Embraer 175 - LOSS OF HYDRAULIC SYSTEM 1 AND 3; LOSS OF HYDRAULIC SYSTEM 2 AND 3

AIRPLANE
FLIGHT
MANUAL
ABNORMAL
PROCEDURES
ANAC APPROVED 4-01
REVISION 15 code 01 Page 19
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1385
LOSS OF HYDRAULIC SYSTEM 1 AND 3
LAND AT THE NEAREST SUITABLE AIRPORT.
NOTE: - Expect lower roll rates and lower speedbrake efficiency.
- Do not accomplish the Spoiler Fault Procedure.
- Do not command engine 1 reverser.
For landing 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 2.30.
LOSS OF HYDRAULIC SYSTEM 2 AND 3
LAND AT THE NEAREST SUITABLE AIRPORT.
N
OTE: - Expect lower roll and pitch rates and lower speedbrake
efficiency.
- Do not accomplish the Elevator Fault and the Spoiler Fault
Procedures.
- Do not command engine 2 reverser.
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 2.20.
If a go around is required, maintain landing gear down, set
slat/flap to 4, and maintain V
REF FULL
+ 10 KIAS until the acceleration
a
ltitude is reached.