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

ABNORMAL
PROCEDURES
AIRPLANE
F
LIGHT
MANUAL
4-01 ANAC APPROVED
Page 18 code 01 REVISION 15
Copyright © by Embraer. Refer to cover page for details.
AFM
-
1385
LOSS OF HYDRAULIC SYSTEM 2
NOTE: - Expect lower roll rates and lower speedbrake efficiency.
- Do not accomplish the Spoiler Fault Procedure.
- Do not command engine 2 reverser.
Plan a long final approach.
For landing configuration, set the landing gear lever to down, pull the
alternate gear extension lever, set slat/flap to full and set V
REF FULL
.
CAUTION: MULTIPLY THE FULL FLAPS UNFACTORED LANDING
DISTANCE BY 1.80.
If a go around is required, maintain landing gear down.
LOSS OF HYDRAULIC SYSTEM 1 AND 2
LAND AT THE NEAREST SUITABLE AIRPORT.
N
OTE: - 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.
- Braking action starts after Emerg/Prkg Brake light
illumination. Apply the brake carefully since antiskid
protection is not available.
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:
• MULTIPLY THE FULL FLAPS UNFACTORED LANDING
DISTANCE BY 2.70.
• AVOID LANDING WITH CROSSWIND COMPONENT
GREATER THAN 10 KT.
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
altitude is reached.