Embraer EMB145 - Page 492

ABNORMAL
PROCEDURES
AIRPLANE
OPERATIONS
MANUAL
1-03-48
Page
2
Code
03
REVISION 36
AOM-145/1114
CONTINUED FROM PREVIOUS PAGE
Approach and landing configuration:
Landing Gear ...................................................... DOWN
Flaps ................................................................... 22°
Airspeed.............................................................. V
REF 45
+
30 KIAS
Use rudder for directional control on the ground.
EMERGENCY BRAKE
TECHNIQUE Procedure..................................... ACCOMPLISH
Do not attempt to taxi.
CAUTION:
TO DETERMINE THE MINIMUM SUITABLE LANDING
DISTANCE, MULTIPLY THE UNFACTORED LANDING
DISTANCE FOR FLAPS 45° BY 2.86.
HYDRAULIC SYSTEM 1 FAILURE
EICAS CAUTION: HYD SYS 1 FAIL, RUDDER SYS 1 INOP,
AIL SYS 1 INOP
EICAS ADVISORY: E1 HYD PUMP FAIL
LIGHT: Master Caution
INDICATION: Hydraulic pressure indication on MFD may be amber.
Check hydraulic systems fluid quantity:
If hydraulic system fluid quantity is in green range:
Electric Hydraulic Pump 1................................... ON
If hydraulic system fluid quantity is in amber range:
Electric Hydraulic Pump 1................................... OFF
If hydraulic power is not recovered:
Airspeed................................................................... MAXIMUM
250 KIAS
Electric Hydraulic Pump 1........................................ OFF
NOTE: As the nose landing gear doors will open, the pilot should
expect a noise increasing during flight.
For landing gear extension:
ABNORMAL LANDING GEAR
EXTENSION Procedure ................................ ACCOMPLISH
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