Embraer EMB145 - Page 260

NORMAL PROCEDURES
AIRPLANE
OPERATIONS
MANUAL
1-02-69
Page
2
Code
01 REVISION 39
AOM-145/1114
Pitch Trim......................................................................SET
Reset the PITCH TRIM back in the green range (approx. 7.0 UP).
APU...............................................................................AS REQUIRED
If the intention is to start the APU, do it now. Do not use the APU
BLEED until the airplane is parked and with blocks on (wait at least
3 minutes for use APU bleed). This will maximize the APU life.
NOTE: To prevent spurious overcurrents in the electrical system,
engines must not be shut down concurrently with the
starting of the APU. A minimum one-minute interval
between those two procedures is recommended.
Transponder..................................................................STBY
Set the Transponder and the TCAS to Standby.
Gust Lock......................................................................LOCKED
The GUST LOCK must be applied immediately after the airplane
leaves the runway.
NOTE: In case of an overcurrent protection is actuated, and the EICAS
message DC BUS 2 OFF (PFD 2 and MFD 1 blank and MFD 2
displaying a red X) is displayed after a commanded engine 2
shutdown during taxi, the following actions must be carried out:
- Stop the airplane.
- Restart the engine 2.
- Taxi the airplane normally to the appropriate area.
- To shut the airplane down and reset the overcurrent
protection, refer to Shutdown Procedures.
CAUTION:
DURING TAXI, THE ENGINE 2 MUST NOT BE SHUT
DOWN JUST BEFORE OR DURING A TURN, AS THIS
MAY CAUSE STEERING COMMAND LOSS (STEERING
IS SUPPLIED BY DC BUS 2).