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they will all move along together. The autopilot airspeed bug is set using the AFDS IAS/MACH
display window.
© Holger Ludwig, EuCom Airlines & Terry Yingling Seite 8 von 53
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Altimeter
DH Bug
DH Bug Knob
Baro Knob
The altimeter setting is shown in both Millibars and Inches of Hg. The altimeter setting is
adjusted by clicking on the left or right side of the BARO knob. Both MB and HG readouts will
respond to the BARO knob movement.
The orange altimeter bug is a selectable Decision Height (DH) bug. Clicking over the left or
right side of the DH Bug knob will cause the DH Bug to rotate around the altimeter.
Additionally, there is a DH window in the EADI just above the digital Radio Altitude readout.
The digital DH readout responds to movement of the altimeter DH bug and indicates the same
value. When the aircraft reaches the radio height indicated in the DH window the radio altitude
readout will change to orange and the GPWS system will call out "Minimums, Minimums".
Tape Radio Altimeter
There are two radio altimeters. The digital readout located in the upper right corner of the EADI
and the tape radio altimeter. The tape radio altimeter only reads out to 1,400ft. The digital
readout displays altitude up to 2,500 feet above the ground.
Vertical Speed
A Vertical Speed indicator is available and is calibrated to show assent or decent in thousands
FPM.
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Electronic Attitude Director Indicator
Artificial Horizon Angle Bank Indicator
Slip Indicator Pitch Bar Indicator
The EADI combines many functions into one instrument. Basic flight guidance is provided by
an artificial horizon for pitch and roll control. At the bottom of the EADI is a slip indicator for
yaw control. Description of the other functions of the EADI is provided in the Navigation
Systems section of this manual.
Throttles
The two throttles may be operated together or when dragged with the mouse, independently.
Reverse thrust is available.
Flaps
Flaps are operated by clicking on the gauge. A plus sign shown will lower the flaps and a minus
sign will raise them.
© Holger Ludwig, EuCom Airlines & Terry Yingling Seite 10 von 53
http://www.eucomairlines.de
Landing Gear
Looking at the picture at left you will see outlined the mouse click areas. Box "1" is where you
click for gear down. Box "2" is where you click for gear up. Box "3 is something new called the
OFF position. Once the gear have retracted and you are climbing out the procedure is to put the
gear handle in the OFF position. This cuts power to the hydraulic systems feeding the landing
gear assembly. So clicking on "3" will bring the handle down to OFF (as shown). Box "4" is
normally an override switch but we are using it as a test switch. Pressing it will test all the
landing gear indicator lights.
A note about the Tail Skid light. Even though it illuminates during the test, it is non operational.
This light only illuminates if the tail skid is out of position and the warning is suppressed during
normal operations.
Spoilers
Just click and drag the spoiler handle to extend or retract the spoilers.
© Holger Ludwig, EuCom Airlines & Terry Yingling Seite 11 von 53
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NAVIGATION SYSTEMS
RMI
DME 1 DME 2
VOR 2 VOR 1
Source
Selection
A significant feature of the RMI is the ability to select the Nav source for each course needle.
Clicking over each knob will change position to indicate the Nav source and the corresponding
needle will point accordingly. VOR 1 is the dashed arrow, VOR 2 is the outlined arrow.
VOR1, VOR2 and ADF are the allowable Nav sources. However, since there is only one ADF
possible in FS2000 both pointers will point to the same ADF. DME 1 and DME 2 correspond to
Nav 1 and Nav 2 information.
AFDS Status
Indicates the status of the autopilot. If the autopilot is engaged the green CMD annunciator will
show. If the autopilot is not engaged but the flight director is in use a green FD would show. If
the AFDS is in FD mode then the flight director bars will command your flight based on
autopilot inputs. Therefore, the pilot can manually fly the aircraft and still have complete control
of the flight director through the autopilot.
Ground Speed DH Alt
Speed Deviation Scale Radar Alt
Glideslope
AutoThrottle Mode
N1 Runway Closure
SPD
FL CH
AFDS Status FD CMD
Vertical Modes Lateral Modes
(lower) (upper) (lower) (upper)
　
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