Diamond DA20-C1 EclipseDiamond DA20-C1 EclipseDiamond DA20-C1 EclipseDiamond DA20-C1 Eclipse
G500 OverviewG500 OverviewComponentsComponentsPFD (Primary Flight Display)PFD (Primary Flight Display)MFD (Multi Function ...
Digital Components – ADC, AHRS, GPSTIS or TAS: Traffic AwarenessTerrain and Obstacle databaseDual 6.5” LCD screens that ar...
A network of LRUsEach unit is self contained and modular in designEach LRU has a specific function or set of functionsEase...
GDC 74A – Air Data ComputerGRS 77 – Attitude, Heading and Reference SystemGMU 44 – MagnetometerGTX 330 – Mode S Transponde...
Compiles information from the pitot static system and outside airtemperature (OAT) sensor  Communicates with GDU 620 and G...
Basically a solid-state gyro. Uses tilt sensors, accelerometers and ratesensors Contains an IGRF which must be updated eve...
Senses Earth’s magnetic fieldInterfaces directly to GRS 77 for determining accurate magnetic heading
Mode S capability    Interfaces with Traffic featureStandard Garmin features    Auto ALT mode when groundspeed is greater ...
Connected Directly to GDC 74A    Provides OAT information
GNS 480, CNX 80, GNS 400W series or GNS 500W seriesUsed as the “navigator”    Crossfills into G500Contains GPS receiver
Menu button and soft keys – Context sensitive depending on page selectedSystem settings on MFD can be selected specificall...
Airspeed IndicatorAirspeed Indicator
Attitude IndicatorAttitude Indicator
AltimeterAltimeter
Vertical Speed IndicatorVertical Speed Indicator
Horizontal Situation IndicatorHorizontal Situation Indicator
Turn CoordinatorTurn Coordinator
Able to access different functions depending on the context of the display  Many shortcuts are available through soft keys...
Both PFD and MFD power on with a red ‘X’ on various items until theAHRS has aligned and air data is available      The AHR...
Airspeed IndicatorAttitude Indicator (& Slip-Skid Indicator)AltimeterVertical Speed IndicatorHorizontal Situation Indicato...
Measured by the Air Data ComputerAirspeed indicated by moving tape    Also boxes for IAS, TAS and GSSix second trend vecto...
Airspeed and Altimeter tapes translucent to allow full view of horizon  Shows pitch warnings using red chevrons when attit...
Measured by the air data computerAltimeter settings must be entered in 2 placesAltitude bug displayed on left side of tape...
Measured by the air data computerThe scale of the VSI will dictate the range of the ASIVertical Speed bug can be set on th...
Includes a turn rate indicator, heading indicator, course pointerand CDI Trend vector serves as the rate indicator Able to...
Wind Vector
Wind VectorOutside Air Temperature
Wind VectorOutside Air TemperatureVDI (Vertical Deviation Indicator)    Either Glideslope or VNAV
Synthetic Vision Technology (SVT)                                             https://buy.garmin.com/shop/shop.do?pID=3763...
MFD panel is identical  MFD panel is identicalto PFD to PFD  Contains dedicated  Contains dedicatedpages for Traffic and p...
Typical Garmin page group/page layout    Map page group    Weather page group (if equipped)    Auxiliary page group    Fli...
Used only for situational awareness – no advisoryWill only be available if the GTX 330 installed    Uses mode STraffic can...
TAS unit must be installed to use this feature  Should only be used for situational awareness – Will provide advisories bu...
Terrain feature should only be used for situational awareness  NOT a radar – uses databases to predict terrain and potenti...
Requires GDL 69A receiverXM weather is a satellite uplink    Not a short range navigation tool    Refreshes a certain inte...
GWX 68  Provides weather and ground mapped radar  Probably not used in the DA20 but the G500 is also certified for Class 2...
Enhances situationalawareness at airports  Aircraft is shown on themap for ease of taxi  Taxiway identificationscan be rem...
G500 OverviewG500 OverviewComponentsComponentsPFD (Primary Flight Display)PFD (Primary Flight Display)MFD (Multi Function ...
Airspeed FailAirspeed FailCondition: Display is not receiving airspeed input from theCondition: Display is not receiving a...
Altitude FailAltitude FailCondition: Display is not receiving altitude input from the AirCondition: Display is not receivi...
Vertical Speed FailVertical Speed FailCondition: Display is not receiving vertical speed input from Condition: Display is ...
Heading FailHeading FailCondition: Display is not receiving valid heading input from Condition: Display is not receiving v...
Red XRed XCondition: A red X through any data field, indicates that theCondition: A red X through any data field, indicate...
AHRS Align – Keep Wings LevelAHRS Align – Keep Wings Level••Attitude and Heading Reference System is aligning Attitude and...
NO GPS POSITIONNO GPS POSITION••GPS data on the systems is no longer valid GPS data on the systems is no longer valid••The...
TRAFFICTRAFFIC•• The configured traffic system has determined that nearby   The configured traffic system has determined t...
No Traffic DataNo Traffic Data•• The configured traffic system is not able to detect traffic   The configured traffic syst...
