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Embraer 190 - Loss of Hydraulic System 1 and 2; (Embraer 195 Models)

Embraer 190
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ABNORMAL
PROCEDURES
AIRPLANE
FLIGHT
MANUAL
4-01 ANAC APPROVED
Page 24 code 01 REVISION 7
AFM
-
1912
LOSS OF HYDRAULIC SYSTEM 1 AND 2
(EMBRAER 195 MODELS)
LAND AT THE NEAREST SUITABLE AIRPORT.
NOTE: - Expect lower roll and pitch rates.
- Do not accomplish the Elevator Fault and the Spoiler Fault
Procedures.
- Apply the Emergency/Parking Brake to stop the airplane
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.
Relevant Inoperative Items:
L.H. Elevator.
Multi Function Spoilers L3, R3, L4, R4, L5 and R5.
Ground Spoilers L1, R1, L2 and R2.
Speedbrake.
Autopilot.
Nosewheel Steering.
Engine 1 and Engine 2 Reversers.
Outboard and Inboard Brakes.
Landing Gear retraction and normal extension.
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
+ 15 KIAS.
CAUTION:
AVOID LANDING WITH CROSSWIND COMPONENTS
ABOVE 10 KT.
MULTIPLY THE FULL FLAPS UNFACTORED LANDING
DISTANCE BY 2.76.
If a go around is required, maintain landing gear down, slat/flap 5 and
V
REF FULL
+ 15 KIAS until the acceleration altitude is reached.

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