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(electrical or otherwise) of these screens the standby engine gauge can display critical engine
data.
© Holger Ludwig, EuCom Airlines & Terry Yingling Seite 31 von 53
http://www.eucomairlines.de
Normally the standby engine gauge is not visible. When the switch is in the AUTO position the
display will be blank. In the AUTO position the display remains blank until there is an electrical
failure and the EICAS screens are inoperative. Switching to ON will force the engine data to be
displayed at all times regardless of EICAS status.
Autobrakes
Operation of the autobrake is by mouse click left or right of the knob. The following settings are
available:
RTO is used for takeoff. In the event of a rejected takeoff full application of the brakes will take
place until the pilot disarms the system or the autobrake automatically disarms.
OFF turns the autobrakes off.
DISARM occurs automatically when the plane slows below a certain speed depending on the
situation. Anytime the autobrake is disarmed you will get an EICAS message. Also when the
autobrake is automatically or manually disengaged after landing or RTO the AUTO BRAKE
warning annunciator will illuminate.
1 2 3 4 MAX: The autobrake is armed for engagement after landing. 1 is the lowest setting and
will result in the least amount of automatic braking. MAX is the highest setting and results in
maximum automatic application of braking after landing.
In all cases the autobrake is disengaged automatically after speed reduction is accomplished,
manually via brake application by the pilot, or manually by switching the switch to OFF.
Standby Flight Instruments
The standby instruments (Airspeed, Altitude and Vertical Speed) are in a separate window that is
displayed by using the STBY INST button located on the panel below the EICAS screens or by
the SHFT-3 keyboard combination.
© Holger Ludwig, EuCom Airlines & Terry Yingling Seite 32 von 53
http://www.eucomairlines.de
Clock
There are 3 major features of the clock: GMT time display, Elapsed
timer, and chronometer.
The GMT time display shows Zulu time. It is adjustable by clicking
directly on the digital display.
The elapsed timer (ET) knob when set to the HOLD (HLD) position
means the elapsed timer is not running. The elapsed timer can be used to
keep track of total flight time or other long term timing needs. Use the mouse click to put the ET
knob to RUN which starts the elapsed timer. The secondhand does not move during operation of
the ET function and the time displayed in the ET/CHR window will be hours:minutes. To reset
the ET just click over the “RESET” and the ET knob will momentarily move to RESET and then
spring back to HLD. This knob is spring loaded to HLD. If at anytime it is necessary to
temporarily hold the elapsed timer and then restart it without resetting, just go back and forth
between RUN and HLD without resetting the ET displayed. The elapsed timer is not affected by
changes in the GMT or the use of the chronometer.
The chronometer is nothing more than a stopwatch. Click the CHR button to start the
chronometer timing. The second hand operates to show seconds and the ET/CHR window
shows minutes. To stop the timing press the CHR button again. Once the chronometer is
stopped it cannot be restarted...the next click of the CHR button will reset the chronometer. Use
of the chronometer is independent of the ET display. The ET runs in the background while the
chronometer is running and will be displayed again once the CHR is reset
OVERHEAD SYSTEMS PANEL
The overhead is called up by pressing either Shift-4 or using the button labeled "LT OVRD" on
the visible portion of the overhead.
A feature of this panel is the ability to start with a completely "cold" aircraft. This means that all
of the systems and buttons are in the off position. All of the switch positions will be
remembered by the panel for the next time the simulator is started.
Turning on the BAT switch brings power to the overhead switches.
© Holger Ludwig, EuCom Airlines & Terry Yingling Seite 33 von 53
http://www.eucomairlines.de
ELECTRICAL SYSTEMS
The heart of this aircraft's systems is the electrical system. If this panel is not set up properly
then you will have all kinds of trouble with your instrumentation because all aircraft components
are dependent on electrical power being available. There are 3 main power sources for this
aircraft: battery power, external power, and APU generator power. EICAS messages are
generated for all aspects of the electrical system.
Battery Power
The batteries are selected ON using the pushbutton under the guarded switch labeled BAT.
　
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