F16 Fuel And Engine Systems

Front 1

the internal fuel storage system consists of how many tanks

Back 1

seven

Front 2

each of the external wing tanks holds how many gallons

Back 2

370 gallons

Front 3

how many fuselage fuel tank drain valves are on the jet

Back 3

seven

Front 4

which fuel tanks equally provide fuel to the engine on demand

Back 4

fwd and aft resevoirs

Front 5

into which fuel tanks does the external centerline tranfer fuel

Back 5

left and right internal wing

Front 6

what provides the refuel receptacle with an emergency disconnect feature during aerial refueling

Back 6

pressure relief valve

Front 7

the fuel scavenge pumps move the residul fuel to the

Back 7

fwd resevoir

Front 8

the fuel scavenge pumps receibe power from

Back 8

fuel bled off the boost pumps

Front 9

the fuel flow proportioner is powered by what hyd system

Back 9

hyd. system a

Front 10

ath what pressure does the fuel flow proportioner operate

Back 10

19 psi

Front 11

a thermal valve in the fuel system heat exchanger outlet prevents the fuel temp from exceeding

Back 11

200 degrees f

Front 12

the vent and pressurization valve for the external fuel tanks is located on the inside of the

Back 12

vent tank

Front 13

thich fuel system valve provides a redundant means of allowing air into the vent tank thus guarding against instances of negative pressure within the fuel tanks

Back 13

negative pressure relief

Front 14

the ground air service connector for the fuel tank pressurizaation is located

Back 14

in the right mlg wheel well

Front 15

what provides a redundant means of relieving excess pressure should the fuel system internal vent and pressurization valve fail

Back 15

remote sensing relief valve

Front 16

which switch provides a way of testing the fuel temp subsystem

Back 16

fuel hot test switch on the ground test panel

Front 17

the dual pointer markers on the fuel quantity indicator are labeled

Back 17

fr and al

Front 18

flammable vapor air mixtures for jp8 are possible at all temps above

Back 18

100 degree f

Front 19

areas that are normally adjacent to fuel tanks or fuel lines and have no means of air circulation even though they are drained are considered

Back 19

internal nonvented areas

Front 20

which fuel leak conditions do not require immediate repair

Back 20

condistion 1 and 2

Front 21

the f100 pw 220 engine compressor contains

Back 21

three stages of low pressure compression and ten stages of high pressure compression

Front 22

one benefit of the modular construction engine is the ease of removal and replacement of

Back 22

faulty engine sections

Front 23

the f100 pw 220 deigital electronic engine control fails, engine control transfers to

Back 23

secondary mode of operation

Front 24

after intitial ignition the main ignition spark on the f100 pw 220 engine is suppressed by

Back 24

combustion chamber pressure

Front 25

what is the position of the 110 ge 100 anti ice valve when electrical power is removed

Back 25

open

Front 26

with an 110 ge 100 engine which condition causes the engine warning light to illuminate

Back 26

engine rpms of 59 percent

Front 27

the capacity of oil tank with the 110 ge 100 is

Back 27

three gallons