Various Alert Messages – “MFD-Alerts” Soft KeyVarious Alert Messages – “MFD-Alerts” Soft Key•• view and understand all adv...
G500 da20 c 1
G500 da20 c 1
G500 da20 c 1
G500 da20 c 1
G500 da20 c 1
G500 da20 c 1
G500 da20 c 1
G500 da20 c 1
G500 da20 c 1
G500 da20 c 1
G500 da20 c 1
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G500 da20 c 1

  1. 1. Diamond DA20-C1 EclipseDiamond DA20-C1 EclipseDiamond DA20-C1 EclipseDiamond DA20-C1 Eclipse
  2. 2. G500 OverviewG500 OverviewComponentsComponentsPFD (Primary Flight Display)PFD (Primary Flight Display)MFD (Multi Function Display)MFD (Multi Function Display)
  3. 3. Digital Components – ADC, AHRS, GPSTIS or TAS: Traffic AwarenessTerrain and Obstacle databaseDual 6.5” LCD screens that are direct sunlight readableHigh resolution 640x480VGAXM weather or weather RadarSVT: Synthetic terrain on PFD overlayAutopilot interfaceSame panel space as standard 6 pack
  4. 4. A network of LRUsEach unit is self contained and modular in designEach LRU has a specific function or set of functionsEase of troubleshooting and maintenance
  5. 5. GDC 74A – Air Data ComputerGRS 77 – Attitude, Heading and Reference SystemGMU 44 – MagnetometerGTX 330 – Mode S TransponderGTP 59 – Outside Air Temperature Probe
  6. 6. Compiles information from the pitot static system and outside airtemperature (OAT) sensor Communicates with GDU 620 and GRS 77
  7. 7. Basically a solid-state gyro. Uses tilt sensors, accelerometers and ratesensors Contains an IGRF which must be updated every five years Interfaces with GDC 74A and GMU 44
  8. 8. Senses Earth’s magnetic fieldInterfaces directly to GRS 77 for determining accurate magnetic heading
  9. 9. Mode S capability Interfaces with Traffic featureStandard Garmin features Auto ALT mode when groundspeed is greater than 30kts and auto GND mode when less than 30kts Solid state electronics require no warm-up time
  10. 10. Connected Directly to GDC 74A Provides OAT information
  11. 11. GNS 480, CNX 80, GNS 400W series or GNS 500W seriesUsed as the “navigator” Crossfills into G500Contains GPS receiver
  12. 12. Menu button and soft keys – Context sensitive depending on page selectedSystem settings on MFD can be selected specifically for each userAuto or manual backlightingDual GDU 620 installation Shares information by crossfilling – baro and CDI can be selected to synchronize manually
  13. 13. Airspeed IndicatorAirspeed Indicator
  14. 14. Attitude IndicatorAttitude Indicator
  15. 15. AltimeterAltimeter
  16. 16. Vertical Speed IndicatorVertical Speed Indicator
  17. 17. Horizontal Situation IndicatorHorizontal Situation Indicator
  18. 18. Turn CoordinatorTurn Coordinator
  19. 19. Able to access different functions depending on the context of the display Many shortcuts are available through soft keys – should be incorporated inyour scan
  20. 20. Both PFD and MFD power on with a red ‘X’ on various items until theAHRS has aligned and air data is available The AHRS will align during taxi and level flight Various annunciations will illuminate during startup Should disappear after 30 seconds Databases should be checked on MFD splash screen
  21. 21. Airspeed IndicatorAttitude Indicator (& Slip-Skid Indicator)AltimeterVertical Speed IndicatorHorizontal Situation Indicator (& Standard Rate Turn Indicator)
  22. 22. Measured by the Air Data ComputerAirspeed indicated by moving tape Also boxes for IAS, TAS and GSSix second trend vectorIAS box turns red if VNE is imminent in 6 seconds
  23. 23. Airspeed and Altimeter tapes translucent to allow full view of horizon Shows pitch warnings using red chevrons when attitude is 50º above or 30º belowhorizon Extreme attitude - PFD declutters Contains slip-skid indicator
  24. 24. Measured by the air data computerAltimeter settings must be entered in 2 placesAltitude bug displayed on left side of tape Gives visual and audible advisoriesAlso contains trend vector
  25. 25. Measured by the air data computerThe scale of the VSI will dictate the range of the ASIVertical Speed bug can be set on the left side of the VSI tapeThe vertical speed value located at the bottom of the tape
  26. 26. Includes a turn rate indicator, heading indicator, course pointerand CDI Trend vector serves as the rate indicator Able to show magnetic or true headings
  27. 27. Wind Vector
  28. 28. Wind VectorOutside Air Temperature
  29. 29. Wind VectorOutside Air TemperatureVDI (Vertical Deviation Indicator) Either Glideslope or VNAV
  30. 30. Synthetic Vision Technology (SVT) https://buy.garmin.com/shop/shop.do?pID=37631https://buy.garmin.com/shop/store/assets/images/products/010-0G600-SVT/en/sc-04-lg.jpg
  31. 31. MFD panel is identical MFD panel is identicalto PFD to PFD Contains dedicated Contains dedicatedpages for Traffic and pages for Traffic andterrain terrain Displays all flight plan Displays all flight plandata crossfilled from data crossfilled fromnavigator unit navigator unit
  32. 32. Typical Garmin page group/page layout Map page group Weather page group (if equipped) Auxiliary page group Flight plan page groupSoft keys offer short cuts to many actions
