Embraer EMB145 Operation Manual page 209

NORMAL PROCEDURES
The ERJ145/135 anti-ice system is such that if any ice is detected
at a speed above 25 Kt the whole ice protection system goes ON.
If chances are that ice will be encountered during takeoff then REF
A/ICE must be set to ON so that the FADEC allows a ITT margin
for the anti-ice ON condition.
If REF A/ICE is set to ON then the takeoff performance-limited
weight must be based on the anti-ice ON condition.
EXTERIOR LIGHTS Panel ......................................... AS REQUIRED
Engine 2 Fire Handle .................................................. PUSHED IN
FLIGHT CONTROLS Panel ........................................ CHECK
AILERON SHUTOFF SYS 1 and 2 Buttons ..... PUSHED IN
RUDDER SHUTOFF SYS 1 and 2 Buttons...... PUSHED IN
Electric Hydraulic Pumps ............................................ CHECKED &
Select the MFD HYD page and switch both electric hydraulic
pumps to AUTO. Verify that the indicated pressures are within
2900 200 psi. Check also the hydraulic fluid level of systems 1
and 2 are within normal range.
Switch both electric hydraulic pumps to ON and verify that the
indicated pressures are within 2900
NOTE: The electric hydraulic pumps should never be switched ON
if the battery is the sole source of electrical power. If the
batteries are the sole source of electrical power, wait until
the APU or a GPU is available before switching ON the
electric hydraulic pumps.
After both pumps have been checked, turn them OFF.
LOGO and DOME Lights ............................................ AS REQUIRED
Pax Signs .................................................................... ON
Switch the FSTN BELTS and NO SMKG signs ON.
Ice Protection .............................................................. SET
Make sure that the ENG, WING and STAB buttons are pressed. If
some of them are not pressed, press them now. The SENSORS
buttons must also be pressed. The WINDSHIELD buttons need to
be pressed only if the windshield needs defogging.
The ICE DETECTION OVERRIDE knob must be in AUTO.
Page
1-02-17
6
AIRPLANE
OPERATIONS
MANUAL
Code
01
OFF
200 psi.
REVISION 37