Explore key hydraulic principles in the CDC Z2A655 Hydraulic Journeyman Vol 3. This quiz assesses knowledge on hydraulic reservoirs, pumps, and manifolds, essential for emergency preparedness and system efficiency in mechanical engineering contexts.
RETURN LINES CAN JOIN TOGETHER
PRESSURE LINES CAN JOIN TOGETHER
COMMON FLUID LINES CAN COME TOGETHER
THE HYDRAULIC TEST STAND CAN BE CONNECTED
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VENT
RUPTURE
OVERHEAT
CREATE A VACUUM
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RIGHT
WRONG
WRONG
WRONG
ELEMENT SCREEN
THUMB SCREEN
FINGER SCREEN
FILTER SCREEN
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OPEN
CLOSED
BYPASS
RUNAROUND
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THEY DELIVER LOW PRESSURE
THE CASE DRAIN WILL RELIEVE HIGH SYSTEM PRESSURE
THEY HAVE AN INTEGRAL FLOW CONTROL VALVE (COMPENSATOR)
THERE IS NO ANGLE BETWEEEN THE DRIVE SHAFT AND CYLINDER BLOCK
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1800 POUNDS
600 POUNDS
300 POUNDS
30 POUNDS
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PULLING THE T-HANDLE
STOPPING THE ENGINES
PULLING THE CIRCUIT BREAKERS
STOPPING THE SUCTION BOOST PUMP
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RIGHT
WRONG
WRONG
WRONG
PLACE A WRITE-UP IN THE AIRCRAFT FORMS UNDER A READ DASH
PLACE A WRITE-UP IN THE AIRCRAFT FORMS UNDER A RED X
TELL YOUR SUPERVISOR
TELL YOUR FLIGHT CHIEF
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MAKE SURE THAT THE ARROW MARKED ON THE VALVE HOUSING IS POINTING IN THE OPPOSITE DIRECTION OF FLUID-FLOW
MAKE SURE THAT THE ARROW MARKED ON THE VALVE HOUSING IS POINTING IN THE DIRECTION OF FREE-FLOW
ADJUST THE SPRING TENSION SO THE VALVE WILL OPEN AT THE SPECIFIED PRESSURE
ADJUST THE CHECK VALVE SO THE FLUID FLOWS IN ONE DIRECTION ONLY
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CO-PILOT'S AIR DELIVERY SYSTEM (ADS) PANEL
FORWARD LOAD MASTER'S CONTROL PANEL
AFT LOADMASTER'S CONTROL PANEL
PILOT'S ADS PANEL
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MICROSWITCH
PRIORITY VALVE
THERMAL SWITCH
BALANCED RELIEF VALVE
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SO ONLY ONE SYSTEM CAN OPERATE AT A TIME
TO ENSURE THAT SYSTEM ACTUATORS EXTEND AND RETRACT AT THE SAME RATE
SO ONE OPERATION IS PERFORMED BEFORE THE REST OF THE SYSTEM CAN OPERATE
TO PREVENT THE NORMAL AND EMERGENCY SYSTEM FROM OPERATING AT THE SAME TIME
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GLAND NUTS
SPACER RINGS
SEAL ASSEMBLY
CONNECTING TUBE
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SNUBBER
ACCUMULATOR
ENGINE-DRIVEN PUMP
PRESSURE TRANSMITTER
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REMOVE AND REPLACE THE FILTERS
BENCH CHECK THE ENGINE-DRIVEN PUMP
TAKE THE SAMPLE FROM THE SERVOIR ONLY
TAKE THE SAMPLE FROM THE RESERVOIR AND VARIOUS OTHER LOCATIONS IN THE SYSTEM
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MATED PARTS
NONREPARABLE
DIFFICULT TO DISASSEMBLE
SERIALLY CONTROLLED PARTS
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ONE STROKE AND FORCED OUT ON ONE STROKE
BOTH STROKES AND FORCED OUT ON ONE STROKE
ONE STROKE AND FORCED OUT ON BOTH STROKES
BOTH STROKES AND FORCED OUT ON BOTH STROKES
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INCREASE OF FLUID VISCOSITY AS THE TEMPERATURE IS LOWERED
SPRING-LOADED MEGNETIC INDICATOR PISTON POP-UP WHEN CONTAMINATED
COLLECTION OF CONTAMINATED PARTICLES ON THE OUTSIDE OF THE FILTER ELEMENT
DIFFERENCE BETWEEEN PRESSURE ENTERING THE ELEMENT AND PRESSURE LEAVING THE ELEMENT
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RETURN
SUPPLY
PRESSURE
CASE DRAIN
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MAGNET
DRIFT PUNCH
WOODEN DOWEL
NEEDLE-NOSE PLIERS
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PLUNGER
