1. With New Jersey Wing Annotations
Aspen Transition Ground Training
National Civil Air Patrol
With New Jersey Wing Annotations 1

2. Flying the C-172 TAA

3. Introduction Aspen EFD 1000 PFD System Overview Operation
Flight Scenario 3

4. N4814C

5. Conventions Conventions for the Aspen
The following conventions, definitions, terminology, and colors are used in this manual and on the EFD1000 PFD.
Covered Functionality
This guide covers all the functionality available in the EFD1000 Pilot PFD. Some functionality is unavailable in the EFD1000 Pilot PFD and is noted in the text.
Terminology 5

6. Conventions Color Philosophy RED
Flight envelope and system limits, and for warning annunciations - immediate pilot recognition and which may require immediate pilot correction or compensatory action.
Color Philosophy
RED
Used to indicate flight envelope and system limits, and for warning annunciations that require immediate pilot recognition and which may require immediate pilot correction or compensatory action. Red is used to indicate Data Link Weather precipitation areas. 6

7. Conventions Color Philosophy GREEN
Navigation information or mode data related to or provided by the navigation source currently selected for display on the Course Deviation Indicator (CDI).
Green is also used to indicate Data Link Weather precipitation areas and the status of user controls
Color Philosophy
GREEN
Used for navigation information or mode data related to or provided by the navigation source currently selected for display on the Course Deviation Indicator (CDI) (i.e., navigation deviations, equipment operating state, waypoint information). Green is also used to indicate Data Link Weather precipitation areas and the status of user controls (i.e., ON, enabled, or active). 7

8. Conventions Color Philosophy AMBER
Abnormal information sources, and for caution information that requires immediate pilot awareness and for which subsequent pilot action may be required.
Color Philosophy
AMBER
Used to indicate abnormal information sources, and for caution information that requires immediate pilot awareness and for which subsequent pilot action may be required. Amber is used to indicate Data Link Weather precipitation areas. 8

9. Conventions Color Philosophy WHITE
Primary flight data (e.g., IAS, ALT, HDG), scales, and menu items that are selectable for editing
Color Philosophy
WHITE
Used to show primary flight data (e.g., IAS, ALT, HDG), scales, and menu items that are selectable for editing. 9

10. Conventions Color Philosophy MAGENTA
Pilot-selectable references (bugs) enabled for editing, for depicting the active GPS navigation leg on a moving map display, and for depicting the flight director bar
Color Philosophy
MAGENTA
Used for pilot-selectable references (bugs) enabled for editing, for depicting the active GPS navigation leg on a moving map display, and for depicting the flight director bar. 10

11. Conventions Color Philosophy GRAY
Show supplemental flight data, and for hotkey and menu legends that are OFF, disabled, or inactive
Color Philosophy
GRAY
Used to show supplemental flight data, and for hotkey and menu legends that are OFF, disabled, or inactive. 11

12. Conventions Color Philosophy CYAN
Indicate editable values that are not currently selected for editing. CYAN is also used to display bearing pointers, proximity and other traffic icons, and GPS track marker
Color Philosophy
CYAN
Used to indicate editable values that are not currently selected for editing. CYAN is also used to display bearing pointers, proximity and other traffic icons, and GPS track marker. 12

13. Conventions Color Philosophy BLUE
Indicates the sky and Data Link Weather precipitation areas
Color Philosophy
RED Used to indicate flight envelope and system limits, and for warning annunciations that require immediate pilot recognition and which may require immediate pilot correction or compensatory action. Red is used to indicate Data Link Weather precipitation areas.
GREEN Used for navigation information or mode data related to or provided by the navigation source currently selected for display on the Course Deviation Indicator (CDI) (i.e., navigation deviations, equipment operating state, waypoint information). Green is also used to indicate Data Link Weather precipitation areas and the status of user controls (i.e., ON, enabled, or active).
AMBER Used to indicate abnormal information sources, and for caution information that requires immediate pilot awareness and for which subsequent pilot action may be required. Amber is used to indicate Data Link Weather precipitation areas.
WHITE Used to show primary flight data (e.g., IAS, ALT, HDG), scales, and menu items that are selectable for editing.
MAGENTA Used for pilot-selectable references (bugs) enabled for editing, for depicting the active GPS navigation leg on a moving map display, and for depicting the flight director bar.
GRAY Used to show supplemental flight data, and for hotkey and menu legends that are OFF, disabled, or inactive.
CYAN Used to indicate editable values that are not currently selected for editing. CYAN is also used to display bearing pointers, proximity and other traffic icons, and GPS track marker.
BLUE Used to indicate the sky and Data Link Weather precipitation areas.
BROWN Used to indicate the ground. 13

14. Conventions Color Philosophy BROWN Indicates the ground
Used to indicate the ground. 14

15. Conventions Warnings, Cautions, and Notes Warnings
Where applicable warnings, cautions, and notes are given. Aspen Avionics uses the following icons and definitions:
Warnings
Emphasizes a crucial operating or maintenance procedure, which, if not strictly observed, could result in injury to, or death of, personnel or long term health hazards. Indicates a hazard that may require immediate corrective action.
Warnings, Cautions, and Notes
Where applicable warnings, cautions, and notes are given. Aspen Avionics uses the following icons and definitions
Warnings
Emphasizes a crucial operating or maintenance procedure, which, if not strictly observed, could result in injury to, or death of, personnel or long term health hazards. Indicates a hazard that may require immediate corrective action. 15

16. Conventions Warnings, Cautions, and Notes Cautions
Where applicable warnings, cautions, and notes are given. Aspen Avionics uses the following icons and definitions:
Cautions
Indicates an essential operating or maintenance procedure, which, if not strictly observed, could result in damage to, or destruction of, equipment. Indicates the possible need for future corrective action.
Warnings, Cautions, and Notes
Where applicable warnings, cautions, and notes are given. Aspen Avionics uses the following icons and definitions
Caution
Indicates an essential operating or maintenance procedure, which, if not strictly observed, could result in damage to, or destruction of, equipment. Indicates the possible need for future corrective action. 16

