Study Guide: Hydraulics Flashcards
757: The power transfer unit (PTU) is automatically activated:
a) If the right engine fails or the right engine-driven pump pressure is low
b) If the left engine fails or the left engine-driven pump pressure is low
c) If the associated hydraulic system pressure drops below a preset value
d) When a dual engine failure occurs in flight
If the left engine fails or the left engine-driven pump pressure is low
757: The hydraulic motor generator (HMG) is automatically powered by the ___ whenever both main AC busses become unpowered in flight.
a) The left engine hydraulic pump or the PTU, if operating
b) The right engine hydraulic pump or the PTU, if operating
c) The center engine hydraulic pump or the PTU, if operating
d) The center engine hydraulic pump or the ADP, if operating
The left engine hydraulic pump or the PTU, if operating
767: The hydraulic motor generator (HMG) is automatically powered by the ___ when electrical power is lost from both main AC busses.
a) The center hydraulic system
b) The right hydraulic system
c) The left engine hydraulic pump or the PTU, if operating
d) The left hydraulic system
The center hydraulic system
757/767: When deployed, the RAT drives a hydraulic pump that supplies adequate pressure for flight controls down to an airspeed of approximately ______.
a) 80 knots
b) 100 knots
c) 120 knots
d) 130 knots
130 knots
757: The center hydraulic system reservoir contains a standpipe to reserve hydraulic fluid for the ____ in the event of a center system hydraulic leak.
a) Reserve brakes
b) Power transfer unit (PTU)
c) Ram air turbine (RAT)
d) Reserve brakes and steering system
Ram air turbine (RAT)
757: To prevent electrical overloads, the No. 2 electric pump is inhibited when only one generator (APU or engine) or only external power is available and:
a) Left and right electric pump switches are on
b) Both engine-driven pump switches are on
c) Both center hydraulic electric pump switches are on
d) The right electric pump switch is on
Both center hydraulic electric pump switches are on
757/767: According to the graphic, what is the status of the ram air turbine (RAT)?
a) The RAT is not stowed and locked, and is not producing adequate hydraulic pressure
b) The RAT is not stowed and locked, and is using standpipe fluid
c) The RAT is armed
d) The RAT is not stowed and locked, and is producing hydraulic pressure
The RAT is not stowed and locked, and is producing hydraulic pressure
757: External power is the sole source of electrical power. The center No. 2 electric hydraulic primary pump PRESS light is illuminated because:
a) The pump is inhibited when the associated N3 is below 50%
b) The pump only operates when associated system pressure is low
c) The pump has failed
d) In order to prevent electrical overloads, the pump is inhibited
In order to prevent electrical overloads, the pump is inhibited
757/767: The hydraulic quantity for each hydraulic system is displayed:
a) On the EICAS control panel
b) On the hydraulic control panel
c) On the standby engine indicator (SEI)
d) On the EICAS STATUS display
On the EICAS status display
757: According to the graphic, the RSVR light is illuminated. This indicates that:
a) Reservoir quantity is low (below 50%) or reservoir air pressure is high
b) Reservoir quantity is low (below 75%) or reservoir air pressure is high
c) Reservoir quantity is low (below 75%) or reservoir air pressure is low
d) Reservoir quantity is low (below 50%) or reservoir air pressure is low
Reservoir quantity is low (below 50%) or reservoir air pressure is low
757: According to the graphic, the EICAS POWER XFER UNIT status message is displayed. What is the status of the power transfer unit (PTU)?
a) The PTU has been activated and is operating properly
b) The PTU has been activated
c) The PTU switch on the auxiliary panel has been placed to the ON position while airborne
d) The PTU is not operating properly
The PTU is not operating properly
757: Trailing edge flaps and leading edge slats are hydraulically operated by drive units normally powered by the ___ hydraulic system(s).
a) Right
b) Left
c) Center
d) Left, center and right
Left
757/767: Yaw control is provided by a single rudder which receives hydraulic power from the ____ hydraulic system(s).
a) Right and center only
b) Left, center, and right
c) Left and right only
d) Left only
Left, center, and right
757: According to the graphic, when the RESERVE BRAKES switch is activated, fluid trapped below a standpipe is made available to the _________ system electric hydraulic pump.
a) Left
b) Right
c) Center No. 1
d) Center No. 2
Right
757: When activated, the power transfer unit (PTU) supplements the left hydraulic system electric motor-driven pump to operate the following:
a) Flaps and slats, landing gear, nose wheel steering, HMG
b) Flaps and slats, landing gear, nose wheel steering
c) Flaps and slats, landing gear, nose wheel steering, reserve brakes
d) Landing gear, nose wheel steering, HMG
Flaps and slats,
landing gear,
nose wheel steering,
HMG