Embraer 190 - Loss of Hydraulic System 2 and 3; (Embraer 190 Models)

AIRPLANE
FLIGHT
MANUAL
ABNORMAL
PROCEDURES
ANAC APPROVED 4-01
REVISION 7 code 01 Page 27
AFM
-
1912
LOSS OF HYDRAULIC SYSTEM 2 AND 3
(EMBRAER 190 MODELS)
LAND AT THE NEAREST SUITABLE AIRPORT.
NOTE: - Expect lower roll and pitch rates and lower speedbrake
efficiency.
- Do not accomplish the Elevator Fault and the Spoiler Fault
Procedures.
Relevant Inoperative Items:
− R.H. Elevator.
− Ailerons.
− Multi Function Spoilers L5 and R5.
− Ground Spoilers L1 and R1.
− Engine 2 Reverser.
− Inboard Brakes.
− Landing Gear retraction and normal extension.
− Nosewheel Steering.
Plan a long
final approach.
For landing configuration, set landing gear down, pull the alternate
gear extension lever, 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 1.96.
If a go around is required, maintain landing gear down, slat/flap 5 and
V
REF FULL
+ 10 KIAS until the acceleration altitude is reached.