17. Conventions Warnings, Cautions, and Notes Notes
Where applicable warnings, cautions, and notes are given. Aspen Avionics uses the following icons and definitions:
Notes
Highlights an important operating or maintenance procedure, condition, or statement.
Warnings, Cautions, and Notes
Where applicable warnings, cautions, and notes are given. Aspen Avionics uses the following icons and definitions
Note
Highlights an important operating or maintenance procedure, condition, or statement. Safe operation. 17

18. System Component Overview
System Overview
The EFD1000 PFD system typically consists of four components
EFD1000 Display Unit
The EFD1000 Pro PFD system typically consists of four components:
1. EFD1000 Display Unit
2. Configuration Module (CM)
3. Remote Sensor Module (RSM)
4. Analog Converter Unit (ACU) - The ACU converts older analog signals and interfaces to the industry-standard digital ARINC 429 interface, which is the native language of the EFD1000. In some installations, generally when the aircraft is not equipped with an autopilot and has only digital GPS/nav/comms, the ACU may be omitted. 18

19. System Component Overview
System Overview
The EFD1000 PFD system typically consists of four components
Configuration Module (CM)
The EFD1000 Pro PFD system typically consists of four components:
1. EFD1000 Display Unit
2. Configuration Module (CM)
3. Remote Sensor Module (RSM)
4. Analog Converter Unit (ACU) - The ACU converts older analog signals and interfaces to the industry-standard digital ARINC 429 interface, which is the native language of the EFD1000. In some installations, generally when the aircraft is not equipped with an autopilot and has only digital GPS/nav/comms, the ACU may be omitted. 19

20. System Component Overview
System Overview
The EFD1000 PFD system typically consists of four components
Remote Sensor Module (RSM)
The EFD1000 Pro PFD system typically consists of four components:
1. EFD1000 Display Unit
2. Configuration Module (CM)
3. Remote Sensor Module (RSM)
4. Analog Converter Unit (ACU) - The ACU converts older analog signals and interfaces to the industry-standard digital ARINC 429 interface, which is the native language of the EFD1000. In some installations, generally when the aircraft is not equipped with an autopilot and has only digital GPS/nav/comms, the ACU may be omitted. 20

21. System Component Overview
System Overview
The EFD1000 PFD system typically consists of four components
Analog Converter Unit (ACU)
The EFD1000 Pro PFD system typically consists of four components:
1. EFD1000 Display Unit
2. Configuration Module (CM)
3. Remote Sensor Module (RSM)
4. Analog Converter Unit (ACU)1
The ACU converts older analog signals and interfaces to the industry-standard digital ARINC 429 interface, which is the native language of the EFD1000. In some installations, generally when the aircraft is not equipped with an autopilot and has only digital GPS/nav/comms, the ACU may be omitted.
The system architecture in Figure 1-5 shows the relationships of the PFD, RSM, Configuration Module and ACU. 21

22. EFD 1000 Display Unit
Integral ADAHRS, backup battery (30 minutes of use minimum) and emergency GPS guidance
Integral altitude alerter/pre-select
GPS flight plan map views: 360º & Arc
Slaved directional gyro with heading bug

23. EFD 1000 Display Unit The EFD1000 PFD
Flat-panel LCD primary flight instrument with single display information delivered by the traditional six-pack of mechanical instruments:
Airspeed
Attitude
Altitude
Turn Coordinator
Heading Indicator- HSI
Vertical Speed Indicator (VSI)
The EFD1000 PFD is a flat-panel LCD primary flight instrument that presents the pilot on a single display with all the information delivered by the traditional six-pack of mechanical instruments: Airspeed, Attitude, Altitude, Turn Coordinator, Heading Indicator (or HSI) 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. 23

24. EFD 1000 Display Unit The PFD Single vertical instrument
Highly customizable
The Attitude and Navigation displays: From stripped-down, minimalist presentations, to dense, information- rich displays — depending on pilot preference and phase of flight.
Replaces the existing Attitude Indicator and Heading Indicator/HSI.
The display is divided into three parts:
Upper Attitude Display
Lower Navigation Display
Data Bar in the middle of the upper and lower halves.
The PFD is a single vertical instrument that replaces the existing Attitude Indicator and Heading Indicator/HSI. The display is divided into three parts: an upper Attitude Display, a lower Navigation Display, and a Data Bar in the middle of the upper and lower halves. The Attitude and Navigation displays are highly customizable — from stripped-down, minimalist presentations, to dense, information-rich displays — depending on pilot preference and phase of flight. 24

25. Controls
Controls
The primary controls for the pilot controlling the EFD1000 are:
Two knobs and three buttons at the bottom of the display.
The knobs control setting CRS and HDG, and bugs and altitude settings.
The three buttons control selection of navigation sources for the CDI and bearing pointers.
The primary means for the pilot to control the EFD1000 are the two knobs and three buttons at the bottom of the display. The knobs control setting CRS and HDG, and additional bugs and altitude settings. The three buttons control selection of navigation sources for the CDI and bearing pointers.
Additionally, five Hot Keys to the right of the Navigation Display toggle various features on and off. The function of each is indicated by the label on the screen to the left of each button. Three additional buttons above the Hot Keys control entering and exiting the Main Menu, setting the Map range, and reversion or manual power control. 25

26. Controls
Controls
The additional primary controls for the pilot controlling the EFD1000 are:
Five Hot Keys to the right of the Navigation Display toggle various features on and off. The function of each is indicated by the label on the screen to the left of each button.
Three buttons above the Hot Keys control entering and exiting the Main Menu, setting the Map range, and reversion or manual power control.
The primary means for the pilot to control the EFD1000 are the two knobs and three buttons at the bottom of the display. The knobs control setting CRS and HDG, and additional bugs and altitude settings. The three buttons control selection of navigation sources for the CDI and bearing pointers.
Additionally, five Hot Keys to the right of the Navigation Display toggle various features on and off. The function of each is indicated by the label on the screen to the left of each button. Three additional buttons above the Hot Keys control entering and exiting the Main Menu, setting the Map range, and reversion or manual power control. 26

27. Right Knob Right Knob Inactive by Default
Home position is Heading: HDG
Altitude Bug-ALT
Heading Bug-HDG
Altimeter Setting-BARO
Approach Minimums Alerter-MIN
Pushing knob changes color of action from cyan to magenta

