Operators and Maintenance Manual
Display
EEM MOT 01 FE04.01
Page
10/16
Copyright:
Auto & Aero Technologies Sp. z o.o.
Mazowiecka 10/5, 20-723 Lublin, Poland
■
email: [email protected]
■
www.aatech.pl
Thus, information on the status of a flight parameter is presented in two
ways:
1)
by means of the colour of two status diodes according to the
following colour code:
a)
green
–
engine parameters within normal range;
b)
orange
–
warning;
c)
red
–
alarm;
2)
by means of the colour of digits and bar graph (if applicable)
presenting the value of the parameter:
a.
green
–
engine parameters within normal range;
b.
orange
–
warning;
c.
red
–
alarm;
The status information is obtained as a result of analysis conducted by the
instrument on the basis of digital input transmitted by the measurement
modules of the system.
Both diodes are always of the same colour corresponding to the status of
the parameter that assumes
“the worst” value.
