGS A Auto Course Select...
Page 156 KEY DESCRIPTION OPTIONS Barometer Pressure Setting Units of Measure in Hg or mB Outside Air Temperature Units of Measure °C or °F Clear WX-500 Strike/Cell Count Action WX-500 Strike Test Action Auto Range DISABLE or ENABLE Figure 5-2 Table 5-2 GENERAL SETTINGS B Menu –...
Page 157 KEY DESCRIPTION OPTIONS ALTITUDE: OFF, ON>5K, ON>6K, ON>7K, ON>8K, ON>9K, ON>10K, ON>11K, ON>12K, ON>13K, ON>14K, ON>15K, ON>16K, MACH Display ON>17K, ON>18K SPEED: OFF, ON>0.1, ON>0.2, ON>0.3, ON>0.4, ON>0.5, ON>0.6, ON>0.7 Overspeed Warning Test Action Figure 5-3 Table 5-3 GENERAL SETTINGS C Menu –...
Page 158 KEY DESCRIPTION OPTIONS 360° Declutter Level 0, 1, 2, 3, 4 360° Flight Plan OFF, AUTO 360° Airports OFF, AUTO 360° VORs (High, Low and Terminal) OFF, AUTO 360° Intersections / NDB OFF, AUTO Figure 5-4 360° MAP SETTINGS Table 5-4 Menu –...
Page 159 KEY DESCRIPTION OPTIONS ARC Declutter Level 0, 1, 2, 3, 4 ARC Flight Plan OFF, AUTO ARC Airports OFF, AUTO ARC VORs (High, Low and Terminal) OFF, AUTO ARC Intersections / NDB OFF, AUTO Figure 5-5 ARC MAP SETTINGS Table 5-5 Menu –...
Page 160 KEY DESCRIPTION OPTIONS KEY DESCRIPTION OPTIONS 0 to 450 or LOCKED VSPEEDS DISABLE or ENABLE 0 to 450 or LOCKED 0 to 450 or LOCKED 0 to 450 or LOCKED 0 to 450 or LOCKED 0 to 450 or LOCKED Vref 0 to 450 or LOCKED Figure 5-6...
Page 161 KEY DESCRIPTION OPTIONS XM Serial Number Status Only XM Receiver Signal Quality Status Only XM Status Status Only Table 5-8 Menu – XM RECEIVER A 1. PFD Only when configured with an EWR50 Weather Receiver and a subscription to XM WX Satellite Weather®. Figure 5-8 XM RECEIVER A 091-00028-001 ( )
Page 162 KEY DESCRIPTION OPTIONS US NEXRAD Age Status Only Puerto Rico NEXRAD Age Status Only Lightning Age Status Only Precipitation Age Status Only US Coverage Age Status Only Figure 5-9 Table 5-9 XM RECEIVER B Menu – XM RECEIVER B 1. PFD Only when configured with an EWR50 Weather Receiver and a subscription to XM WX Satellite Weather®.
Page 163 KEY DESCRIPTION OPTIONS Canada Radar Age Status Only Canada Coverage Age Status Only Display Weather Legend Action Table 5-10 Menu – XM RECEIVER C 1. PFD Only when configured with an EWR50 Weather Receiver and a subscription to XM WX Satellite Weather®. Figure 5-10 XM RECEIVER C 091-00028-001 ( )
Page 164 KEY DESCRIPTION OPTIONS Operating from or Switch to Battery Power. Green when current state (Pressing key performs no action). White if selection is Status or Action possible. Operating from or Switch to External Power. Green when current state (Pressing key performs no action). White if selection is Status or Action possible.
Page 165 KEY DESCRIPTION OPTIONS Main Application Processor Software Version Status Only Input Output Processor Software Version Status Only Unit Serial Number Status Only Table 5-12 Menu – SYSTEM STATUS Figure 5-12 SYSTEM STATUS 091-00028-001 ( ) EFD1000 VFR PFD Pilot’s Guide Page 5-11...
Page 166: Customizing Basemap Symbol Declutter Settings
5.2. Customizing Basemap Symbol Declutter Settings The pilot can customize the Basemap symbol declutter settings to Level 4, Level 3, Level 2, Level 1, or Level 0 (OFF) by pressing the MENU Button and selecting the 360 MAP SETTINGS Menu page or the ARC MAP SETTINGS Menu page. Each Compass Mode has its own Menu page for Map Setting basemap symbol display.
Page 167 Set Map Symbol Display Press the MENU Button. Rotate the Right Knob to navigate to the appropriate Map Settings Menu page. Press the desired Map Symbol Menu Key. The menu label turns magenta, and the EDIT VALUE label displays above the Right Knob (Figure 5-14 and 5-15).
Page 168 Feature Group and Layer Order Max Range Declutter Setting (from Top to Bottom) Figure 5-16 Level 4 Figure 5-17 Level 3 Figure 5-18 Level 2 Figure 5-19 Level 1 Figure 5-20 Level 0 (Off) Overlay – enabled Traffic Overlay Symbols Always ON, regardless of declutter level via Hot Key Ownship Symbol...
Page 169: Configuring Vspeeds