28. Setting the Heading Bug
From the Home state, press the Right Knob once to select HDG for editing. The Knob label (HDG), the Heading Bug, and the Selected Heading field will all turn magenta.
Rotate the Knob to the desired heading value, shown both by the position of the Heading Bug and the numeric value in the Selected Heading field.
After 10 seconds of inaction, the knob reverts to its Home state (HDG), and the Heading Bug and Selected Heading field value will be in cyan color (inactive) state.
From the Home state (at least 10 seconds since last using the Right Knob), press the Right Knob once to select HDG for editing. The Knob label (HDG), the Heading Bug, and the Selected Heading field will all turn magenta.
Rotate the Knob to the desired heading value, shown both by the position of the Heading Bug and the numeric value in the Selected Heading field.
After 10 seconds of inaction, the knob reverts to its Home state (HDG), and the Heading Bug and Selected Heading field value are shown in cyan (inactive). 28

29. Left Knob Left Knob CRS: Course IAS: Airspeed Reference Bug
Inactive by Default
Home position is Course: (CRS)
Pushing knob changes color of action from cyan to magenta-numerical value changes, as well
If CDI is set by GPS inputs, the course cannot be controlled by the pilot

30. Sync Function Right Knob Press knob with the indication of:
Left Knob
Press knob with the indication of:
IAS: Bug current airspeed
CRS: VOR mode-Center CDI with TO; ILS mode- Current course
Right Knob
ALT: Sync to current altitude
BARO: Sync barometric setting to in
HDG: Sync heading to current heading 30

31. Buttons Three buttons at the bottom of the Display Unit
Center Button: CDI Source Select, which navigational source will couple to the CDI (Green letters indicate the source)
GPS-Garmin will control the source and course
VLOC-VOR or Localizer
If navigational source unavailable-a red slash through the letters and CDI bar not shown
Left Button: Single-Line Bearing Pointer Source Select- cycle through the available navigational sources
Right Button: Double-Line Bearing Pointer Source Select- cycle through the available navigational sources

32. Navigation Source Select
Three buttons at the bottom of the Display Unit
Center Button: CDI Source Select, which navigational source will couple to the CDI (Green letters indicate the source)
GPS-Garmin will control the source and course
VLOC-VOR or Localizer
If navigational source unavailable-a red slash through the letters and CDI bar not shown

33. Bearing Pointer Source
Left Button:
Single-Line Bearing Pointer Source Select- cycle through the available navigational sources
Right Button:
Double-Line Bearing Pointer Source Select- cycle through the available navigational sources

34. Hot Keys Single action buttons for frequently used commands
½: Not Applicable without Hazard Awareness
MIN: Approach minimums display and change with right knob
360: ARC/360 compass select (Supplemental bearing pointer not visible with ARC
MAP: Display GPS map; de- clutter press key and level is displayed in lower left of navigation display
GPSS: Not Applicable without Auto Pilot

35. Menu Button
Pressing MENU Button Activates the Main Menu

36. Menu Button With MENU Active:
Left knob controls screen display brightness, AUTO is default, push knob and twist to change, push again back to AUTO brightness

37. Display Lighting
Pressing the MENU Button and the Main Menu is active, the Left Knob can be used to adjust the EFD1000 display brightness.
By default, the LCD brightness operates in AUTO mode, and is adjusted based on photocell sensing of ambient lighting conditions. When the MENU is active and the LCD is in AUTO, the word AUTO and a brightness level of will be displayed in green above the Left Knob.
To override the AUTO brightness setting, press the Left Knob once to switch into Manual mode, and then rotate the Left Knob to set the brightness to the desired level. To return to AUTO brightness control, press the Left Knob again.
Display Lighting
When the MENU Button is pressed and the Main Menu is active, the Left Knob can be used to adjust the EFD1000 display brightness.
By default, the LCD brightness operates in AUTO mode, and is adjusted based on photocell sensing of ambient lighting conditions. When the MENU is active and the LCD is in AUTO, the word AUTO and a brightness level of will be displayed in green above the Left Knob.
To override the AUTO brightness setting, press the Left Knob once to switch into Manual mode, and then rotate the Left Knob to set the brightness to the desired level. To return to AUTO brightness control, press the Left Knob again. 37

38. Edit Main Menu Edit Main Menu Items 1. Access the Main Menu.
2. Navigate to the desired menu page.
3. Push the Menu Key of the desired option. The menu label turns magenta, and the EDIT VALUE label displays above the Right Knob.
4. Rotate the Right Knob to the desired value.
5. Push the Right Knob to return to menu navigation mode.
6. Push the MENU Button to exit the Main Menu.

39. Main Menu
Each menu page displays up to five selectable options, each adjacent to one of the five Hot Keys. After navigating to the menu page, press the Menu Key adjacent to that option label, which initiates the menu’s Edit mode.
When the Menu is in Edit mode, the label EDIT VALUE displays above the Right Knob in magenta and the label of the item selected for editing is also shown in magenta. Rotate the Right Knob to change the value of the selected item. When done, either select another displayed option to change , or push the Right Knob to exit Edit mode and return to Navigation mode to select another menu page.
When you are finished changing menu options, press the MENU Button again to exit the Main Menu.
Each menu page displays up to five selectable options, each adjacent to one of the five Hot Keys (which double as Menu Keys when the Main Menu is active). 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. When the Menu is in Edit mode, the label EDIT VALUE displays above the Right Knob in magenta and the label of the item selected for editing is also shown in magenta. Rotate the Right Knob to change the value of the selected item. When done, either select another displayed option to change , or push the Right Knob to exit Edit mode and return to Navigation mode to select another menu page.
When you are finished changing menu options, press the MENU Button again to exit the Main Menu. 39

40. Menu Menu Menu Page number and mode (Navigation mode shown)
Menu Page Name
Menu Page graphical bar
Brightness Control

41. Main Menu With MENU Active:
Left knob controls screen display brightness, AUTO is default, push knob and twist to change, push again back to AUTO brightness
Page 1 of 11- General Settings
TPS: Tapes enable
VSPEED:
Auto CRS:
ARC MODE:
AHRS: Reset

