Embraer EMB145 - Page 242

NORMAL PROCEDURES
AIRPLANE
O
PERATIONS
MANUAL
1-02-33
Page
2
Code
01
REVISION 41
Copyright © by Embraer. Refer to cover page for details.
AOM
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1
4
5/1
114
Ice Protection Test........................................................AS REQUIRED
The ice protection test must be carried out once a day (not
necessarily at the first flight of the day) when icing conditions are
forecast.
The test may be carried out completely on the ground, or in 2
separate phases (first phase on the ground and second phase in
flight), depending on weather conditions and crew discretion. For
ice protection test information, refer to AOM Supplementary
Procedures, Environmental, section 1-02-79.
Crossfeed......................................................................OFF
PC Power System (if installed) .....................................OFF
The PC Power System must be turned off until the airplane reaches
10000 ft.
Lights.............................................................................ON
Brakes Temperature .....................................................CHECKED
Verify on the MFD HYD page that the brakes temperature are
within the green range. Takeoff cannot be attempted with brake
temperatures outside the green range.
EICAS ...........................................................................CHECK
Check:
− No EICAS messages displayed.
− Thrust rate mode.
Transponder..................................................................TA/RA
Takeoff Configuration....................................................CHECK
Right Seat Pilot presses the T/O CONFIG Button and
“TAKEOFF OK” synthetic message shall be heard.
Flight Director................................................................ SET
Verify that the AUTOPILOT is selected to his side then press the
FD button and select GO AROUND by pressing the respective
button at the thrust lever head. Check that the flight director bar on
T/O mode became visible on the PFD.