5.3. Configuring Vspeeds Vspeeds are used to designate different operating speeds of the aircraft and are defined in Table 5-13. High Speed Red MOL or Vspeed DEFINITION PRE-SET ADJUSTABLE PRE-SET Vne (power-on) BANDS TEXT LABELS MARKERS Never exceed (Red Line) Vno (Structural Cruise) Maximum structural cruising speed...
Page 170 Vspeed DEFINITION PRE-SET ADJUSTABLE PRE-SET BANDS TEXT LABELS MARKERS Maximum landing gear operating speed NOTE (Multi-engine) Single-engine minimum control airspeed (Red Line) Setting the value of the white triangle, Vyse, and Vmc markers to zero (0) during installation disables the (Multi-engine) Best single-engine rate Vyse markers.
Page 171 The PFD uses color speed bands, color speed markers, and textual labels to help the pilot recall Vspeed settings and limits. The speed band markings are determined by the Federal Regulations and correspond to the aircraft operating speeds that are identified in the Aircraft Flight Manual.
Page 172 On aircraft with flaps, setting the upper and lower thresholds of the white and/or yellow bands to the same value disables the applicable band. When disabled, the band does not display. When using the Vspeed textual markers, the pilot must first ENABLE the display of the markers and then set values for each Vspeed.
Page 173 Set Textual Vspeed Labels Press the MENU Button. Rotate the Right Knob to the appropriate Vspeed Menu page (Figure 5-25). Press the appropriate Vspeed Menu Key. The Menu label turns magenta, and the EDIT VALUE label displays above the Right Knob (Figure 5-26). Rotate the Right Knob to the desired value (Figure 5-27).
Page 174: Lcd Brightness Control
5.4. LCD Brightness Control The LCD brightness of the PFD operates in either of two modes, Automatic or Manual (Figures 5-28 and 5-29). The LCD brightness range is displayed as a value from 1–100, displayed above the Left Knob. LCD MODE DESCRIPTION AUTOMATIC LCD backlight intensity is automatically adjusted based on the ambient...
Page 175: Expanded Emergency And Abnormal Procedures
Chapter 6 Expanded Emergency and Abnormal Procedures This section supplements and provides an expanded description of the emergency and abnormal procedures included in the FAA-approved Aircraft Flight Manual Supplement. The information provided here is intended to provide additional background information to enhance the pilot’s understanding of the emergency and abnormal conditions and the associated procedures provided in the AFMS.
Page 176: Pitot/Static System Blockage
6.1. Pitot/Static System Blockage A pitot line blockage will result in the airspeed indicator behaving like an altimeter when the aircraft’s altitude changes, and it will not respond to airspeed changes. A pitot line blockage can also affect the PFD’s attitude indication. A static line blockage will result in altitude remaining fixed and a zero vertical speed despite aircraft pitch and/or power setting changes.
Page 177 Blocked Pitot or Static Line Suspected Turn Pitot heat ON Open the Alternate Static Source Refer to alternate attitude, airspeed, altitude, and heading sources for primary flight information Consider exiting IMC Land as soon as practicable CAUTION Most light aircraft have only a single pitot and static port available for flight instrument use.
Page 178: Identifying And Handling Suspected Pitot And/Or Static System Failures
6.1.1. Identifying and Handling Suspected Pitot and/or Static System Failures Blocked pitot and/or static system ports will compromise the PFD’s attitude solution and soon cause it to Red-X (fail). Immediately begin flying by reference to backup attitude sources. Therefore, the pilot must be especially vigilant about verifying proper operation of the pitot and static systems both before and during flight.
