The 2A655 Volume 3 Unit Review 1-60 focuses on hydraulic systems in aircraft, assessing knowledge on hydraulic pumps, motors, and reservoir pressures. It is designed for individuals seeking to understand or reinforce their understanding of aircraft hydraulic mechanics.
Vent
Rupture
Overheat
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Brake pedals
The accumulator
Antiskid control box
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Mechanical
Elecrical
Trim
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Stopping the engines
Pulling the fire handles
Pulling the circuit breakers
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Fixed pivot
Fixed pivot
Nutating plate
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Change the foot values
The head should be rotated 180 degrees
Change the direction of fluid flow into the motor
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They deliver low pressure
They have an integral compenator
The case drain wil relieve high system pressure
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Tandem
Internal locking
Internal snubber
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Signal coil
Power relay
Limit switches
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A single hydraulic actuator
A single electric actuator
Two hydraulic actuators
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Microswitch
Thermal switch
Priority valve
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Capacity test
Static test
Drive shaft torque test
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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
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2 min
10 min
20 min
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Faulty bulb
Internal leakage in vavlve
Press to test frature of the bulb
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One quart
One-half quart
One gallon
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Forward loadmaster's control panel
Aft loadmaster's control panel
Co-pilots ADS panel
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10(+5/-0)
20(+10/-0)
40(+10/-0)
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Both the cylinder block and pistons rotate.
The universal link and cylinder block rotates.
The pistons move back and forth, and the cylinder block is stationary.
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The increase of fluid viscosity as the temperature is lowered
The difference between pressure entering the element and pressure leaving the element
The spring loaded magnetic indicator postin pop-up when contaminated
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Excessive gas pressure is being applied
The accumulator is not properly vented
The end cap is leaking
The piston is leaking
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Be 1800 lbs
Be 30 lbs with no back pressure
Be 300 lbs with no back pressure
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Seat all forur poppets
Seat both of the pressure poppets
Unseat one pressure poppet and one return
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Snubber
Accumulator
Engine driven pump
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Automatic brake actuator
Copilot's metering valve
Copilot's brake pedals
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5
25
50
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Proof pressure test
Internal leakage test
External leakage test
Piston seizure
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Back Pressure
Static Pressure
Emergency Pressure
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Elevator
Rudder
Spoiler
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Perform an operational check
Consult the appropriate fault isolation manual
Consult the appropriate General System manual
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Gland nuts
Spacer rings
Seal assembly
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Bypass
Relief
Shuttle
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Remove and replace the filters
Take the sample from the reservoir only
Open line connections to take the sample
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Pressurization system
Indication system
Nitrogen system
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Ensure proper operattion at all pressure and revolutions per minute settings
Ensure that fluid in the test stand is properly heated
Provide a check of leakage rate at the shaft seal
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Hydrualic roller assembly
Electriacally actuated downlocks
Hydraulically actuated downlocks
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Extend
Retract
Neutral
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Solenoid operated shutoff valve
Bypass valve
Servo ram
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Fixed
Variable
Check valve
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In both directions
In one direction
Only when there is macimum load on the actuator
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Relief
Flow control
Pressure reducer
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Suction shutoff valve
No. 3 engine relay
Pressure shutoff valve
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Magnet
Brass dowel
Wooden dowel
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Toggle latches only
Open side of the slipway door actuators
Open and close side of the door actuators
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50 psig
100 psig
1500 psig
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Deformation/ failure
Internal leakage
Piston leakage
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Dragging brakes
Shock strut conical bearings binding
Metering valve malfunction
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Pressure
Supply
Return
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Quiz Review Timeline (Updated): Mar 21, 2023 +
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