111
AI - attitude indicator
DG - directional gyro
VSI - vertical speed indicator
ALT - altimeter
ASI - airspeed indicator
TC - turn coordinator
FAILURE TIME WINDOW
The “Between” column is used to set the “failure time window” inter-
val. The values entered in minutes (00-99) are compared to the Ref.
Failure Time and determine when or during what time period (win-
dow) the corresponding ARMed failure will occur. If for example we
want the Attitude Indicator to gradually fail at some point between
seven and fifteen minutes from now, we would simply enter 07 and
15 respectively in the “Between” column and press the ARM button
in the “Gradual” column next to “AI.” If this were done at the start of
our flight the Ref. Failure Time would already be set to zero. But, if
we had been flying for some time and wanted the failure to occur be-
tween seven and fifteen minutes from now we could just RESET the
Ref. Failure Time. As the Ref. Failure Time counts up from zero as
we fly, the Attitude Indicator will begin its gradual failure at some
time between seven and fifteen minutes.
Содержание iGATE G500 Series
Страница 17: ...17 Single Seat Twin Piston iGATE Closed Cockpit Configuration iGATE Dual Control with Center Console ...
Страница 20: ...20 iGATE with 3 screen projection display iGATE with Curved Screen Projection ...
Страница 21: ...21 Desktop iGATE Twin Engine w G1000 Avionics Cockpit iGATE Twin Engine w HSI and RMI ...
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Страница 135: ...135 ADDING FACILITIES ...
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Страница 152: ...152 Abbreviate Operation of the EFS Control Panel ...
Страница 154: ...154 EFS Symbol Definition ...
Страница 155: ...155 EADI Symbology Definition ...