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Embraer EMB145 - Page 494

Embraer EMB145
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ABNORMAL
PROCEDURES
AIRPLANE
OPERATIONS
MANUAL
1-03-48
Page
4
Code
03
REVISION 40
AOM-145/1114
CONTINUED FROM PREVIOUS PAGE
Approach and landing configuration:
Landing Gear...........................................................DOWN
Flaps ........................................................................45°
Airspeed...................................................................V
REF 45
CAUTION:
DO NOT OPEN THE SPEED BRAKE.
TO DETERMINE THE MINIMUM SUITABLE LANDING
DISTANCE, MULTIPLY THE UNFACTORED LANDING
DISTANCE FOR FLAPS 45° BY 1.53.
NOTE: - The following systems will be inoperative: Outboard Spoiler,
Inboard Brakes, RH Thrust Reverser, and
Emergency/Parking Brake.
- The Emergency/Parking Brake will be available only with the
accumulator charge.
HYDRAULIC SYSTEM OVERHEAT
EICAS CAUTION: HYD SYS 1 (2) OVHT
LIGHT: Master Caution
Associated Engine Hydraulic Pump.............................. SHUTOFF
Associated Electric Hydraulic Pump ............................. OFF
Airspeed ........................................................................ MAXIMUM
250 KIAS
For the remainder of flight, if required:
Affected Hydraulic system ....................................... 15 MINUTES OFF,
1 MINUTE ON
During approach and landing or when required:
Affected Hydraulic system ....................................... ON
After reaching taxi speed or when the system is no longer required:
Affected Hydraulic system ....................................... OFF
NOTE: To turn the hydraulic system on, first turn the electric pump to
AUTO. As soon as the system pressure is recovered, release
the engine pump shutoff button.

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