Embraer 190 - Loss of Hydraulic System 1 and 3; (Embraer 190 Models)

AIRPLANE
FLIGHT
MANUAL
ABNORMAL
PROCEDURES
ANAC APPROVED 4-01
REVISION 7 code 01 Page 25
AFM
-
1912
LOSS OF HYDRAULIC SYSTEM 1 AND 3
(EMBRAER 190 MODELS)
LAND AT THE NEAREST SUITABLE AIRPORT.
NOTE: - Expect lower roll rates and lower speedbrake efficiency.
- Do not accomplish the Spoiler Fault Procedure.
Relevant Inoperative Items:
− Rudder.
− Multi Function Spoilers L3, R3, L4 and R4.
− Ground Spoilers L2 and R2.
− Autopilot.
− Engine 1 Reverser.
− Outboard Brakes.
For landin
g configuration set slat/flap to 5 and set V
REF FULL
+ 10 KIAS.
CAUTION:
• AVOID LANDING WITH CROSSWIND COMPONENTS
ABOVE 10 KT.
• MULTIPLY THE FULL FLAPS UNFACTORED LANDING
DISTANCE BY 2.11.