Embraer EMB145 - Page 493

AIRPLANE
OPERATIONS
MANUAL
ABNORMAL
PROCEDURES
REVISION 40
1-03-48
Page
3
Code
03
AOM-145/1114
CONTINUED FROM PREVIOUS PAGE
Do not actuate left Thrust Reverser.
Use rudder and differential braking technique for directional control
on ground.
Approach and landing configuration:
Landing Gear........................................................... DOWN
Flaps........................................................................ 45°
Airspeed .................................................................. V
REF 45
CAUTION:
TO DETERMINE THE MINIMUM SUITABLE LANDING
DISTANCE, MULTIPLY THE UNFACTORED LANDING
DISTANCE FOR FLAPS 45° BY 1.60.
NOTE: The following systems will be inoperative: Inboard Spoiler,
Outboard Brakes, LH Thrust Reverser, Landing Gear
Extension, Steering and Nose Landing Gear Doors
Retraction.
HYDRAULIC SYSTEM 2 FAILURE
EICAS CAUTION: HYD SYS 2 FAIL, RUDDER SYS 2 INOP, AIL SYS
2 INOP
EICAS ADVISORY: E2 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 2 .................................. ON
If hydraulic system fluid quantity is in amber range:
Electric Hydraulic Pump 2 .................................. OFF
If hydraulic power is not recovered:
Airspeed................................................................... MAXIMUM
250 KIAS
Electric Hydraulic Pump 2 ....................................... OFF
Do not actuate right Thrust Reverser.
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