Embraer EMB145 - Page 481

AIRPLANE
OPERATIONS
MANUAL
ABNORMAL
PROCEDURES
REVISION 38
1-03-45
Page
7
Code
03
AOM-145/1114
ENGINE AIRSTART
Affected engine:
One Electric Fuel Pump (A or B) ............................. ON
Ignition ..................................................................... AUTO
Start/Stop Selector .................................................. STOP
Engine Bleed ........................................................... CLOSE
Thrust Lever............................................................. IDLE
Airspeed and Altitude.................................................... REFER TO
AIRSTART
ENVELOPE
Perform an assisted start or windmilling, as required:
CAUTION:
IN ICING CONDITIONS DO NOT USE APU BLEED
START, TO AVOID LOSS OF ANTI-ICE SYSTEM
PERFORMANCE.
Assisted start:
Crossbleed start:
N2 (operating engine)......................................... ABOVE 80%
Crossbleed ......................................................... AUTO OR
OPEN
Engine Bleed (operating engine)........................ OPEN
Start/Stop Selector ............................................. START, THEN
RUN
Engine Indication ................................................ MONITOR
Check ignition. Check N2 rising. Observe limits. Abort start
immediately if an Abnormal Engine Start is detected.
APU bleed start:
APU .................................................................... START
APU Bleed .......................................................... OPEN
Crossbleed ......................................................... AUTO OR
OPEN
Engine Bleed (operating engine)........................ CLOSE
If only the APU Generator is operative:
Windshield Heating ....................................... OFF
Electric Hydraulic Pump
(inoperative engine) ............................... OFF
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