  33. 33. Used only for situational awareness – no advisoryWill only be available if the GTX 330 installed Uses mode STraffic can be overlaid on navigation map pages
  34. 34. TAS unit must be installed to use this feature Should only be used for situational awareness – Will provide advisories butno resolution Uses mode S transponder to actively scan for other transponders Traffic can be overlaid on navigation map pages
  35. 35. Terrain feature should only be used for situational awareness NOT a radar – uses databases to predict terrain and potential impactpoints
  36. 36. Requires GDL 69A receiverXM weather is a satellite uplink Not a short range navigation tool Refreshes a certain intervals so information becomes expired quicklyRequires a subscription and activation
  37. 37. GWX 68 Provides weather and ground mapped radar Probably not used in the DA20 but the G500 is also certified for Class 2airplanes (Light twins 6000lbs and less)
  38. 38. Enhances situationalawareness at airports Aircraft is shown on themap for ease of taxi Taxiway identificationscan be removed withDCLTR
  39. 39. G500 OverviewG500 OverviewComponentsComponentsPFD (Primary Flight Display)PFD (Primary Flight Display)MFD (Multi Function Display)MFD (Multi Function Display)
  40. 40. Airspeed FailAirspeed FailCondition: Display is not receiving airspeed input from theCondition: Display is not receiving airspeed input from theAir Data Computer; accompanied by a red X through theAir Data Computer; accompanied by a red X through theairspeed display.airspeed display.•• Use standby Airspeed Use standby Airspeed
  41. 41. Altitude FailAltitude FailCondition: Display is not receiving altitude input from the AirCondition: Display is not receiving altitude input from the AirData Computer; accompanied by a red X through theData Computer; accompanied by a red X through thealtitude display.altitude display.•• Use standby Altimeter Use standby Altimeter
  42. 42. Vertical Speed FailVertical Speed FailCondition: Display is not receiving vertical speed input from Condition: Display is not receiving vertical speed input fromthe Air Data Computer; accompanied by a red X through the the Air Data Computer; accompanied by a red X through thevertical speed display. vertical speed display.•• Cross check instruments Cross check instruments
  43. 43. Heading FailHeading FailCondition: Display is not receiving valid heading input from Condition: Display is not receiving valid heading input fromthe AHRS; accompanied by a red X through the digital the AHRS; accompanied by a red X through the digitalheading display. heading display.•• Use standby compass or GPS Track information Use standby compass or GPS Track information
  44. 44. Red XRed XCondition: A red X through any data field, indicates that theCondition: A red X through any data field, indicates that thedisplay field is not receiving valid data..display field is not receiving valid data..•• Reference the data source of alternate equipment Reference the data source of alternate equipment
  45. 45. AHRS Align – Keep Wings LevelAHRS Align – Keep Wings Level••Attitude and Heading Reference System is aligning Attitude and Heading Reference System is aligning••Keep wings level using the standby attitude indicator Keep wings level using the standby attitude indicator••AHRS will align even if you must bank, but the alignment AHRS will align even if you must bank, but the alignmenttime may be slightly longer if manoeuvring time may be slightly longer if manoeuvring ••Limit aircraft banking as AHRS aligns. OK to taxi. Limit aircraft banking as AHRS aligns. OK to taxi.
  46. 46. NO GPS POSITIONNO GPS POSITION••GPS data on the systems is no longer valid GPS data on the systems is no longer valid••The Moving Map and associated data as not updating The Moving Map and associated data as not updating ••If equipped with dual GPS, press the “1-2” button If equipped with dual GPS, press the “1-2” button
  47. 47. TRAFFICTRAFFIC•• The configured traffic system has determined that nearby The configured traffic system has determined that nearbytraffic may be a threat to the aircraft. traffic may be a threat to the aircraft. ••Visually acquire the traffic to see and avoid Visually acquire the traffic to see and avoid
  48. 48. No Traffic DataNo Traffic Data•• The configured traffic system is not able to detect traffic The configured traffic system is not able to detect trafficand/or provide the pilot with any traffic awareness. and/or provide the pilot with any traffic awareness. ••Use vigilance, as the traffic sensor is not able to detect Use vigilance, as the traffic sensor is not able to detect traffic traffic
  49. 49. Various Alert Messages – “MFD-Alerts” Soft KeyVarious Alert Messages – “MFD-Alerts” Soft Key•• view and understand all advisory messages. Typically, view and understand all advisory messages. Typically,they indicate communication issues with the G500 system. they indicate communication issues with the G500 system.Refer to the G500 Cockpit Reference for the appropriate Refer to the G500 Cockpit Reference for the appropriatepilot or service action pilot or service action

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