42. Menu Button Page 2 of 11-General Setting B BARO: In/Mb OAT: C/F
Clear Strikes:
Strikes Test:
Auto Ring: Enable

43. Menu Button Page 3 of 11-360 Map Setting 360 FLT PLAN: On/Off
360 APTS: On/Off
360 NDB: On/Off
360 VOR: On/Off
360 INTRS: On/Off

44. Menu Button Page 4 of 11-ARC Map Setting 360 FLT PLAN: On/Off
360 APTS: On/Off
360 NDB: On/Off
360 VOR: On/Off
360 INTRS: On/Off

45. Menu Buttons Page 5 of 11-Vspeeds A Va: Value Vbg: Value Vref: Value
Vr: Value
Vx: Value

46. Menu Buttons Page 6 of 11-Vspeeds A Vy: Value Vlo: Value Vle: Value
If grayed out, the values were locked out during installation and cannot be changed by the pilot 46

47. Menu Buttons
Page 10 of 11-Power Settings (Emergency Section discussion)
Battery:
EXT Power:
Restart:
BAT:

48. Menu Buttons Page 11 of 11-System Version
MAP VER:
IOP VER:
S/N:
Green indicator is status only

49. Range Key RNG Allows to zoom in/out on navigation display
Value is indicated lower left of screen; adjustable to 2-200nm
Hold down RNG key for Auto zoom which will keep next WAP at the out ring of the compass

50. Shutdown Procedure Shutdown EFD1000 PFD (with internal battery)
1. Either pull or turn off the EFD Circuit Breaker Switch/Circuit Breaker (as configured).
2. Push and hold the REV Button until the display turns off.

51. Shutdown Procedure Shutdown EFD1000 PFD (with internal battery)
1. Press the MENU Button. The Menu displays.
2. Rotate the Right Knob to the POWER SETTINGS menu page.
3. Press the RESTART Menu Key. The power down sequence initiates, and a power down message displays.
A powering off annunciation displays indicating that the unit will shut down in 5 seconds. The pilot can press any control to abort the power- down sequence.

52. Shutdown Procedure Shutdown EFD1000 PFD (with internal battery)
Power On Manually
Press the REV Button until the EFD1000 PFD powers on.

53. Unusual Pitch Attitude Indications
Pitch Ladder
2.5  increments
Unusual pitch attitude will show Red Chevrons on the pitch Ladder for direction to go
Chevrons enabled with 15 pitch up and 10 pitch down

54. Roll Scale Attitude Indications
10, 20, 30, 45 and 60
Brick replaces ball on inclinometer

55. Airspeed Tape and Bug Airspeed Tape Indicator Rolling drum readout
Colored bands, Green, Yellow, and Red
Red for Vso and Vne
Vspeeds on tape
Airspeed Bug
The pilot can set a target airspeed using the Left Knob. The target airspeed is shown on the Airspeed Tape in the form of an Airspeed Bug and will also be displayed numerically above the Airspeed Tape . The bug and numerical value are for visual reference only, to help the pilot maintain a target airspeed; there is no alerting for deviations from the target. 55

56. Airspeed Tape Selected to Edit and New Speed
A target airspeed using the Left Knob can be set. The target airspeed is shown on the Airspeed Tape in the form of an Airspeed Bug and will also be displayed numerically above the Airspeed Tape . The bug and numerical value are for visual reference only, to help the pilot maintain a target airspeed; there is no alerting for deviations from the target.
The pilot can set a target airspeed using the Left Knob. The target airspeed is shown on the Airspeed Tape in the form of an Airspeed Bug and will also be displayed numerically above the Airspeed Tape . The bug and numerical value are for visual reference only, to help the pilot maintain a target airspeed; there is no alerting for deviations from the target. 56

57. Altitude Tape and Alerter
Altimeter
Current altitude in 20 foot increments
Pitch trend for the next 6 seconds
Altitude Alerter
Yellow flag when in 15 seconds or 200 feet away from a pre- selected altitude

58. Instrument Approach Indications
Lateral Display
Displays when GPS is the active source and GPS is in Approach mode
GPS1 (2)
LOC 1 (2)
BC1 (2)
VOR1 (2)
ILS1 (2)

59. Instrument Approach Indicators
Navigation Source ins Visible to the left of the LDI
Lateral Deviation Indicator (LDI)
ILS, LOC, LOC (BC), or GPS in Approach Mode
Instrument Approach Indicators
When flying certain types of instrument approaches. These enable the pilot to maintain a tighter instrument scan on the ADI, reducing workload and improving safety.
A Lateral Deviation Indicator (LDI) is presented on the attitude indicator whenever the pilot has coupled an ILS, LOC, LOC(BC), or a GPS in Approach Mode to the HSI, and valid lateral guidance is being provided. The navigation source coupled to the LDI is annunciated to the left of the LDI. A Vertical Deviation Indicator (VDI) is presented on the attitude indicator whenever the LDI is shown
Whenever the lateral or vertical deviation exceeds the maximum displayable range of 2.5 dots, the deviation diamond is rendered as a hollow, ghosted image pegged to the corresponding side. As soon as the deviation comes into range, the diamond turns solid green, making it easy to identify when the needle is alive.
Additionally, the pilot can pre-set the minimums (MIN) for the approach, which will be displayed on the ADI until the pilot toggles off the display using the MIN Hot Key. Once the MIN data field value is set to a Decision Altitude or Minimum Descent Altitude, the EFD1000 Pro PFD provides a visual annunciation when the aircraft reaches or descends below this altitude. Additionally there is a minimums bug presented on the altitude tape. The bug includes three components – a green marker 500 ft. above programmed minimums, a hollow yellow triangle in the area from 100 ft to 200 ft. above minimums, and a red and yellow marker at the programmed minimums value. 59

