Embraer EMB145 - Page 475

AIRPLANE
OPERATIONS
MANUAL
ABNORMAL
PROCEDURES
REVISION 40
1-03-45
Page
1
Code
03
AOM-145/1114
POWER PLANT
ENGINE FAILURE
Remaining Engine Thrust Rating.................................. CON
Altitude .......................................................................... MAX 25000 ft
MINIMUM MEA
ENGINE AIRSTART Procedure ................................... AS REQUIRED
TCAS ............................................................................ TA ONLY
WARNING:
IF IN ICING CONDITIONS, REFER TO SINGLE
ENGINE OR SINGLE BLEED OPERATION IN ICING
CONDITIONS PROCEDURE.
In flight, the air conditioning pack valves will close automatically when:
 For AE3007A or AE3007A1/1 engines Pre-Mod. SB 145-73-
0010: below 15000 ft, TAT above -18°C and the remaining
engine at T/O-1 or CON mode.
 For AE3007A1 engines and AE3007A or AE3007A1/1 engines
Post-Mod. SB 145-73-0010: below 9700 ft, TAT above 19°C at
sea level, decreasing linearly to -5°C at 9700 ft and the
remaining engine is at T/O-1 mode.
 For AE3007A1P or AE3007A1/3 engines: below 9700 ft, TAT
above 19°C at sea level, decreasing linearly to -5°C at 9700 ft
and the remaining engine is at T/O or T/O RSV mode.
If APU bleed is being used, the packs are not shut down.
ONE ENGINE INOPERATIVE APPROACH AND
LANDING
Inoperative Engine Thrust Lever .................................. IDLE
Landing Gear ................................................................ DOWN
Thrust Rating ................................................................ TAKEOFF
MODE
When landing is assured:
Flaps ........................................................................ 22°
Airspeed................................................................... V
REF45
+ 10
KIAS
CAUTION:
TO DETERMINE THE MINIMUM SUITABLE LANDING
DISTANCE, MULTIPLY THE UNFACTORED LANDING DISTANCE
FOR FLAPS 45° BY 1.48.