TM 1-1520-240-102-15-132-15-7. Gravity Refueling. Perform the followingsteps:a.Be sure the helicopter is at least 50 feet from anyhangar or structure.b.Be sure the fueling vehicle is at least 10 feet fromthe helicopter.c.Electrically ground the helicopter as follows:(1)Connect one end of an approved groundcable to the aft landing gear eyebolt or to one of the jackson the side of the fuselage. Grounding jacks are locatedat sta. 115 on the RH side and sta. 530 on the LH side inthe fuselage skin. Connect the other end to a groundingrod or ramp ground point. Make sure the cable has nobroken strands and the clip are securely attached to thecable and ground points.(2)Make sure the fueling unit is grounded to thesame ground rod or ground point as the helicopter.(3)Before opening the filler cap, ground thenozzle to the ground jack directly above the fuel tankfiller.d.When the fuel is at the desired level, remove thenozzle. Secure the filler cap. Then, disconnect the nozzleground wire.e.Remove the ground connection. If the helicopteris to remain parked, do not disconnect the helicopterground.2-15-8. ERFS Refueling and Fuel Transfer.ERFS Refueling and Fuel transfer will be in accordancewith existing Air Worthiness Release (AWR).2-15-9. ERFS II Refueling.Refueling the ERFS II tanks is performed by either singlepoint pressure refueling or gravity refueling.WARNINGThe manually operated fuel/defuel ventvalve on each tank must be placed in theclosed position following pressure refue-ling. Failure to do so could permit signifi-cant fuel leakage in the event of a crashand the vent self–sealing breakaway valvefails to actuate.CAUTIONIf the fuel/vent valve is not opened, thetank cannot be pressure refueled.a.Single Point Pressure Refueling. The ERFS IItanks are single point pressure refuled from a connectionat the motorized gate valve. The motorized gate valvemust be open to pressure refuel and is controlled by therefuel valve switch on the ERFS II fuel control panellocated on the forward most ERFS II tank installed. Thefuel transfer hose is connected to the forward intercon-necting ERFS II fuel manifold. Fuel from the transferhose passes through the breakaway valve and themanual fuel/defuel valve to the lower fuel/shutoff valve inthe tank bottom.CAUTIONThe operator must exercise caution toavoid ERFS II tank overflow during gravityrefueling. There is no automatic fuel flowshutoff.b.Gravity Refueling. If pressure refueling of ERFSII tanks is not performed or prevented, each tank can alsobe gravity filled through the gravity filler opening on thetop of each tank. To gravity fill, the crashworthy filler capis removed and external fuel source nozzle is insertedand the tank is filled. Low pressure flow rates must bemaintained as venting or vapors bypass the filler openingand the fuel/defuel vent valve is closed during this opera-tion. Because fuel is not entering the tank through thefuel/defuel line, the high level shutoff valve has no effectstopping the fuel flow into the tank.2-15-10. Single Point Pressure Refueling.a.Electrical ground — Connect electrical groundfrom refueling aircraft. Check that the ground wire fromeach ERFS II tank is connected to an aircraft groundreceptacle.b.Fuel hose from refueling source — Connect toaircraft single-point pressure refueling connection.c.Single-Point Pressure Refueling HoseAssembly - Unisex valve at the ERFS II tank — OPEN.d.Manual FUEL/DEFUEL VALVE at each tank as-sembly — OPEN.e.REFUEL STA switch located on the overheadFUEL CONTR Panel — ON.f.REFUEL VALVE switch on the ERFS II Fuel Con-trol Panel OPEN. IN TRANSIT light will briefly illuminateg.Refuel the ERFS II tanks. Fuel flow will automati-cally stop when tanks are full.h.FUEL QUANTITY switch — Set to 1, 2, 3, andTOTAL to confirm tanks and system contain desired fuelquantities.i.REFUEL VALVE switch. — CLOSE. IN TRANSITlight will briefly illuminate.
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