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Embraer 190 - Avionics Mau 2 A Failure; Avionics Mau 2 B Failure

Embraer 190
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ABNORMAL
PROCEDURES
AIRPLANE
FLIGHT
MANUAL
4-18 ANAC APPROVED
Page 6 code 01 REVISION 7
AFM
-
1912
AVIONICS MAU 2A FAILURE
Relevant Inoperative Items:
Nosewheel Steering.
FMS 1.
On ground, steer the airplane using rudder and differential braking.
AVIONICS MAU 2B FAILURE
Relevant Inoperative Items:
Inboard Brakes. EGPWS.
Autopilot 1. ADS 2.
Right Side Weather Radar
Control.
IESS
– Localizer and Glide
Slope Indication.
MCDU 2 (except circuit
breakers page).
Mach Trim.
Transponder 2.
For landing configuration, set slat/flap to full and set V
REF FULL
.
On ground
apply brakes normally. If necessary, use the
emergency/parking brake.
CAUTION: • APPLY THE EMERGENCY/PARKING BRAKE
MONITORING THE EMERGENCY/PARKING BRAKE
LIGHT.
WHEN THE EMERGENCY/PARKING BRAKE LIGHT IS
ON, MAINTAIN STEADY PRESSURE SINCE THE ANTI-
SKID PROTECTION IS NOT AVAILABLE.
FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS
UNFACTORED LANDING DISTANCE BY 1.51.
FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS
UNFACTORED LANDING DISTANCE BY 1.58.

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