Embraer EMB145, Operation Manual

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NORMAL PROCEDURES AIRPLANE
OPERATIONS
MANUAL
1-02-17
Page
10
Code
01 REVISION 40 AOM
-145/
111
4
Verify if the ATC/TCAS window is in SBY. Select the ABOVE
function.
Test the TCAS by placing the yellow cursor box over the code.
Press the RMU test button for 5 to 7 seconds until the test OK
message on the RMU and "TCAS TEST, PASSED" aural
annunciation is heard.
Enter the flight number or CALL SIGN on the appropriated window
into the RMU.
Verify that BACK-UP TUNING is set to NORMAL and is copying
RMU2.
Flight Control DISCONNECT Handles ......................... CHECK
Speed Brake Lever ....................................................... CLOSED
Thrust Levers ................................................................ IDLE
Stall Protection System................................................. CHECKED
The AHRS 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.