Embraer EMB145 Operation Manual page 492

ABNORMAL
PROCEDURES
Approach and landing configuration:
Landing Gear ...................................................... DOWN
Flaps ................................................................... 22°
Airspeed.............................................................. V
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,
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
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
Page
2
1-03-48
AIRPLANE
OPERATIONS
MANUAL
CONTINUED FROM PREVIOUS PAGE
AIL SYS 1 INOP
CONTINUES ON NEXT PAGE
Code
03
+
REF 45
30 KIAS
250 KIAS
REVISION 36