AIRCRAFT
DA 42 NG AMM
Indicating Systems
Doc # 7.02.15
Rev. 4
31-40-00
Page 9
15 Mar 2018
B. Multi-Function Display (MFD)
The MFD is a 10.4 in liquid crystal display. Bezels on the left and right side of the MFD have the
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controls for the ICS. The lower edge of the MFD has ‘softkeys’. The function of the soft keys relates
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to the on-screen display and if a key has a function related to the current display the display will
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show the function of the key.
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The MFD displays engine and airplane pages on the left slide of the screen. The remainder of the
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screen is used to display navigational pages. The bezels on the left and right side of the MFD have
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the same controls and function as the bezels on the PFD. The left side bezel on the MFD has also
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the controls for the autopilot system. Refer to Chapter 22 for more information about the autopilot.
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The Engine instrumentation system window (EIS) is on the left side of the MFD and displays a full-
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time dedicated display of engine parameters. The information is presented in three displays:
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Engine Display. This is the default display and shows following critical engine and fuel
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indicators:
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Engine load. The engine loads are displayed as a percentage. Pointers on each side of a
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vertical scale move to show the engine load. If the system fails the display shows a red or
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yellow cross to the left or right of the load indicator to show which engine system has failed.
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Engine RPM. Pointers on each side of a vertical scale move to show the engine rpm. If the
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system fails the display shows a red or yellow cross to the left or right of the RPM indicator
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to show which engine system has failed.
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Fuel flow. Small windows to the left and right of a GPH marking show the engine fuel flow
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digitally. If the system fails a red or yellow cross is displayed in place of the digital indication
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for the failed system(s).
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Oil temperature. Pointers above and below a range bar indicate the oil temperature. The
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range bar is color coded, green to show the normal operating range, yellow in the cautionary
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range and red in the warning range. The pointers move from left to right to indicate the oil
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temperature. The pointer above the range bar indicates the oil temperature of the left engine
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and the pointer below the range bar indicates the oil temperature of the right engine. If the
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system fails a red or yellow cross is displayed above or below the range bar to show which
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engine system has failed.
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Oil pressure. Pointers above and below a range bar indicate the oil pressure. The range bar
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is color coded, green to show the normal operating range, yellow in the cautionary range and
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red in the warning range. The pointers move from left to right to indicate the oil pressure. The
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pointer above the range bar indicates the oil pressure of the left engine and the pointer below
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the range bar indicates the oil pressure of the right engine. If the system fails a red or yellow
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cross is displayed above or below the range bar to show which engine system has failed.
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Summary of Contents for DA 42 NG
Page 933: ...AIRCRAFT DA 42 NG AMM Fuel Doc 7 02 15 Rev 4 28 TITLE Page 1 15 Mar 2018 CHAPTER 28 FUEL ...
Page 1459: ...AIRCRAFT DA 42 NG AMM Lights Doc 7 02 15 Rev 4 33 TITLE Page 1 15 Mar 2018 CHAPTER 33 LIGHTS ...
Page 1711: ...AIRCRAFT DA 42 NG AMM Doors Doc 7 02 15 Rev 4 52 TITLE Page 1 15 Mar 2018 CHAPTER 52 DOORS ...
Page 1853: ...AIRCRAFT DA 42 NG AMM Wings Doc 7 02 15 Rev 4 57 TITLE Page 1 15 Mar 2018 CHAPTER 57 WINGS ...
Page 2071: ...AIRCRAFT DA 42 NG AMM Engine Doc 7 02 15 Rev 4 72 TITLE Page 1 15 Mar 2018 CHAPTER 72 ENGINE ...
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