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Hydraulic reservoirs, valve positioning and pump operations are pictorially displayed. System temperatures, fluid quantities and pressures are represented digitally. Flow lines connect components and legends display system status.
HYDRAULIC SYNOPTIC PAGE
Reservoir HYDRAULIC SYSTEM #3
AC Motor Pump Status
Engine Driven Pump Status
RAT Deployed Hydraulic Fluid Temperature Readout
Hydraulic Fluid Quantity Readout
Firewall Shut-off Valve Position
Hydraulic Pressure Readout
GF1310_002
The synoptic page and hydraulic panel control switches are detailed later in this Chapter.
HYDRAULIC CONTROL PANEL
The hydraulic control panel is located on the overhead panel in the flight compartment. There are four switches which control electrically operated pumps for each system.
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
SYSTEMS OVERVIEW SCHEMATIC
RAT PUMP
LANDING GEAR, STEERING AND BRAKES
HEAT EXCHANGER
ACCUMULATOR SYSTEM 2 BRAKE GROUND SPOILER
ACCUMULATORS
SYSTEM 3 RAT (FORWARD)
SYSTEM 3 BRAKE (AFT)
AILERON
CENTRAL HYDRAULIC
SYSTEM COMPONENTS
FILTERS MULTI-FUNCTIONAL SPOILERS
RESERVOIR
RELIEF VALVE
REVERSER
PRESS/TEMP SENSING
RUDDER
ELEVATOR
LEGEND
System pressure 1 AC motor pump RAT hydraulic pump
System pressure 2
Engine driven pump
System pressure 3
GF1310_004
Volume 2 Flight Crew Operating Manual Rev 2A, Apr 11, 2005
HYDRAULIC SYSTEM 1 AND 2
Each system includes an EDP, reservoir, ACMP, manifolds with pressure, return and case drain filters, hydraulic shutoff valve, heat exchanger and ground servicing panel. Hydraulic overfill bottles for system 1 and 2 are provided and located near their system components.
Engine Driven Pump
EDP . Located on the accessory drive of each engine.
GF1310_005
The EDPs 1A and 2A are used as primary pumps and draw fluid from the reservoirs through hydraulic shut-off valves. Fluid is delivered to the applicable manifold, filtered and distributed to the airplane’s hydraulically-actuated components.
Aft Equipment Bay Components
RESERVOIR 1
RESERVOIR 2
DIRECT READING GAUGE
FILTER MANIFOLDS ACMP’S
Reservoir
GF1310_006a
System 1 and 2 reservoirs are located at the top of the aft equipment bay. Fluid quantity and temperature transducers are located on the reservoir and are indicated on the HYDRAULIC synoptic page.
Rev 2A, Apr 11, 2005 Flight Crew Operating Manual Volume 2
HYDRAULIC SYSTEM 1 AND 2 (CONT'D)
AC-Motor Pumps (ACMPs)
The back-up ACMPs 1B and 2B are normally operated in the AUTO mode and come on automatically during take-off, approach and landing or in support of a primary pump failure.
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