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STANDBY ALTIMETER/AIRSPEED INDICATOR
The Standby Altimeter/Airspeed indicator uses the standby pitot-static source. The
standby indicated airspeed readout displays noncorrected indicated airspeed.
0
9
8
7
6
5
4
3
2
1
10 0 FEET
ALT
1 000 32
4
10 13
mb/hPa
29 9 2
IN HG
IAS KNOTS
180 200 220 250
BARO
GX_07_076
IAS KNOTS
0 60 80 100 120 140 160 180 200 220 250 300 350 400 450
SPEED IAS RANGE
ALTITUDE DRUM RANGE
ALTITUDE RANGE
-1,000 to + 51,000 FT
10,000 FT
DRUM
1,000 FT
DRUM
100 FT
DRUM
NEG
8
7
6
5
4
3
2
1
9
8
7
6
5
4
3
2
1
0
000
900
Below
Sea Level
Indication
Below
10,000 feet
Indication
ALTIMETER RANGE
mb/hPa
746
1013
1049
in Hg
22.00
29.92
30.99
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
7-104 For Training Purposes Only
Sept 04
STANDBY MAGNETIC COMPASS
A standby magnetic compass is located below the overhead panel, at the center of the
windscreen. The standby magnetic compass retracts into a compartment in the
overhead panel. The compass lighting is controlled by the Cockpit Lights Integral
panel, located on the pedestal.
GX_07_077
B 10 10 C
6
3
33 3 N
TO FLY N 45 E 135 S 225 W 315
STEER
STBY COMPASS WITH ALL RADIOS ON SWUNG / / BY
Bracket
Compensators
Compass
Dial
Compass Light Unit
Correction
Card
6
3
333
N
For Training Purposes Only
Sept 04
7-105
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
CLOCK
Two digital electronic clocks are installed on the side panels, and are the time base
source for the avionics equipment.
SEL
RST
ET
CHR
MODE
GPS
CHR
11:1350
01:43
GX_07_078
Time/Date Display
GMT, Local Time or Date
displayed here. Date is
displayed as month/day/year
and the colon (:) is removed
when in Date mode.
Mode Control
DT
GPS
INT
LT
– Date (mo/dy/yr)
– GPS fed GMT
– Internally computed
GMT (Manual selection)
– Local Time
Elapsed Time (ET) /
Chronometer (CHR)
Function
ET
CHR
– Corresponds to the
aircraft’s flight time from
takeoff (weight off wheels)
to landing (weight on
wheels). Automatic.
– Displayed as soon
as the CHR button is
pressed. Replaces ET if
present.
CHR Control
1st push
2nd push
3rd push
– Start and replaces ET in
bottom window if it was displayed.
– Stop. Value is held.
– Reset. Display zeroed
and blanked.
ET Controls
SEL
RST
– ET comes on in bottom
window. Does not increment
on ground.
– Blanks the digits and
resets to zero. Ground only.
Mode Display
DT
GPS
INT
LT
– Date (mo/dy/yr)
– GPS fed GMT
– Internally computed
GMT (Manual selection)
– Local Time
P I LOT T R A I N I N G GU I D E
ELECTRONIC DISPLAY SYSTEM
7-106 For Training Purposes Only
Sept 04
TIME SETTING
Set at Power-up
At the first application of power, the clock will be in GMT minutes adjustment if GPS
is invalid and the clock is not transmitting on the ARINC bus. If the GPS data is valid,
the clock is automaticafly updated and swiched in GPS mode.
In the SET function, the GMT minute’s digits are flashing. The flashing rate is one
flash per second. The setting is obtained by pressing the ET SEL pusbbutton to
decrease the data and pressing the ET RST button to increase the data. The counter
increments one digit for each push of the button. The INT flag is lit.
• By depressing the MODE button, the GMT hour’s digit is flashing, and you can
adjust the display in the same way. The INT flag is lit
• By depressing the MODE button once more, the year’s digits are flashing and you
can adjust the display in the same way. The DT flag is lit
• By depressing the MODE button once, the month’s digits are flashing and you can
adjust the display in the same way. The DT flag is lit
• By depressing the MODE button once, the day’s digits are flashing and you can
　
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