60. Instrument Approach Indicators
Vertical Deviation Indicator (VDI) in ILS or GPS WAAS
Instrument Approach Indicators (unavailable on Pilot PFD)
Additional indicators are shown or available on the Attitude Display when flying certain types of instrument approaches. These enable the pilot to maintain a tighter instrument scan on the ADI, reducing workload and improving safety.
A Lateral Deviation Indicator (LDI) is presented on the attitude indicator whenever the pilot has coupled an ILS, LOC, LOC(BC), or a GPS in Approach Mode to the HSI, and valid lateral guidance is being provided. The navigation source coupled to the LDI is annunciated to the left of the LDI. A Vertical Deviation Indicator (VDI) is presented on the attitude indicator whenever the LDI is shown and valid 36 guidance is provided, such as from an ILS or WAAS GPS.
Whenever the lateral or vertical deviation exceeds the maximum displayable range of 2.5 dots, the deviation diamond is rendered as a hollow, ghosted image pegged to the corresponding side. As soon as the deviation comes into range, the diamond turns solid green, making it easy to identify when the needle is alive.
Additionally, the pilot can pre-set the minimums (MIN) for the approach, which will be displayed on the ADI until the pilot toggles off the display using the MIN Hot Key. Once the MIN data field value is set to a Decision Altitude or Minimum Descent Altitude, the EFD1000 Pro PFD provides a visual annunciation when the aircraft reaches or descends below this altitude. Additionally there is a minimums bug presented on the altitude tape. The bug includes three components – a green marker 500 ft. above programmed minimums, a hollow yellow triangle in the area from 100 ft to 200 ft. above minimums, and a red and yellow marker at the programmed minimums value.
If a Radar Altimeter is installed in the aircraft and connected to the EFD1000, a Decision Height annunciation will be displayed when the aircraft descends to, or below, the selected radar altitude. 60

61. Instrument Approach Indications
Vertical Display- Deviation Display
Displays when flying WAAS approach with vertical guidance (LPV, LNAV/VNAV, LNAV+V) (Green diamond ghosted if out of range)

62. Approach Minimums Indicators
Minimum Green Triangle:
The aircraft is 500 feet above selected MINIMUM.
Hollow Yellow :The aircraft is between 200 and 100 feet above the selected MINIMUM. The marker base is at 100 feet above MINIMUM, and the tip is at 200 feet above MINIMUM.
Yellow Triangle and Red Striped: The aircraft is at the selected MINIMUM Approach MINS
Green bug at 500 feet above minimums
Yellow bug at 100 feet above minimums
Yellow-Orange striped at minimums

63. Data Bar Center of display True Airspeed GPS Ground Speed
Outside Air Temperature
Wind Velocity-is relative to the current direction of flight
Altimeter setting

64. Navigation Heading Display
Compass has input from Flux Detector and requires no pilot action
Heading bug in ARC/360
ARC Display Mode
Compass Display Mode

65. Vertical Speed Indicator (VSI)
Vertical Speed Tape is on the right side of the heading/compass
0.5=500 f/m, 1=1000 f/m 2=2000 f/m; exceeding 2000 f/m will indicate with white arrow and value
In ARC mode only the value ID displayed

66. Direction Indicator (Magnetic Compass)
The compass always shows the current magnetic heading of the aircraft, both with a numerical value of the current heading at the top of the display, and with a lubber line, or pointer, to that heading on either a full or partial compass rose.
Direction Indicator (Magnetic Compass)
The center of the Navigation Display is the Direction Indicator, or Magnetic Compass. The compass always shows the current magnetic heading of the aircraft, both with a numerical value of the current heading at the top of the display, and with a lubber line, or pointer, to that heading on either a full or partial compass rose. This slaved compass system compensates both for the turning and acceleration errors exhibited by wet compasses and for precession errors found in common Directional Gyros, so the pilot does not need to make adjustments to the heading indicator during the flight.
The Direction Indicators of both the Pilot and Pro PFDs share many common features, explained below, while the Pro PFD adds features for instrument navigation. The Pilot PFD Direction Indicator is a slaved Directional Gyro (DG) with Heading Bug. The Pro PFD Direction Indicator adds capabilities to make it an electronic Horizontal Situation Indicator (HSI) with dual Bearing Pointers. The HSI features are explained in a separate section below. 66

67. Direction Indicator (Magnetic Compass)
Compass Modes: 360º vs. ARC
The Direction Indicator on the EFD1000 can be presented in either a full 360º compass rose mode, or in a 100º ARC format.
In 360 Mode, the compass resembles the mechanical instrument, with the own ship position in the center of the display.
ARC Mode provides an extended forward view with the own ship position at the bottom of the display. The ARC mode is especially good for map displays.
The middle Hot Key is used to toggle the display between 360 and ARC modes, with the current mode shown in green adjacent to the Hot Key.
Compass Modes: 360º vs. ARC
The Direction Indicator on the EFD1000 can be presented in either a full 360º compass rose mode, or in a 100º ARC format. In 360 Mode, the compass resembles the mechanical instrument, with the own ship position in the center of the display. ARC Mode provides an extended forward view with the own ship position at the bottom of the display. The ARC mode is especially good for map displays. The middle Hot Key is used to toggle the display between 360 and ARC modes, with the current mode shown in green adjacent to the Hot Key. 67

68. Navigation Heading Display
Rate of Turn Indicator
Top of Compass/Heading
1st Tick mark = Half-Standard Rate
2nd Tick mark = Standard Rate
If greater than 6 per second will show an arrow at the end of tape

69. Navigation Heading Display
Navigation Source selected with center button
Information about the source is in the top left area of display
GPS will show
Source
WAP
Desired Track/Distance
Time to WAP
Ground Based Source will show
Source e.g. LOC2 (BC)
Frequency
Course

70. Deviation Off Scale Indication
Current Course
To the right of the navigation source indication on top of navigation display
TO/FROM is triangle on the CDI needle
CDI Needle is 2.5 dots wide and hollow indication if current navigation source is unavailable
If source is completely out of range CDI and TO/FROM indications are removed

71. Navigation Heading Display
GPS Auto Course (With Garmin 430)
Automatically sets HSI needle to current course (multiple legs in GPS flight plan)
When active “A” in box is displayed left of course readout
At this point left knob can only change IAS
Menu Page: 1 of 11 (Auto CRS: enable on/off)
GPS sensitivity in compass mode: TERM or APR

