Embraer 190 - Avionics Mau 1 A Failure; Avionics Mau 1 B Failure

AIRPLANE
FLIGHT
MANUAL
ABNORMAL
PROCEDURES
ANAC APPROVED 4-18
REVISION 7 code 01 Page 5
AFM
-
1912
AVIONICS MAU 1A FAILURE
Exit and avoid icing conditions.
Relevant Inoperative Items:
− Multi Function Spoilers L5
and R5.
− MCDU 1 (except circuit
breakers page).
− Outboard Brakes. − Pitch Trim Indication.
− Weather Radar. − Autopilot 1.
− Left Aileron Indication.
− Nosewheel Steering.
− ACARS.
− ADS 1.
For landin
g configuration, set slat/flap to full and set V
REF FULL
.
On ground steer the airplane using differential braking, apply brakes
normally and, 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 1.58.
FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS
UNFACTORED LANDING DISTANCE BY 1.65.
AVIONICS MAU 1B FAILURE
Relevant Inoperative Items:
− Multi Function Spoilers L5 and R5.
− Pitch Trim Indication.
− GPS 1.
For landin
g configuration, set slat/flap to full and set V
REF FULL
.
CAUTION: FOR THE EMBRAER 190, MULTIPLY THE FULL FLAPS
UNFACTORED LANDING DISTANCE BY 1.07.
FOR THE EMBRAER 195, MULTIPLY THE FULL FLAPS
UNFACTORED LANDING DISTANCE BY 1.18.