Hélicoptères Guimbal
SECTION 7
CABRI G2
SYSTEMS DESCRIPTIONS
7-12
Approved under DOA EASA.21J.211
Starting sequence
The EPM is powered through the MASTER switch. The functioning
synoptic after switching on is as follows:
System startup
–
logo displayed
Welcome page
–
software releases
Flight log page
Sensors test and alarms page
Flight screen
Note :
Hot start is defined by “Rotor in flying mode” signal (refer to
page 7-17).
After an unexpected power cut in this condition, the EPM flight
screen recovers within seconds.
Restart in the Flight log page can be done by pressing key #3
for 1 sec. while on the ground with rotors and engine stopped.
Flight log page
This page presents, for each of the
last 36 flights
:
•
The date and time of the engine start-up,
•
The technical time (refer to page 7-14),
•
The flight time (refer to page 7-14),
•
The average fuel consumption (refer to page 7-15),
•
The fuel quantity added since previous flight.
Configuration
page
Hot start
Maintain key #3 for 1 sec
