This quiz focuses on the R-14 ATHRS, covering its purpose, fuel compatibility, operational flow rates, and safety requirements.
Jet fuel and gasoline.
Diesel and jet fuel.
Diesel and gasoline.
Diesel, jet fuel, and gasoline.
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10 ft.
20 ft.
50 ft.
100 ft.
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Never.
After initial start up.
Prior to air shipment.
Any time the system has been purged of fuel.
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ON and OFF.
ON and IDLE.
OFF and RUN.
RUN and IDLE.
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ABFDS.
Ocean tanker.
Aircraft systems.
The same source of supply used by the host airfield.
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Disconnect all hose assemblies.
Drain all the fuel from the piping.
Remove the filter separator elements.
Install dust plugs and caps on all fittings and hoses.
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3 in.
5 in.
6 ½ in.
7 ½ in.
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Stem.
Hose.
Valve.
Coupler.
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None.
Flow control.
Bi-directional.
Positive displacement.
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Two.
Three.
Four.
Six.
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Epoxy coated.
Single ply nylon.
Double ply Kevlar.
Rubber impregnated.
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Bronze disc.
Adhesive label.
Wooden placard.
Round aluminum disc.
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1,000 feet.
1,500 feet.
3,000 feet.
4,500 feet.
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Transferring large quantities of fuel.
Blending multiple fuel additives at different ratios.
Servicing aircraft where permanent systems are not available.
Servicing small aircraft and transferring small quantities of fuel.
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Thoroughly clean the unit.
Drain all fuel from the piping.
Disconnect and drain all hose assemblies.
Place the unit in the low mobility position.
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Sump tank.
Control valves.
Micronic filter.
Surge suppressors.
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A reading of 16 pounds per square inch, differential (psid) on the differential pressure (DP) gauge.
A reading of 22 psid on the DP gauge.
Elements that have been in use for 36 months
Filter separator vessel performance is questionable.
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3,000 gal.
6,000 gal.
9,000 gal.
30,000 gal.
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300 gpm.
350 gpm.
600 gpm.
650 gpm.
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JP-4.
JP-5.
JP-8.
JPTS.
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6
12
18
24
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ON.
OFF.
OFFLOAD.
NO DEADMAN.
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Transfer.
Relocation
Deployment.
Reassignment.
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15° F to 135° F.
25°F to 145° F.
40°F to 160° F.
50° F to 170° F.
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1 minute.
2 minutes.
4 minutes.
5 minutes.
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5.
10.
15.
20.
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Idle.
Half speed.
Two-thirds speed.
Full speed.
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162 ft.
173 ft.
186 ft.
190 ft.
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Using organization.
Accountable officer.
Home unit LRS customer service element.
Expeditionary LRS at the forward location.
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Two.
Three.
Four.
Five.
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Overwing nozzle.
D-1 single point nozzle.
D-2 single point nozzle.
Closed circuit refueling nozzle.
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JP-5.
Jet A.
Jet A-1.
Jet B.
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100,000.
200,000.
250,000.
500,000.
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Numbered Air Force.
MAJCOM.
Joint petroleum office.
DESC.
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Safety.
Feasibility.
Force protection.
Proximity of aircraft servicing operations.
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2°.
3°.
4°.
5°.
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45 pounds per square inch (psi).
75 psi.
90 psi.
150 psi.
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300 gpm.
350 gpm.
450 gpm.
600 gpm.
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35 psi.
40 psi.
50 psi.
55 psi.
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1
2
3
4
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1,550 rpm.
1,850 rpm.
1,950 rpm.
2,250 rpm.
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100 gpm.
200 gpm.
300 gpm.
600 gpm.
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10 to 15 psig.
15 to 25 psig.
25 to 30 psig.
30 to 40 psig.
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Battery charging.
Battery charge low.
Battery disconnected.
Battery at middle capacity.
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Site location.
Asset security.
Force protection.
Geographical dispersion.
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Required tankage.
Resupply method.
Product requirements.
Sufficient product availability.
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AF Form 1807.
AFTO Form 39.
AFTO Form 95.
A locally developed form.
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3
6
15
30
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