72. Auto Course Select GPS Auto Course (With Garmin 430)
Automatically sets HSI needle to current course (multiple legs in GPS flight plan)
When active “A” in box is displayed left of course readout
At this point left knob can only change IAS
Menu Page: 1 of 11 (Auto CRS: enable on/off)
GPS sensitivity in compass mode: TERM or APR

73. Navigation Heading Display
Map Overlay
Magnetic Heading always up and centered
Active leg in Magenta and subsequent legs in White
Use range key to zoom in/out nm
Use MAP Key to show the level of detail of the map
Bearing Pointers-use for situational awareness during approaches
Photos on following slides

74. Bearing Pointers
Bearing Pointers-use for situational awareness during approaches

75. Situational Awareness Map
Map Hot Key used to cycle and de-clutter the map
Range Button to zoom in or out on the map
Situational Awareness Map
When the EFD1000 is connected to a compatible GPS navigator, a base map can be displayed underneath the Direction Indicator in either 360º or ARC modes. Most GPSs put out data to enable the EFD1000 to display the GPS flight plan legs and waypoints. The active GPS flight plan leg, waypoint, and its identifier are shown in magenta. Other waypoints and legs are shown in white.
Some GPS navigators (typically those using the ARINC 429 data protocol, such as the Garmin 400/500 series) additionally put out information on nearby waypoints (e.g., airports, VORs, NDBs, and intersections), which are also displayed on the EFD1000 base map. Often these GPSs also display curved flight paths, such as course reversals and holding patterns.
The base map is always oriented with magnetic heading up and centered so that the current aircraft position coincides with the aircraft own ship symbol. These base map elements underlay all other instruments and annunciations in the Navigation Display.
The MAP Hot Key is used to cycle through four levels of map de-clutter and to turn off the base map display. Each successive press of the MAP Hot Key selects the next de- clutter level or OFF.
The map display range is controlled by the Range button, enabling the pilot to zoom in or out on the map. Automatic de-clutter logic changes the map features displayed depending on the selected map range.
The current map settings (range and feature level) are shown in the lower left-hand corner of the navigation display whenever the map is not OFF. The current map range is displayed in nautical miles, measuring the distance from the own ship symbol to the edge of the map display. The current map feature level is indicated by one to four green trapezoids underneath the range value (one mark is Low, while four marks indicates the highest map feature level). 75

76. Remember
Color Coding
Magenta-modify or edit current function with button or knob
Cyan-deactivated state, change display option or view (Ready to change)
Knobs deactivated by default to prevent erroneous input

77. Flying the PFD Selected Altitude: Check and Set Map Range Buttons: Set
Bearing Pointers Navigational Source: Check and Set
Barometric Pressure Setting: Check and set
CDI Navigation Source: Select
Heading Bug: Set
Course Pointer Value: Set
Compass Hot Key: 360° or ARC Set
MINIMUMS Setting: Set approach minimums
Map Settings Hot Key: Set
Selected Airspeed: Set

78. Pre-Departure Pre-Departure (Startup)
Once the pre-flight inspections and checklists are complete, start the engines. After engine starts, turn on the EFIS Master switch or PFD power switch.
The bezel backlighting illuminates and within a few seconds the EFD1000 PFD splash screen displays while the EFD1000 PFD initializes and AHRS data is validated.
Software initializes, the Attitude and Navigation Displays will appear first (typically within seconds), with red X’s showing for the airspeed and altitude tapes and the CDI source slashed as invalid.
The air data sensors will warm up to operating temperature, and the airspeed and altitude tapes will appear. At that point, when all red X’s are gone, the EFD1000 is ready to go.
Pre-Departure (Startup)
Once the pre-flight inspections and checklists are complete, start the engines. After engine starts, turn on the EFIS Master switch (if installed).
When power is applied to the EFD1000, the bezel backlighting illuminates and within a few seconds the EFD1000 PFD splash screen displays while the EFD1000 PFD initializes and AHRS data is validated .
As the software initializes and the PFD warms up, the Attitude and Navigation Displays will appear first (typically within seconds), with red X’s showing for the airspeed and altitude tapes and the CDI source slashed as invalid. In a short while (from a few more seconds to a few minutes, depending on how cold the aircraft is), the air data sensors will warm up to operating temperature, and the airspeed and altitude tapes will appear. At that point, when all red X’s are gone, the EFD1000 is ready to go. 78

79. Pre-Departure
The display of deviations on the LDI and VDI are not necessary to verify the communication between the Garmin 430 and EFD1000 system.
With the radios in service, we pick up the ATIS and learn the local altimeter setting and the runway in use for departures.
Set the standby altimeter to the barometric setting and then set the EFD1000 PFD barometric setting. 79

80. Pre-Departure
Turn the Avionics Master ON. Until the navigation radios are operational, the navigational source annunciations on the EFD1000 will be shown with a red line slashed through them, and the GPS1, GPS2 caution annunciations on the left and INTEG caution annunciated on the right edge of the display. The CDI Source Select will default to VLOC1 the first time the PFD is turned on, after that the CDI Source Select will display the last used CDI Source. Once the navigational radios have warmed up, the red slash will be removed from the CDI Source annunciation. 80

81. Barometric Pressure Set the Barometric Pressure
Press the Right Knob three times until BARO is displayed.
Now you can use the Right Knob to set the Barometric Pressure.
After 10 seconds the field will once again show HDG.

82. Heading Bug
For example, 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 in magenta. The color of the Heading Bug will be in magenta with a dashed magenta line extending from the own ship symbol to the Heading.
Rotate the Right Knob to the value required for the Heading Bug. After 10 seconds the HDG will change to cyan color.
For example, 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. The Heading Bug will also be rendered in magenta, and a dashed magenta line will extend from the own ship symbol to the Heading Bug to make it easier to see the bug position.
Rotate the Right Knob to change the value of the Heading field. Rotate clockwise to increase, or counterclockwise to decrease, the value. Once the correct heading is selected and after 10 seconds of inaction, the field is disabled, and the label and field are rendered in cyan. 82

83. Clearance Delivery
We will call Clearance Delivery to pick up our IFR clearance.
We will copy and read back our clearance, and then set up our avionics for an instrument departure. We will set our transponder code and communication radio frequencies. Then we will enter our flight plan into GPS, load the departure and activate the flight plan. We make sure the CDI button on the 430W is set to GPS. (See Garmin 430 Training Module)
This departure calls for vectors to our route. While we’ll be navigating on GPS, for situational awareness we tune those first two VOR fixes into our navigation radios. For example, we will tune ABQ VOR (113.2) into VLOC1 and ZUN VOR (113.4) into VLOC2.