Page 179 On the initial climb-out after takeoff, it is also good practice to note and call out passing through a pre-determined altitude above ground level (AGL) a couple of minutes after takeoff and ideally before entering the clouds (e.g., “2,000 feet”). If your primary and backup instruments are not showing the altitude and airspeed you normally expect to see at that point, you might have partially blocked static system ports.
Page 180 Airspeed going to zero is by far the most common symptom of a blocked pitot tube. If you see either of these indications of a blocked pitot tube, the first thing to do is turn on the pitot heat to remove any ice blockage. This will quickly restore the attitude and airspeed indications on the PFD systems (it takes about 40 seconds to recover after the pitot pressure is restored).
Page 181: Frequent Or Persistent Cross Check Attitude Annunciation
6.2. Frequent or Persistent CROSS CHECK ATTITUDE Annunciation Refer to alternate attitude, airspeed, altitude, and heading sources for primary flight information. Consider the following: CROSS CHECK ATTITUDE Reference standby mechanical attitude indicator. Turn Pitot heat ON. Consider exiting IMC. Land as soon as practicable For a detailed explanation of when and why the PFD may display a CROSS CHECK ATTITUDE annunciation, either momentarily or persistently, see Chapter 4, Section 4.1.
Page 182: Abnormal Shutdown Procedure
6.4. Abnormal Shutdown Procedure The PFD is typically powered through an PFD master switch that is connected to the aircraft’s Battery bus. Normally, the PFD will power down when the PFD Master switch is turned OFF or when aircraft power is removed when on the ground. To force the PFD to power down, the following procedures are provided.
Page 183: Loss Of Aircraft Electrical Power
6.5. Loss of Aircraft Electrical Power In the event that aircraft generated power is degraded or fails, the PFD will automatically switch to its own dedicated battery (Figure 6-2). When continued safe operation depends on the PFD, UNRESTORABLE LOSS OF EXTERNAL POWER IS AN EMERGENCY SITUATION.
Page 184 NOTE WARNING When operating on the internal battery, the display When fully charged, the internal battery will power the PFD to provide ADAHRS and backlight intensity is limited to a value of 70. emergency RSM GPS position (if enabled) for approximately 30 minutes. When continued safe operation depends on the PFD’...
Page 185: Overvoltage Protection
6.5.1. Overvoltage Protection In the event of an overvoltage condition in the aircraft’s electrical system, (greater than 33 volts) the PFD will automatically switch to its battery power and continue to operate without any pilot action. Operation from the aircraft electrical system will not be possible while the overvoltage condition is present.
Page 186 If all aircraft panel-mounted GPS receivers experience a failure, the RSM Emergency NOTE GPS receiver will provide position data that is shared among all EFDs. In addition, a text alert is presented at the bottom center of the Navigation Display annunciating RSM When airborne, if the PFD’...
Page 187: Power Override
6.7. Power Override NOTE In the event that the pilot wishes to override the PFD’s automatic power configuration, When airborne, if the PFD’ s input voltage is below the proceed as follows: 12.8V (14V Electrical System) or 25.6V (28V Electrical Power Override System) automatic battery transition threshold, and EXT PWR is selected through the POWER SETTINGS...
Page 188: In-Flight Ahrs Reset
6.8. In-Flight AHRS Reset In the unlikely event the PFD determines a potential degradation of attitude information, a warning annunciation, CROSS CHECK ATTITUDE, is shown (Figure 6-5). If the attitude pitch or roll data become invalid, a red X and the textual annunciation of ATTITUDE FAIL replaces the Attitude Indicator, and all aircraft roll, pitch, and Figure 6-5 slip information is removed from the Attitude Display (Figure 6-6).
Page 189 Perform an In-Flight AHRS Reset Maintain straight and level flight. Consider exiting IMC. Fly by visual reference or by standby instruments. Disconnect the autopilot. Press the MENU Button. Rotate the Right Knob to display the GENERAL SETTINGS A Menu page. Press the AHRS RESET? Menu Key (Figure 6-7).
