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Flight Crew Operating Manual MASTER
CSP A-
013
FUEL SYSTEM Vol. 1 13-
50-
1
Refueling and Defueling REV 56, Jan 31/03
1. REFUELING AND DEFUELING
The refuel/defuelsystemiscontrolledbytheFuelSystemComputer(FSC)throughselection onarefuel/defuel controlpanel. Pressure refuelingand suction defueling oftheaircraft are accomplished using arefuel/defueladapterlocatedin the right wing,leadingedge, root fairing.
Gravity refuelingis carriedoutthroughfiller caps installed on the upperwing surface. The fuelquantity can bemonitored using magnetic levelindicators installedin thetanks. Water drain valves, installed at various low points, permittestingoffuelforcontamination and provide the means ofdraining any accumulated water.
Thegravityfillercapsarelocatedbelowthemaximum pressure refueling level. Never remove the gravity fillercapsifthewingtanksarefullorifthefuelquantity is unknown.
Flight Crew Operating Manual MASTER
CSP A-
013
Vol. 1 13-
50-
2
FUEL SYSTEM
REV56,Jan 31/03
Refueling and Defueling
Refuel/Defuel Adapter
Bayonet typepressure fuelingadapter. Remove protective capto connect refuel/defuelhose adapter.
NOTE
Right sideis shown. Left sideis opposite.
Gravity Filler Cap (3)
Lift latch andturn counterclockwise to unlock.
Right Wing Top View
TANK FUEL DRAIN VALVE (3)
Lift latch andturn counterclockwise to
PUSH TO
UNLOCK
remove plug. Insert gravity defueleradapter to start gravitydefueling.
Refuel/Defuel
<0017>
Control Panel
Refuel/Defuel Control Panel
WATER DRAIN VALVE (16)
Push and rotate water drain valve core withfuel sampler to drainfuelinto fuel sampler.
NOTE
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