Aspen Primary Flight Display - Langley Flying School

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CHAPTER 7 APPENDICES Cross Track Crosstrack Error CRS CTS dBZ DC Decision Height Declutter Deg Desired Track DH Distance (Next) DME DTK The perpendicular distance, left or right, away from the selected course. The distance the aircraft is off the desired course. Course Course to Steer decibels ‘Z’ (radar return) Direct Current A specified height or altitude in the precision approach at which a missed approach must be initiated if the required visual reference to continue the approach has not been acquired. This allows the pilot sufficient time to safely reconfigure the aircraft to climb and execute the missed approach procedures while avoiding terrain and obstacles. Reduce amount of objects displayed on screen. Degree The desired course between the active “from” and “to” waypoints. Decision Height The great circle distance from current location to a Go To destination or the final waypoint in a route. Distance Measuring Equipment Desired Track EFD EFIS Elevation Enroute Safe Altitude ETA (Destination) ETA (Next) ETE (Destination) ETE (Next) FAA FAF FD Flight Timer Fpm Ft Evolution Flight Display Electronic Flight Instrument System The height above mean sea level. The recommended minimum altitude within ten miles left or right of the desired course on an active flight plan. Estimated Time of Arrival. The estimated time you will reach a Go To destination or the final waypoint in a route. Estimated Time of Arrival. The estimated time you will reach a Go To destination or the next waypoint in a route. Estimated Time En route. The estimated time required to reach a Go To destination or the final waypoint in a route Estimated Time En route. The estimated time required to reach a Go To destination or the next waypoint in a route. Federal Aviation Administration Final Approach Fix Flight Director The length of time for the current flight. Feet Per Minute Feet Page 7-8 EFD1000 PFD Pilot’s Guide 091-00005-001 REV B
Fuel Timer Glide Ratio, G/R GPS GPSS Ground Track Groundspeed GS Heading Hg HSI Hz IAF IAS IAT IFR ILS IMC in Hg The fuel required to travel from current location to the indicated route waypoint. The estimated distance an aircraft will move forward for any given amount of lost altitude. Global Positioning System GPS Steering see Track The velocity that the aircraft is travelling relative to a ground position. Glide Slope or Ground Speed The direction an aircraft is pointed, based upon indications from a magnetic compass or a properly set directional gyro. Mercury Horizontal Situation Indicator Hertz (frequency) Initial Approach Fix Indicated Air Speed Indicated Air Temperature Instrument Fight Rules Instrument Landing System Instrument Meteorological Conditions Inches of Mercury Indicated IOP kHz KIAS km kt LAT LCD LDI Leg LOC MAP METAR MFD MHz Minimum Safe Altitude MOA MSA MSG MSL Information provided by properly calibrated and set instruments on the aircraft panel. Input/Output Processor Kilohertz Knots Indicated Air Speed Kilometer Knots Latitude Liquid Crystal Display Lateral Deviation Indicator The portion of a flight plan between two waypoints. Localizer Main Application Processor Aviation Routine Weather Report Multi-Function Display Megahertz Uses Grid MORAs to determine a safe altitude within ten miles of the aircraft present position. Military Operations Area Minimum Safe Altitude Message Mean Sea Level CHAPTER 7 APPENDICES 091-00005-001 REV B EFD1000 PFD Pilot’s Guide Page 7-9
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091-00005-001 REV B EFD1000 PFD Pil
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A Using new part number 091-00005-0
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Table of Contents Document Revision
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4.2.3.5. Decision Height...........
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Table of Figures Figure 1 EFD1000 P
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Figure 3-24 Selected Airspeed Bug E
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Figure 4-72 Menu, GENERAL SETTINGS,
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Figure 6-4 Battery Status..........
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Chapter 6 Table 6-1 Warning Annunci
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Enable Auto Range .................
