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31 Cards in this Set
- Front
- Back
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The EFIS is composed of the EFIS control panel, the EADI and one other component.
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Electronic Horizontal Situation Indicator (EHSI)
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The electronic instrument displays (EID) receive sensor data from the ___.
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air data computer (ADC)
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Which of the following is a standby instrument?
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Turn and bank indicator
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Both the EADI and EHSI operate in the ___ modes.
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enroute and approach
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If the pitch values approach their limits, red chevrons are used to indicate the nearest direction ____.
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for a level attitude recovery
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The EHSI displays a 360* rotating compass scale divided into 5 and 10* increments and referenced to a _____.
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white triangular heading index (lubber line)
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Pulling out on the HDG knob resets the HDG bug to the present aircraft ____.
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heading
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The upper left corner of the EHSI contains which set of information, if selected?
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Distance to next selected point, aircraft groundspeed, and time to go to the next point.
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When the EHSI is in HSI normal mode, pressing the map button (MAP) changes the display to the ____ mode.
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navigation map
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The bearing pointer select buttons are used to cycle the EHSI bearing pointers through the ____ navigation source display, ____ navigation source display, or the ____ mode.
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VOR; GPS; declutter
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On the EHSI, the course deviation bar indicates the centerline of the selected course relative to ___.
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the aircraft symbol
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For ILS glidepath, a ___ is displayed on the right side of the instruments with a green deviation pointer which moves in relation to the scale to indicate glidepath center with respect to aircraft position.
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station vertical scale
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The VIS indicates to the pilot if the aircraft is climbing or descending, and at what _____.
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rate
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The VSI shows climbs or descents in feet per minute (FPM) from 0 to ____.
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6000
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The ASI Mach number window is blanked below ____ Mach.
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0.40
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As altitude increases, maximum operating airspeed (Vmo) will ___.
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decrease
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The baro-set correction knob is used to set ____ settings in the altimeter so it displays correct altitude indications.
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pressure
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The standby instruments can be used for a limited time in the event of a failure of the aircraft primary ____ system.
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electrical
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The red and white "barber pole" ont he airspeed indicator ____.
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is a velocity/Mach limiting pointer
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The standby attitude indicator is caged ____.
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by pulling and turning the PULL TO CAGE knob.
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The standby altimeter is operated by static pressure from the primary pitot/static system.
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FALSE
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Which system is not part of the T-6A flight instruments?
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Environmental system
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In the composite mode, both attitude and heading information can be displayed on either the EADI or EHSI
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TRUE
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The primary pitot probe at the right wingtip and primary static ports on the sides of the aft fuselage provide necessary pressures to the ___.
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air data computer
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The EFIS system provides uncluttered unusual attitude information on the EADI when the aircraft exceeds which set of predefined limits?
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Pitch +30* or -20*, roll angle greater than 65*
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The altimeter displays baro-set data into windows in what format?
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inches of mercury and millibars
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The conventional magnetic compass can be used in case of total electrical failure, or as an instrument cross-check
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TRUE
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If pitch or roll attitude failure cocurs, what words appear in red letters at the top center of EADI screen?
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ATTITUDE FAIL
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In NAV MAP mode on the EHSI, which full circle range scales are available?
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5,10,20,40,80,160,240,320, and 1000 NM
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The standby attitude indicator will supply accurate information for at least how many minutes after electrical failure?
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Nine
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If either pilot selects EFIS composite mode, the displays in the other cockpit are not affected.
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FALSE
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