Page 190: Gpss Operation, Annunciations, And Autopilot Modes
6.9. GPSS Operation, Annunciations, and Autopilot Modes The Pro PFD offers GPSS. Three modes, Enabled, Wings Level, and Disabled, are possible and annunciated in the PFD’s Navigation Display. When enabled, the configured GPS source not only provides the Basemap and flight plan data, but also passes GPSS as the heading input to a configured autopilot.
Page 191 The Wings Level mode removes roll steering inputs to the autopilot, causing the aircraft to roll wings level, and displays a red slash through the annunciated A HDG and GPSS# source. The amber GPSS Hot Key label requires pilot action. If this occurs, do the following: When GPSS Automatically Changes to Wings Level Mode Check the configured GPS source.
Page 192: Warning, Caution, And Advisory Summary
6.10. Warning, Caution, and Advisory Summary WARNINGS Presented when the PFD is operating on the internal battery. The countdown timer begins at 15 seconds and is then replaced by the ON BAT annunciation with the battery’s % charge remaining. NOTE Figure 6-12 Figure 6-13 If the battery temperature is less than 0°...
Page 193 WARNINGS When the Attitude Indicator display extreme pitch up or extreme pitch down attitudes, the red chevrons indicate the direction to restore level flight. Figure 6-17 Figure 6-16 Chevrons indicate Pitch Down Chevrons indicate Pitch Up Table 6-1 Warning Annunciations 091-00028-001 ( ) EFD1000 VFR PFD Pilot’s Guide Page 6-19...
Page 194 CAUTION Presented when the PFD AHRS internal integrity monitor determines that attitude is potentially degraded. When a CROSS CHECK ATTITUDE annunciation is presented, the pilot should cross check attitude, airspeed, and altitude indications with other sources of primary flight information. Figure 6-18 Cross Check Attitude The CHECK PITOT HEAT annunciation accompanies the ATTITUDE FAIL annunciation and is...
Page 195 CAUTION Figure 6-21 Figure 6-20 RSM GPS GPS Invalid Presented when a configured GPS source’s data is invalid or unavailable. GPS# or RSM REVERSION annunciations indicate the current GPS Basemap source Figure 6-22 Figure 6-23 GPS Reversion GPS Reversion Emergency Presented when the PFD’s Selected CDI Navigation Source is a GPS and that GPS is sending an Integrity alert.
Page 196 CAUTION Presented when the previously enabled and valid GPSS source is lost or has changed. Indicates the GPSS Wings Level mode Figure 6-27 GPSS Source Lost/Changed Data Link Weather product data not received for 30 seconds after an error is detected Figure 6-28 Data Link Weather Data Error 1.
Page 197 ADVISORY Presented when the REV Button is pressed. Figure 6-30 REV Button Off Presented when GPSS is enabled and the GPS source is valid. Either GPSS1 or GPSS2 may be annunciated, depending on selection and the number of configured GPS navigators. This also indicates the autopilot heading source NOTE Figure 6-31...
Page 198 ADVISORY Associated with the GPS and the Selected CDI Navigation Source. See the GPS AFMS for more information. NOTE Figure 6-32 These annunciations do not display for RS232-based GPS. GPS Annunciations Indicates the traffic sensor is enabled Figure 6-33 Traffic Enabled WX-500 Strike display mode selected.
Page 199 ADVISORY A horizontal red line through any legend indicates that the data is invalid or unavailable. Figure 6-37 Data Invalid or Unavailable A horizontal red line through the Selected CDI Navigation Source indicates that the data from the source is invalid or unavailable. Figure 6-38 Navigation Source Invalid or Unavailable GPSS Hot Key label with a blue background and gray letters indicate that the GPSS is disabled.
Page 200 Page Intentionally Left Blank Page 6-26 EFD1000 VFR PFD Pilot’s Guide 091-00028-001 ( )
Page 201: Chapter 7 Appendices
