iS
G3-8 MA FM 9407 - R01
7
Airplane and Systems Description
Systems 7 - 16
screen of DYNON HDX800/HDX1100
Figure shows elements. Display may vary in flight
primary instrumentation
The primary flight instrumentation and engine indication are realized
by the DYNON SkyView glass cockpit system. This is an integrated
system, it includes the “Electronic Flight information Display” and the
„Multinational Function Display“. Any primary and secondary flight in-
struments as well as navigation and engine instruments are shown on
the screen. This does not include the fuel tank indication. Although
such an instrument is integrated into the SkyView, the primary fuel
indication is the fuel sight tube behind the right seat.
standby instrumentation
A dedicated airspeed indicator and altimeter may be installed in the
left panel, but the primary instrumentation is the DYNON system.
Summary of Contents for GXiS
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Page 93: ...iS G3 8 MA FM 9405 R01 5 Performance Performance 5 11 5 6 Cruise Speed and Fuel Flow...
Page 94: ...iS G3 8 MA FM 9405 R01 5 Performance Performance 5 12 5 7 Range and Endurance...
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Page 96: ...iS G3 8 MA FM 9405 R01 5 Performance Performance 5 14 5 8 Rate of Climb...
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Page 116: ...iS G3 8 MA FM 9406 R01 6 Weight and Balance Weight and Balance 6 16 intentionally left blank...
Page 199: ...REMOS GXiS POH Supplement Flight Training...
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Page 214: ...REMOS GXiS POH Supplement Continued Airworthiness...
Page 230: ...REMOS GXiS POH Supplement Abbreviated Checklists...
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