84. Map De-clutter Select Map De-clutter Level
Push the MAP Hot Key (fourth Hot Key) to cycle through and select the desired level of detail.
Each time the Hot Key is pressed, the Map De- clutter level icon changes to the next option

85. Map Range Change the Map Range
Press the Range Button UP (+) to increase the range, or DOWN (-) to decrease the range, until the desired range is reached.

86. Altitude Alerter Set the Altitude Alerter
Press the Right Knob twice showing the “ALT” above the Right Knob; the color of the altitude numerical field and bug is magenta.
Rotate the Right Knob to change the value of the Altitude field, you have set the altitude alerter. After 10 seconds the field will once again show HDG in cyan.

87. Airspeed Bug Set the Airspeed Bug
For example, our normal climb speed is 90 KIAS, set the airspeed bug as a reminder. Press the Left Knob twice, until it shows IAS in magenta above the knob. Turn the knob until 90 shows in the Selected Airspeed Field.
Rotate the Left Knob to change the value of the Selected Airspeed field. Once the correct value is selected, and after 10 seconds of inaction, the field is disabled, and the color of the label and field is in cyan. 87

88. Airspeed Bug Set the Airspeed Bug (cont'd)
With our avionics set, we taxi out to the runway, do our run-up, and call tower, ready for departure.
As we taxi into position and hold on Runway 8, we verify that our EFD1000 compass shows 080º, lined up with our pre-set heading bug. As tower clears us for takeoff, it tells us to wait until reaching the end of the runway, and then to turn left to heading 250º. We press the Right Knob once to activate HDG, and turn the knob left to set the Heading Bug to 250. 88

89. Departure
Departure
As we start the takeoff roll, we note the airspeed on the EFD1000 comes alive at 20 KIAS. All indications are normal, so we continue the takeoff, rotate at 55 KIAS and command bars at 7º pitch up with wings level.
Around this time, on our 250º vector, we pass abeam VOR, (BRG#1 points to our 9 o’clock position and begins to swing behind us).
Departure now tells us to fly heading 220º to join the departure, and climb and maintain 10,000. Departure also calls out slower traffic at our 10 o’clock, seven miles, west-bound at 8,000, and asks us to expedite our climb through 8,000.
Press the Right Knob once to activate HDG, and turn it left to set the Heading Bug to 220º.
Press the Right Knob again to activate ALT, and turn it right to set 10,000 in the Selected Altitude field at the top of the airspeed tape. 89

90. Enroute
Auto Course Select has already set our Course Pointer to the departure, and a 220º heading sets us up for a nice intercept.
At about 9,700 feet, the Altitude Alerter tone sounds, and the yellow alert flag by the Selected Altitude illuminates, telling us we are 15 seconds from reaching our assigned 10,000 feet. We begin our level-off, and upon reaching 10,000 feet.
Departure calls again to hand us off to Center on
As we level out, accelerate to cruise speed, and then power back. 90

91. Enroute
Now that we’re established at our final cruise altitude and in the enroute phase of our flight, we’ll switch to the ARC mode of the HSI to maximize a forward view.
1. Press the 360 Hot Key and observe the HSI changes to its ARC view, and the legend adjacent to the Hot Key changes to ARC in GREEN.
2. Adjust the map range to suit your preference.
360 Display Mode

92. Enroute Select a Compass Mode
Push the 360/ARC Hot Key (third Hot Key) to alternately select either the 360° or the ARC compass display.
We set cruise power and lean the mixture. As the airplane stabilizes in cruise, we check the Data Bar to monitor performance. True Airspeed (TAS) is close to book performance for this altitude and power setting. OAT is close to ISA.
ARC Display Mode

93. Arrival and Approach to Landing
Nearing Mustang VOR (FMG), Oakland Center hands us off to Reno Approach, and we request navigation for the ILS16R. Approach gives us the new altimeter setting of 30.08, clears us down to 9,000 feet, and after FMG direct TAKLE. We initiate the descent, set in the standby altimeter, and set the EFD1000:.
Fifteen seconds before reaching 9,000 feet, the Altitude Alerter flag illuminates. 93

94. Arrival and Approach to Landing
Approaching FMG, the GPS turn anticipation sequences to TAKLE, our Course Pointer swings automatically from 302º to 316º, and GPSS steers us through the turn, rolling out precisely on course.
We power back and select the first notch of flaps to slow down. Reno Approach calls, reports us six miles from TAKLE, and clears us for the ILS16R approach, pilot nav.
We activate the approach on the GPS and ensure the ILS frequency is in the active window of the Garmin 430.
We turn outbound on a 344º course for the procedure turn.
We see the procedure turn drawn on the base map ahead of us. 94

95. Arrival and Approach to Landing
Final approach course of 164º, we begin a descent down to 8,500 feet, which we will maintain until glideslope intercept.
We are still navigating along the ILS16R approach using GPS.
Along this intermediate segment of the approach, verify the 430W is changed from GPS to VLOC output on its CDI.
Watch for the EFD1000 CDI Source Select field to change from GPS1 to VLOC1.
This automatic switch from GPS to VLOC should occur 2–10 NM outside the Final Approach Fix (FAF). If it has not occurred automatically by 2 NM outside the FAF, manually press the CDI button on the 430W to make the switch to the ILS frequency. 95

96. Arrival and Approach to Landing
As the PFD navigation source switches to the ILS on VLOC1, the LDI and VDI will appear on the Attitude Display.
The LDI Navigation Source Indication will show ILS, if it is receiving a valid glide slope signal, or LOC, if it is not receiving the glide slope (GS).
The CDI Source Information Block will also show ILS or LOC. 96

97. Arrival and Approach to Landing
Even though the PFD Navigation Source for the CDI has switched to VLOC1 and the ILS, and the CDI, LDI and VDI are showing deviation relative to the localizer and glideslope. We are not yet flying the ILS, required for this approach.
A couple of miles outside the FAF (TAKLE), we begin tracking the localizer and ready for glideslope capture. With that setup, if we have to fly the Missed Approach, climbing straight ahead to 6,700 feet. 97