Chapter 7 Appendices 7.1. Operating Limitations Refer to the latest version of the Airplane Flight Manual Supplement (AFMS), Aspen Avionics document 900-00008-001 for the limitations that apply to your specific aircraft installation. The AFMS and this Pilot’s Guide must be carried in the aircraft and be immediately available to the pilot while in flight.
Page 202 .View the Main Application Processor Software Version Press the MENU Button. Rotate the Right Knob to the SYSTEM STATUS Menu page. The MAP VER Menu Key displays the current Main Application Processor Software Version (Figure 7-1). Press the MENU Button to exit. Figure 7-1 View Main Application Processor Software Version...
Page 203: Evolution Database
7.3. Evolution Databases NOTE The Evolution Flight Display System EFD 100 PRO PFD with EFD1000/500 MFD includes two separate databases loaded on a microSD card; one from Jeppesen and one from The Pro PFD only requires a preloaded microSD card Seattle Avionics Software.
Page 204 • Register for Jeppesen data • Set Up Your Customer Port Login Aspen Avionics will automatically forward your Evolution Flight Display product registration information to Jeppesen for activation of the complimentary service. Page 7-4 EFD1000 VFR PFD Pilot’s Guide 091-00028-001 ( )
Page 205: Monthly Jeppesen Updates
You will receive a confirmation email directly from Jeppesen indicating service activation as well as instructions on how to use the Jeppesen Services Update Manager (JSUM). Although we make every effort to turn the registrations around very quickly, the entire process may take up to 3-4 days If you already have a login and password and need to register an additional Evolution Flight Display unit...
Page 206: Seattle Avionics Software Database
Click on the service you want to download to the microSD card. Click on the Start button in JSUM to initiate the download. For complete detailed instructions, refer to jeppesen.com. Once the download is completed with the latest Jeppesen data, download the latest Seattle Avionics data. 7.3.2.
Page 207: Seattle Avionics Software Updates
From the Seattle Avionics ChartData Manager, select Aspen Click on the Download Now button to initiate the download. Only microSD cards received from Aspen Avionics For complete detailed instructions, refer to seattleavionics.com/aspen and click on How or Jeppesen may be used. Use of any other card can...
Page 208: Loading The Microsd Card Into The Efd Unit
Lost or misplaced microSD card? Contact Jeppesen Customer Service (800-621-5377) or email captain@jeppesen.com to purchase a replacement or additional microSD card(s) pre-loaded with terrain data. 7.4.1. Loading the microSD Card into the EFD Unit The microSD card slot on the EFD is a small horizontal slot located on the bottom center part of the bezel (Figure 7-5).
Page 209: Removal Procedure
Select the functions that use the databases (moving map, terrain, charts, and synthetic vision). Verify the functions can be accessed. Database Confirmation Screen The Database Confirmation Screen is presented at system startup and displays the validity dates of the currently loaded: •...
Page 210: Specifications
7.5. Specifications 7.5.1. Primary Flight Display Unit (PFD) GENERAL SPECIFICATIONS Width 3.50 in. (Measured at Bezel) Height 7.00 in. (Measured at Bezel) Can Depth 4.15 in. (Rear of Bezel to Rear of Can) Overall Depth 6.35 in. (Knob to Rear Pressure Fitting) Weight 2.9 lbs.
Page 211 Input Voltage +8 to +32 Volts DC Max Current 2.4 Amps @ 28 VDC 4.8 Amps @ 14 VDC I/O SPECIFICATIONS ARINC 429 Inputs ARINC 429 Outputs RS-232 Inputs RS-232 Outputs Pitot / Static Quick Connect CERTIFICATION SPECIFICATIONS FAA Technical Standard Order TSO-C2d / ETSO-C2D...............Airspeed Instruments TSO-C3d / ETSO-C3D..............Turn and Slip Instrument EASA (European Aviation Safety Agency)
Page 212: Remote Sensor Module (Rsm)
7.5.2. Remote Sensor Module (RSM) Width 2.65 in. Length 4.40 in. Height 1.00 in. Weight 0.2 lbs. Input Voltage Provided by PFD Max Current Included in PFD Current Table 7-2 Remote Sensor Module (RSM) Specifications 7.5.3. Analog Converter Unit (ACU) Width 5.75 in.
