Embraer EMB145 - Page 226

AIRPLANE
OPERATIONS
MANUAL
NORMAL PROCEDURES
REVISION 40
1-02-17
Page
11
Code
02
AOM-145/1114
Thrust Levers................................................................ IDLE
Stall Protection System................................................. CHECKED
The AHRS/IRS should be aligned.
CUTOUT 1 and 2 buttons must be guarded and not illuminated and
QUICK DISCONNECT BUTTON must be released.
Carry out the Stall Protection System test as follows:
- Pull the control column all the way back and momentarily
press the SPS TEST button (the TEST button must not be
kept pressed beyond the shaker actuation). Both stick
shakers and stick pusher will actuate, the caution and
warning lights will illuminate and an aural warning will be
heard.
- Lightly counteract the control column tendency to move
forward.
- The test takes about 5 seconds and is valid if the amber light
on the TEST button extinguishes.
- Press the caution and warning light buttons to turn them off.
Trims............................................................................. CHECKED
Verify that the aileron, rudder, main and backup pitch trims are
operating properly both ways up to the 3 seconds automatic stop;
leave the aileron and rudder trims to the neutral and the pitch trim
to the green band.
BACK-UP TUNING (if installed) ................................... SET
Set to NORMAL and copying RMU2.
COMM 3 (if installed).................................................... SET
Press the transfer button in case of an error message on the radio
display.
Pressurization ............................................................... SET
Set the system to the destination airport elevation and verify that
the DUMP and AUTOMAN switches are guarded and were not
pushed (if they have been pushed the white mark on the buttons
will be lit). The manual controller knob must be set to the green
mark (DN position) to enable automatic pressurization control.