98. Arrival and Approach to Landing
When the GS is full-scale deflection above us, the GS indicator on the VDI will show as a hollow diamond at the top of the scale.
When the GS comes alive, the indicator will change to a solid green diamond and begin to move down the scale. On GS intercept, we verify and track down the glide slope. 98

99. Arrival and Approach to Landing
We continue monitoring the approach with verifying localizer and glide slope. As we get close to minimums, a green triangle appears on the altimeter tape at 500 feet above minimums; a hollow yellow Minimums Triangle appears with its tip at 200 feet above minimums and its base at 100 feet above. A red striped triangle appears at the MINIMUMS setting. These three colored markers on the altimeter tape give us visual cues that we are approaching minimums.
On reaching our pre-set minimums (5,520 feet):
The MINIMUMS alert displays below the Aircraft Reference Symbol on the ADI.
Tracking the glide slope down to a smooth landing. 99

100. IFR Procedures Full ILS Approach (Example)
Navigate to IAP (Via VOR, GPS, etc) using CDI navigation source
Set bearing pointer to next WAP
Set altitude alerter to current assigned altitude
Load Garmin 430 with Procedure
Initiate procedure turn, as appropriate
Turn on Flight Plan Overlay (de-clutter for detail)

101. IFR Procedures CDI VLOV to GPS, as appropriate Review weather
Procedure turn outbound and inbound
Localizer Alive
Descent-Use Pink trend Bar for smooth 500 f/m
Set MIN for approach “MIN HOT Key”
Vertical Guidance-solid green triangle
Alert to MIN altitude

102. IFR Procedures Minimums
500 feet above Green Triangle
100 feet above Yellow Triangle
Minimums Yellow-Orange Striped Triangle
Note: Equipped with Garmin 430w, use the GPS for primary navigation until localizer intercept.

103. Emergency and Abnormal Procedures
Loss of External (to the Aspen) Power
Internal standby battery provides at least 30 minutes of backup power
Auto switch at these values:
25.6 volts on 28 volt system
12.8 volts on 14 volt system
Red indicator on Attitude Display
Can override automatic switch from external to internal battery using the top two Hot Keys
Active source in Green
Voltage must remain below cutoff for two minutes before transferring to standby battery (e.g. taxi-landing roll out)
If system voltage immediately goes to zero the system will transfer to standby under all conditions

104. Emergency and Abnormal Procedures
Pitot Static System Failure
Blockage (Ice or water)
If IAS drops below 30 knots and GPS GS is greater than 50 knots, and BIG RED X will appear on attitude indicator
“ATTITUDE FAIL” -“CHECK PITOT HEAT”
Turn on Pitot Heat
Open Alternate Air Source
After IAP is >30 knots – system returns to normal

105. Pitot-Static System Failure

106. Emergency and Abnormal Procedures
Heading Indication Failure
RED X
With “DIRECTION INDICATOR FAIL”
Cross Check Attitude (Degradation)
If becomes invalid will RED X and “ATTITUDE FAIL”
Requires a system RESET (Menu 1 of 11)-no excessive rates of turn will resetting

107. Cross Check Attitude

108. Emergency and Abnormal Procedures
GPS Malfunctions
Flight plans are stored in ASPEN
Aspen continuously stores location of GPS flight plan waypoints and nearest airports in its internal memory
If GPS fails- the built-in ASPEN emergency GPS will kick-in: “RSM GPS REVERSION”-”EMER USE ONLY”
Displayed at bottom of compass/heading indicator

109. Conclusion on the ASPEN PFD
When navigating with the buttons/knobs/hot keys remember to use the self-explanations of the associated keys
If you twist, turn, press something you need to expect, anticipate, and see a given reaction some place on the panel
The buttons are inactive until PRESSED
Generally pressing a button will go to the source and pressing again will go back

110. Take a Break… The following slides will have a few Questions helping you determine your Aspen Learning Knowledge

111. Review - Questions?

112. Questions on the ASPEN PFD
1. What does the “A” in the Aspen snapshot indicate on the Aspen PFD below?
Answer:
GPS Auto Course (With Garmin 430), automatically sets HSI needle to current course (multiple legs in GPS flight plan)
When active “A” in box is displayed left of course readout (Auto Coursing)
At this point left knob can only change IAS
(Reference Slide 73)
112

113. Questions on the ASPEN PFD
2. What does this caution ICON message tell the pilot during Aspen Initialization or during flight?
Answer:
The display of deviations on the LDI and VDI are not necessary to verify the communication between the Garmin 430 and EFD1000 system.
Turn the Avionics Master ON. Until the navigation radios are operational, the navigational source annunciations on the EFD1000 will be shown with a red line slashed through them, and the GPS1, GPS2 caution annunciations on the left and INTEG caution annunciated on the right edge of the display.
(Reference Slide 80)
113

114. Questions on the ASPEN PFD
3. What is the wind direction and velocity on the Aspen screen shot below?
Answer:
Direction 148 degrees and 16 knots relative to the direction of flight
(Reference Slide 64)
114

115. Questions on the ASPEN PFD
4. If the coupled Garmin GPS 430 is suddenly out of service after initialization and 30 minutes of flight, will the pilot have any flight plan guidance on the Aspen PFD? Why or Why not?
Answer:
Yes. The Emergency Back-up/Standby function within Aspen GPS will have a copy of the initial flight plan in its system for guidance, provided the Aspen and the Garmin authenicated together.
Additionally, if we have a total electrical failure, the Aspen Standby battery will provide power for a minimum of 30 minutes of use for the PFD.
(Reference Slide 22)
115

116. Questions on the ASPEN PFD
5. What does the hollowed Course Deviation Bar indicate to the pilot on the HSI snapshot below?
Answer:
CDI Needle is 2.5 dots wide and hollowed indication of the bar states that the current navigation source is unavailable.
If the navigation source is completely out of range CDI and TO/FROM indications are removed.
(Reference Slide 71)
116

117. End of Aspen TAA Transition Course