Embraer EMB145 - Page 461

AIRPLANE
OPERATIONS
MANUAL
ABNORMAL
PROCEDURES
REVISION 38
1-03-37
Page
3
Code
03
AOM-145/1114
ESSENTIAL BUS 1 OFF
EICAS CAUTION: ESS BUS 1 OFF
LIGHT: Master Caution
MFD Indication: ESS BUS may be amber.
On Reversionary Panel 1:
SG............................................................................ PUSH IN
Fuel Pump 1 ................................................................. 1B OR 1C
Fuel Pump 2 ................................................................. 2A OR 2C
Altitude .......................................................................... MAX 25000 FT,
MINIMUM MEA
WARNING:
IF IN ICING CONDITIONS, REFER TO SINGLE
ENGINE OR SINGLE BLEED OPERATION IN ICING
CONDITIONS PROCEDURE.
COM 2 on Digital Audio Panel 2 ................................... PUSH IN
Monitor fuel quantity indication 1 through FMS.
Brake effectiveness will be reduced.
If the EICAS is not energized:
DAU 1 on EICAS Rev.............................................. PUSH IN
At pilot’s discretion, on Reversionary Panel 1:
MFD Knob .......................................................... EICAS
Landing configuration:
Landing Gear ........................................................... DOWN
Flaps ........................................................................ 45°
Airspeed................................................................... V
REF 45
CAUTION: TO DETERMINE THE MINIMUM SUITABLE LANDING
DISTANCE, MULTIPLY THE UNFACTORED LANDING
DISTANCE FOR FLAPS 45° BY 1.45.