This quiz titled '2F051 Edit Code 6 Volume 4' assesses knowledge on the Kovatch-Volvo R-11 Refueler, covering aspects like storage tank capacity, tire maintenance, and safety mechanisms. It is designed for learners focusing on vehicle maintenance and mechanical engineering.
DEFUELl.
LOW-FLOW.
HIGH-FLOW.
SINGLE-POINT.
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60
65
70
80
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17166
17615
61517
15617
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Air pressure drops below 30 to 40 pounds per square inch (psi).
Transmission selector is in the neutral position.
Unit is in the AIR TRANSPORT mode.
Interaxle differential lock is activated.
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International 6-cylinder, liquid-cooled diesel engine.
International 6-cylinder, liquid-cooled mogas engine.
International 8-cylinder, liquid-cooled diesel engine.
International 8-cylinder, liquid-cooled mogas engine.
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60-foot long 2 ½-inch and 1 ½-inch hoses.
75-foot long 2 ½-inch and 1 ½-inch hoses.
60-foot long 3-inch and 1-inch hoses.
75-foot long 3-inch and 1-inch hoses.
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Sculcon.
Duocept® socket assembly.
Overfill Sensor (optic probes).
Multifunction loading rack controller.
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Stop fuel flow.
Stop the aircraft engines.
Notify the fire department.
Disconnect the fuel nozzle.
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400 to 500 foot-pounds (ft-lbs.).
300 to 400 ft-lbs.
200 to 300 ft-lbs.
100 to 200 ft-lbs.
30 seconds.
1 minute.
1 ½ minutes.
2 minutes.
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Vent valve.
Float level sensor.
Bottom loading interlock.
Emergency/bottom loading valve.
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AF Form 1233, Bulk Storage Summary.
AF Form 1235, Physical Inventory (Fuels/Missile Propellants).
DD Form 1896, DOD Fuel Identaplate.
DD Form 1898, Energy Sale Slip.
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Spotter behind the unit.
Prepositioned chock behind the unit.
Spotter and a prepositioned chock behind the unit.
Spotter in front of the unit, and a spotter and a prepositioned chock behind the unit.
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Neutral (N).
Drive (D).
Third (3).
Second (2).
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Not enter or exit the aircraft at any time.
Enter or exit the aircraft provided a jetway is used.
Enter the aircraft but cannot exit the aircraft at any time.
Not enter the aircraft but can exit the aircraft at any time.
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Assessing fueling operations.
Taking action to correct deficiencies.
Providing assistance for hydrant-servicing operations.
Coordinating and directing cryogenic-servicing operations.
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Unfiltered fuel from being dispensed to an aircraft.
Fuel from passing through the pump when the engine is idling.
Auxiliary throttle from operating when the PTO is in the vehicle drive position.
Auxiliary throttle from operating when the PTO is in the vehicle pump position.
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Crew chief.
Fuels operator.
Line expeditor.
Concurrent servicing supervisor.
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No action is required as this is a common occurrence.
Stop the operation and do not resume until the problem has been resolved.
Stop the operation temporarily, restart fuel flow, then re-attempt the fuel flow precheck.
Continue the operation and inform the concurrent servicing supervisor (CSS) of the situation.
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Hot refuel.
Rapid defuel.
Multisource refuel.
Concurrent servicing.
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Up
Inc
Low
Down
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1000
1200
1500
2000
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Float level sensor.
Bottom loading interlock.
Emergency valve operator.
Emergency/bottom loading valve.
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Six inches in height, five inches wide.
Six inches in height, four inches wide.
Four inches in height, two inches wide.
Four inches in height, three inches wide.
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10
25
35
50
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Differential pressure.
Nozzle pressure.
System outlet.
Pump pressure.
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25 degrees Celsius (°C).
32°C.
40 degrees Fahrenheit (°F).
45°F.
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Safety interlock override switch.
Interlock override indicator light.
Interlock engaged indicator light.
Power takeoff (PTO) control switch.
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Four.
Three.
Two.
One.
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AF Form 4427.
AF Form 1807.
AF Form 1800.
AFTO Form 244.
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OKAY TO PUMP.
PUMP ENGAGED.
SUMP TANK FULL.
THROTTLE READY.
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Oil servicing.
Liquid oxygen servicing.
Liquid nitrogen servicing.
Hydraulic fluid servicing.
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50
75
100
125
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Hot defueling.
Rapid defueling.
In-shelter refueling.
Concurrent servicing.
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Inspect the locking pins/lugs and seal for serviceability visually.
B. Check the strainer coupling quick-disconnect device.
Set the applicable tank refuel switches to open.
Perform the fuel preflow check.
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Reverse.
Neutral.
Drive.
Three.
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65
70
75
80
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450
600
750
1200
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100
250
450
600
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Observes the fuel equipment pressure gauges.
Maintains visual contact with the prepositioned fireguard.
Maintains intercom contact with the fuels equipment operator.
Ensures the aircrew maintains their hands out of the cockpit instrumentation area.
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Fuels manager.
Fuels distribution supervisor.
Fuels management flight chief.
Fuels operations superintendent.
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7
14
30
45
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30
60
90
120
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8
12
24
48
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Customer identification code.
Last four digits of the tail number.
Full tail number and the mission, design and series (MDS) of the aircraft.
Last four digits of the aircraft’s tail number and Department of Defense Activity Address Code (DODAAC).
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A fault in the automatic and continuous self-testing circuity.
A power take off system is activated inside the cab.
A wet sensor, tank is filled to maximum capacity.
A dry sensor, tank is not filled to capacity.
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System Safety Engineering Analysis.
Air Force Civil Engineer Support Agency Inspection.
Headquarters Air Force Materiel Command, Senior Executive Service Inspection.
Headquarters United States Air Force, Directorate of Logistics, Materiel Support Division Analysis.
C-5 Galaxy.
C-27 Spartan.
C-130 Hercules.
C-17 Globemaster III
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