SPRING
SPOOL
SEAT
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MECHANICAL
HYDRAULIC
ELETRICAL
TRIM
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ELEVATOR
RUDDER
SPOILER
FLAP
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BOMB DOORS WILL OPEN AS NORMAL
DAMAGE TO THE AIRCRAFT COULD OCCUR
THE RIGHT BODY BOMB DOOR RELIEF VALVE WILL COMPENSATE
THE DUAL SHUTTLE VALVE WILL PORT THE TRAPPED PRESSURE BACK TO THE RETURN SIDE OF THE DOOR RELIEF VALVE
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BRAKE PEDALS
THE ACCUMULATOR
ANTISKID CONTROL BOX
BRAKE METERING VALVE
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PROTECT THE PUMP
RESERVE FLUID FOR THE POWER PUMP
SUPPLY THE PUMP DURING INVERTED FLIGHT
RESERVE FLUID FOR THE EMERGENCY PUMP
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INTERNAL LEAKAGE IN VALVE
ELETRICAL POWER AT THE PUMP
LOW-PRESSURE WARNING SWITCH
PRESS-TO-TEST FEATURE OF THE WARNING LIGHT
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NONE
1 QUART
1/2 QUART
1 GALLON
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AN EXTERNAL LEAKAGE TEST
AN INTERNAL LEAKAGE TEST
A PROOF PRESSURE TEST
A PISTON SEIZURE TEST
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A LACK OF PROPER ACCUMULATOR VENTING
EXCESSIVE GAS PRESSURE IS BEING APPLIED
INTERNAL LEAKING OF THE ACCUMULATOR PISTON
INTERNAL LEAKING OF THE ACCUUMULATOR END CAP
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RELIEF
SHUTTLE
BYPASS
CONTROL
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CHECK THE CONDITION OF THE RATIO CHANGER CONNECTING LINK
CONSULT THE APPROPRIATE GENERAL SYSTEM (GS) MANUAL
CONSULT THE APPROPRIATE FAULT ISOLATION (FI) MANUAL
PERFORM AN OPERATIONAL CHECK
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LATCH ACTUATOR
PRESSURE SWITCH
DUAL SHUTTLE VALVE
DOOR CONTROL VALVE
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AUTOMATICALLY BY ELETRICAL SEQUENCING
MANUALLY BY MECHANICAL SEQUENCING
AUTOMATICALLY BY MICROSWITCHES
MANUALLY BY OPERATOR
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FIXED
MANUAL
VARIABLE
CHECK VALVE
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HYDRAULIC ROLLER ASSEMBLIES
ELETRICALLY ACTUATED DOWNLOCKS
HYDRAULICALLY ACTUATED DOWNLOCKS
MECHANICALLY ACTUATED DOWNLOCKS
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PRESSURIZATION SYSTEM
INDICATION SYSTEM
NITROGEN SYSTEM
SUCTION SYSTEM
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PRESSURE COMPENSATOR IS NOT WORKING PROPERLY
METERING VALVE FILTER HAS BECOME CLOGGED
STEERING CENTERING MECHANISM IS BROKEN
NOSEWHEEL STEERING ACTUARTOR IS LEAKING
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HYDRAULICALLY-OPERATED
MANUALLY-OPERATED
SOLENOID-OPERATED
MOTOR OPERATED
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FLIGHT
NEUTRAL
FREEWHEEL
RAISE/LOWER
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SIGNAL AMPLIFIER CIRCUIT BREAKER
CORRODED INDUCTION COIL
FUEL DUMP SWITCH
OVERRIDE SWITCH
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IN BOTH DIRECTIONS
IN ONE DIRECTION ONLY
ONLY WHEN THERE IS NO LOAD ON THE ACTUATOR
ONLY WHEN THERE IS MAXIMUM LOAD ON THE ACTUATOR
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FREE FLOATING PISTON SHIFTS POSITION
VARIABLE ORIFICE CHANGES IT'S OPENING
CHECK VALVE OPENS ON THE SIDE HAVING LESS PRESSURE
CHECK VALVE OPENS ON THE SIDE HAVING GREATER PRESSURE
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SIGNAL COIL
POWER RELAY
LIMIT SWITCHES
OVERRIDE SWITCH
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SELECTOR VALVE HAS FOUR PARTS
SELECTOR VALVE IS MORE COMPLEX
SERVO VALVE WILL CONTROL FLUID FLOW
SERVO VALVE IS ELETRICALLY OPERATED
50 PSIG
100 PSIG
1500 PSIG
3000 PSIG
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