Page 213 7.5.4. Operational Specifications Airspeed Range Minimum displayed airspeed 20 KIAS Maximum displayed airspeed 500 KIAS Altitude Range Minimum displayed altitude -1,600 ft. MSL Maximum displayed altitude 51,000 ft. MSL Vertical Speed Maximum displayed vertical speed rates (tape) +/-2,000 fpm Range Maximum displayed vertical speed rates (numerical +/- 9,990 fpm value)
Page 214 7.6. Glossary AWOS Automated Weather Observation System Back Course Localizer back course approach where the ºC Degrees Celsius signal on the back side of the localizer is used ºF Degrees Fahrenheit for alignment to the runway opposite of normal localizer alignment. Accuracy Estimated position accuracy in feet or meters Battery Time...
Page 215 Evolution Flight Display Crosstrack Error The distance the aircraft is off the desired course. EFIS Electronic Flight Instrument System Course Elevation The height above mean sea level. Course to Steer ETA (Destination) Estimated Time of Arrival. The estimated time decibels ‘Z’ (radar return) you will reach a Go To destination or the final Direct Current waypoint in a route.
Page 216 Ground Speed The velocity that the aircraft is travelling relative Liquid Crystal Display to a ground position. Lateral Deviation Indicator Glide Slope or Ground Speed The portion of a flight plan between two Heading The direction an aircraft is pointed, based upon waypoints indications from a magnetic compass or a Localizer...
Page 217 TACAN Tactical Air Navigation System True Air Speed TCAS Traffic Collision Avoidance System TERM Terminal Mode Traffic Information System Track Direction of aircraft movement relative to a ground position; also Ground Track’ Technical Standard Order Volts, Alternating Current Volts, Direct Current Vertical Deviation Indicator Visual Flight Rules Very High Frequency...
Page 218 7.7. Index Symbols 1/2, Hot Key ..........................2-11 Airspeed Indicator (Airspeed) ................4-10 – 4-13 2/2, Hot Key ..........................2-12 Airspeed ..........................4-10 360/ARC, Hot Key .........................2-11 Bug ............................4-10 Bug, Set ........................3-17, 4-12 Range ..........................4-11 Airspeed Display ......................4-13 ADAHRS ........................... 4-2 – 4-7 Tape ............................4-10 Attitude .............................4-3 Hide/Display ........................4-13 Free Gyro Mode ......................
Page 219 Analog Converter Unit ......................1-6 Operational ..........................6-18 Approvals ............................x Status, View ..........................6-13 ARC/360, Hot Key .........................2-11 Nav Sources, Select ......................3-10 Attitude Display ................... 2-22 – 2-26, 4-8 Source Select Buttons ......................2-9 Airspeed Indicator ....................4-10 – 4-13 Brightness Control .......................5-20 Altimeter ........................4-15 – 4-19 See also Lighting Attitude Indicator .......................4-8 BRT ADJUST ..........................2-17...
Page 220 Source Label ........................4-31 Warnings, Cautions, Notes ....................xx Source Select Button .....................4-31 Copyrights, Trademarks and Patents ................ix Check Pitot Heat ........................6-20 Course Deviation Indicator and Scale ..............4-29 CHECK PITOT HEAT .........................4-4 Course Pointer ........................4-27 Cleaning the Display Screen ..................2-20 Course Pointer and Deviation Indicator ..............4-32 Color Philosophy ........................xix Covered Functionality ......................xvii Compass ............................4-24...
