Aspen Primary Flight Display - Langley Flying School

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7.3.4. Operational Specifications CHAPTER 7 APPENDICES Airspeed Range Minimum displayed airspeed 20 KIAS Maximum displayed airspeed 999 KIAS Altitude Range Minimum displayed altitude -1,500 ft. MSL Vertical Speed Range Maximum displayed altitude Maximum displayed vertical speed rates (tape) Maximum displayed vertical speed rates (numerical value) 60,000 ft. MSL +/-2,000 fpm +/- 9,990 fpm Turn Rate Maximum displayed turn rate 6.0 °/second Barometric Pressure Correction Range 28.10 to 30.99 In Hg (946 to 1049 mB) Internal Battery Minimum operating time while on internal battery 30 minutes 1 Table 7-4 Operational Specifications 1. At extreme cold temperatures the internal current limiting protections of the internal battery may cause the battery to shut off and not power the display. Page 7-6 EFD1000 PFD Pilot’s Guide 091-00005-001 REV B
7.4. Glossary ºC Degrees Celsius ºF Degrees Fahrenheit Accuracy Estimated position accuracy in feet or meters A/D Analog to Digital AC Alternating Current ACU Analog Converter Unit ADC Air Data Computer ADI Attitude Director Indicator ADIZ Air Defense Identification Zone AFMS Airplane <strong>Flight</strong> Manual Supplement AGL Above Ground Level AHRS Attitude Heading Reference System AI Attitude Indicator AIM Airman’s Information Manual AIRMET Airman’s Meteorological Information Altitude Elevation above sea level APPR Approach APT airport ARC Partial heading arc format (100°) ARINC Aeronautical Radio, Inc. ATC Air Traffic Control ATIS AWOS Back Course Battery Time BC Bearing BP Calibrated Airspeed CDI CFR CM COM Course Course to Steer Automatic Terminal Information Service Automated Weather Observing System Localizer back course approach where the signal on the back side of the localizer is used for alignment to the runway opposite of normal localizer alignment. Without compensation, the CDI would reverse sense. The time remaining on the battery before it is fully discharged. Back Course The compass direction from the current position to the destination. Bearing Pointer Indicated airspeed corrected for installation and instrument errors. Course Deviation Indicator Code of Federal Regulations Configuration Module communication radio The route taken from the starting position to destination. The recommended direction to steer in order to reduce cross-track error and return to the course line. CHAPTER 7 APPENDICES 091-00005-001 REV B EFD1000 PFD Pilot’s Guide Page 7-7
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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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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: 7.3.2. Remote Sensor Module (RSM) W
Page 237 and 238: Fuel Timer Glide Ratio, G/R GPS GPS
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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Aspen Primary Flight Display - Langley Flying School

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