WARNING: DO NOT REFUEL MORE THAN THE MAXIMUM PERMITTED RATE OF 155 U.S. GALLON (580 LITERS) PER MINUTE FOR EACH TANK. THIS WILL REDUCE STATIC CHARGE IN THE FUEL TANK.
(5)
Monitor the fuel quantity.
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WARNING: DO NOT OVERFILL THE TANK. THERE IS NO AUTOMATIC SHUTOFF CONTROL FOR OVERWING REFUELING.
D. Stop the Refuel Operation
(1)
When you have the necessary fuel quantity, stop the refuel operation.
(2)
Release the deadman switch to stop the fuel flow.
(3)
Disconnect the refuel nozzle from the airplane.
(4)
Install the overwing fill cap.
(5)
Remove the overwing refuel nozzle bonding cable.
(6)
Remove all equipment used for the overwing refuel operation.
(7)
Transfer fuel the center tank or auxiliary tank (if installed) as necessary
(AMM 28-23-0/301).
(8)
Make sure the onboard fuel load is in a valid pre-flight fuel distribution.
(9)
Record the actual fuel quantities from the fuel quantity indicators.
(10)
If the fuel quantity indicators are not available, record the actual fuel quantities from the fuel measuring sticks.
(11)
Do the discrepancy check and make sure it is within limits.
(12)
Complete the Fuel Sheet.
(13)
Complete the Delivery Receipt.
(14)
Give a copy of the forms to the airline representative or flight crew.
(15)
Make sure all the P15 switches are in the CLOSED position (if necessary).
E. Put the Airplane Back to Its Usual Condition
(1)
Close and latch the fueling station access door (if opened).
(2)
Do these steps in this sequence to remove the bonding/grounding cables
(AMM 20-40-11/201).
(a)
Disconnect the bonding cable from the airplane to the fuel source.
(b)
Disconnect the grounding cable from the earth ground to the fuel source.
(c)
Disconnect the grounding cable from the airplane to the earth ground.
(3)
Do the operator supplied procedure to remove the fuel vehicle.
(4)
Do this task to remove the lock from the extended leading edge flaps and slats: Leading Edge Flap and Slat Lock Application (AMM 27-81-0/201).
WARNING: DO THE PROCEDURE IN AMM 27-81-0/201 TO REMOVE THE LOCKS ON ALL EXTENDED LEADING EDGE FLAPS AND SLATS. THE FLAPS AND SLATS MOVE QUICKLY AND CAN CAUSE INJURY TO PERSONS OR DAMAGE TO EQUIPMENT.
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N96688
500 Overwing Fill Ports
May 01/03 Figure 301 12-11-03
Page 305
BOEING PROPRIETARY - Copyright . - Unpublished Work - See title page for details.
ALTERNATE REFUELING PROCEDURES - SERVICING
1. General
A. This procedure contains these tasks:
(1)
Refuel Operation - Inoperative Fueling Quantity Indicator
(2)
Refuel Operation -Early Shutoff (Airplanes with a VTO unit)
(3)
Refuel Operation - Inoperative Fueling Shutoff Valve
2. Refuel Operation - Inoperative Fueling Quantity Indicator
A. Prepare the Airplane
(1)
Read and obey the precautions in this task: Precautions and Limits for Fuel Servicing (AMM 12-11-01/301).
WARNING: OBEY ALL THE FUEL SERVICING AND MANUAL PRESSURE REFUEL PRECAUTIONS IN AMM 12-11-01/301. FAILURE TO OBEY THE PRECAUTIONS CAN CAUSE SERIOUS INJURY TO PERSONS AND DAMAGE TO EQUIPMENT.
(2)
Do this task: Prepare the Airplane for a Refuel Operation (AMM 12-11-01/301).
(3)
Do one of these procedures to refuel the airplane with an inoperative fueling quantity indicator:
(a)
Fuel Transfer Method
(b)
Fuel Truck Flow Meter Method
(c)
Fuel Measuring Sticks Method
B. Fuel Transfer Method
(1) Transfer fuel from the tank with an inoperative fueling quantity indicator:
(a)
Make sure the fueling shutoff (refuel) valve(s) in the tank with an inoperative indicator are closed.
(b)
Make sure the receiving tank(s) have enough fuel capacity to accept all of the fuel from the tank with an inoperative indicator.
(c)
Transfer all of the fuel from the tank with an inoperative (AMM 28-23-0/201). 1) Continue the fuel transfer until the fuel pump low pressure lights come on.
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