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Copyrights and Trademarks Copyright
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LIMITED WARRANTY Aspen Avionics, In
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11. Extension of Warranty. No exten
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XM WX Satellite Radio Service Agree
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Conventions The following conventio
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Color Philosophy Table 2 provides t
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Example Graphics The example graphi
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Chapter 1 Welcome and Introduction
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You can even add another MFD, repla
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1.1.1. EFD1000 Display The EFD1000
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1.1.4. Analog Converter Unit (ACU)
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Chapter 2 Controls and Display The
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DATABAR 38 True Airspeed (TAS) 39 B
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Once set, you can either press the
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Left Knob SYNC Action IAS CRS Set t
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2.2.2. Navigation Source Select But
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2.2.3. Hot Keys The five buttons al
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Hot Key DESCRIPTION OPTIONS LTNG NX
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Each menu page displays up to five
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Edit Main Menu Items 1. Access the
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2.2.5. Range Button When the MAP is
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EFD1000 PFD is their first real exp
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ATTITUDE DISPLAY 16 Attitude Displa
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2.3.2.2. Airspeed Tape and Bug Airs
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2.3.2.4. Instrument Approach Indica
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2.3.4. Navigation Display The lower
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2.3.4.1. Direction Indicator (Magne
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2.3.4.2. Horizontal Situation Indic
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2.3.4.6. Bearing Pointers One or tw
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2.3.4.9. Situational Awareness Map
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Chapter 3 Flying the EFD1000 Pro PF
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3.1. Quick Controls Overview Chapte
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3.2. Example Flight Scenario This s
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Turn the Avionics Master ON. Until
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Next, since we’ll be departing fr
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Select Map Declutter Level • Push
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Because we need all the help we can
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Set the Altitude Alerter 1. Press t
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3.2.2. Departure As we start the ta
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3.2.3. En Route Albuquerque Center
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Check TAS, GS, and winds and temper
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We’re all set up for the approach
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Even though the PFD Navigation Sour
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3.3. Conclusion The EFD1000 Pro PFD
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Chapter 4 Reference Guide The EFD10
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4.1.1. Attitude The Aspen ADAHRS at
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In summary, loss or degradation of
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Two minutes after detection, a FREE
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4.2.1.1. Roll Scale The Roll Scale
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Indicated airspeed is displayed in
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4.2.2.2. Airspeed Display In some c
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4.2.3.1. Barometric Pressure Adjust
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Set Altitude Bug 1. Press the Right
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Once the MIN data field value is se
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4.2.3.6. Altitude Display In some c
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4.3. Data Bar The Data Bar presents
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4.3.5. Barometric Pressure Setting
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All instrument values on the HSI ar
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Select Compass Type • Push the 36
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4.4.3. TO/FROM Indicator Each of th
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4.4.5. CDI Navigation Source When t
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Whenever the CDI navigation source
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4.4.6. Auto Course The pilot can ei
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4.4.8. Bearing Pointer Source Selec
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Select the Single-Line Bearing Poin
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4.4.10. Aircraft Heading Display Th
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4.4.12.1. Map Declutter and Range T
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Auto range is only available when a
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4.5. Lateral and Vertical Deviation
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4.6. Vertical Speed Indicator When
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4.7.1. GPS Steering (GPSS) GPS Stee
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When GPSS is Enabled, and the autop
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Several conditions can cause GPSS t
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NAV Mode Operation - GPS Navigation
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APPR Mode Operation - GPS or GPS/RN
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GPS APPR Mode Operation - WAAS GPS
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Hot Key Display Symbol Annunciation
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NEXRAD coverage displays using the
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The data age (except Puerto Rico NE
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4.8.3.1. Traffic Symbols The EFD100
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When multiple traffic symbols parti
Page 185 and 186: Chapter 5 Customizing the EFD1000 P
Page 187 and 188: KEY DESCRIPTION OPTIONS 360° Fligh
Page 189 and 190: KEY DESCRIPTION OPTIONS KEY DESCRIP
Page 191 and 192: KEY DESCRIPTION 1 US NEXRAD Age OPT
Page 193 and 194: KEY DESCRIPTION OPTIONS Operating f
Page 195 and 196: 5.2. Customizing the Map (Declutter
Page 197 and 198: Feature Group & Layer Order (top to
Page 199 and 200: Vspeed DEFINITION PRE-SET BANDS Vlo
Page 201 and 202: On aircraft with flaps, setting the
Page 203 and 204: 5.4. LCD Brightness Control The LCD
Page 205 and 206: Chapter 6 Expanded Emergency and Ab
Page 207 and 208: Blocked Pitot or Static Line Suspec
Page 209 and 210: On the initial climb-out after take
Page 211 and 212: 6.2. Frequent or Persistent CROSS C
Page 213 and 214: 6.5. Loss of Aircraft Electrical Po
Page 215 and 216: 6.6. GPS Failures and RSM Emergency
Page 217 and 218: 6.8. In-Flight AHRS Reset In the un
Page 219 and 220: 6.9. GPSS Operation, Annunciations,
Page 221 and 222: 6.10. Warning, Caution, and Advisor
Page 223 and 224: CAUTION Figure 6-18 Cross Check Att
Page 225 and 226: CAUTION Figure 6-27 GPSS Source Los
Page 227 and 228: ADVISORY Associated with the GPS co
Page 229 and 230: Chapter 7 Appendices 7.1. Operating
Page 231 and 232: 7.3. Specifications 7.3.1. EFD1000
Page 233 and 234: 7.3.2. Remote Sensor Module (RSM) W
Page 235: 7.4. Glossary ºC Degrees Celsius
Page 239 and 240: 7.5. Index Symbols 1/2, Hot Key ...
Page 241 and 242: GPS Invalid .......................
Page 243 and 244: Operation, Annunciations, and Autop
Page 245 and 246: Vertical Speed Indicator ..........
Page 247 and 248: Weather Data ......................
Page 250: Aspen Avionics, Inc. 5001 Indian Sc
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