Page 221 Display ....................... 1-5, 2-19 – 2-35 Attitude Display ........................2-21 Annunciations ........................6-23 Cleaning the Display Screen ..................2-20 Failures ............................6-11 Lighting ..........................2-17 Integrity Flag ........................6-21 Document Revisions ........................ iv Invalid ............................6-21 Dual Display ..........................1-2 Reversion ..........................6-21 Reversion Emergency ....................6-21 GPSS Disable ............................6-17 Electrical Power, Loss of Aircraft ..................6-9 Enable/Disable ........................4-46 Emergency and Abnormal Procedures .............
Page 222 ARC MAP SETTINGS ......................5-5 GENERAL SETTINGS A ....................5-1 ..........................2-5 – 2-8 GENERAL SETTINGS B ....................5-2 Information Covered in this Pilot’s Guide ..............xvii POWER SETTINGS ......................5-10 Initial Flap Extension Speed Marker .................4-10 SYSTEM STATUS ......................5-11 Internal Battery Status, View ..................6-13 VSPEEDS A ..........................5-6 Introduction ........................
Page 223 Micro Electro-Mechanical Systems ................4-2 Navigation Source MicroSD Card ........................1-8, 7-7 Select Buttons CDI Nav Source Select Button ................2-9 NEXRAD Methodology .....................4-55 Notes Navigation See also Advisory Information ..........................2-31 Explained ........................... xx Source .............................4-23 NRM, Hot Key ..........................2-12 Source Info Block ......................4-23 Numerical Airspeed Value ....................4-11 Source Invalid or Unavailable ...................6-25 Numerical Altitude Value ....................4-15...
Page 224 REV Button ..........................2-18 ............................6-23 Terminology ..........................xvii Right Knob Functions ......................2-5 Buttons ............................ xviii Roll Scale ............................4-9 Hot Keys ..........................xviii RSM Emergency GPS Use ....................6-11 Knobs ............................xviii RSM GPS .............................6-21 Menu Keys ..........................xviii TO/FROM Indicators ....................4-23, 4-28 Track Marker ........................4-23, 4-42 Service Agreement, XM WX Satellite Radio ..............xv Traffic ............................4-58 Shutdown Procedure ......................6-8...
Page 225 Direction ..........................4-20 Direction Arrow ........................4-20 Warning, Caution, and Advisory Summary ...........6-18 – 6-25 Speed ............................4-20 Warnings ........................6-18 – 6-19 Speed, Direction, and Arrow ..................4-22 Attitude Fail .........................6-18 Wings Level ..........................4-48 Battery Countdown ......................6-18 WX-500 Battery Operational ......................6-18 Cell Rate ..........................6-24 Direction Indicator Fail ....................6-18 Self-Test ..........................6-24 Explained ...........................
Page 226 Page 7-26 EFD1000 VFR PFD Pilot’s Guide 091-00028-001 ( )
Page 228 Aspen Avionics, Inc. 5001 Indian School Road NE Albuquerque, NM 87110 Phone: 888-99ASPEN (888-992-7736) Phone, International: (505) 856-5034 Fax: (505) 314-5440 info@aspenavionics.com www.aspenavionics.com 091-00028-001 ( ) Printed in USA...

Aspen Avionics Evolution EFD1000 VFR PFD Pilot's Manual

Copyrights, Trademarks and Patents

Approvals

LIMITED WARRANTY Aspen Avionics, Inc

Weather Data Warranty

XM WX Satellite Radio Service Agreement

Conventions

Chapter 1 Welcome and Introduction

Chapter 2 Controls and Display

Chapter 3 Flying the VFR PFD

Chapter 4 Reference Guide

Chapter 5 Customizing the PFD

Chapter 6 Expanded Emergency and Abnormal Procedures

Chapter 7 Appendices

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