Embraer EMB145 - Page 476

ABNORMAL
PROCEDURES
AIRPLANE
OPERATIONS
MANUAL
1-03-45
Page
2
Code
03
REVISION 40
AOM-145/1114
ONE ENGINE INOPERATIVE GO-AROUND
Quick Disconnect Button............................................... PRESS
Go Around Button ......................................................... PRESS
Engine Thrust Levers.................................................... MAX
Rotate to go-around attitude (10° nose up).
Flaps ............................................................................. 9°
With positive rate of climb:
Landing Gear ........................................................... UP
Minimum Airspeed ................................................... APPROACH
CLIMB SPEED
At level off height, proceed as for TAKEOFF WITH ENGINE FAILURE
Procedure.
NOTE: - Limiting bank angle to 5° towards operative engine improves
climb performance.
- During GO-AROUND procedure, the DON’T SINK aural
warning may sound. In this case monitor the sink rate and
follow the GO-AROUND guidance.
ENGINE ROTOR BURST
CONDITION: Depending on the burst direction, one of the following
conditions may be verified: E1 (or E2) FIREDET FAIL
message displayed simultaneously with engine failure,
or a sudden cabin depressurization, or impact noise, or
hydraulic system failure.
ENGINE FIRE, SEVERE DAMAGE
OR SEPARATION Procedure.................................. APPLY