NOTE : Refer to the fuel tables for the maximum capacity of each fuel
____ tank and for the total fuel capacity. If the intercell transfer valves are open, the full capacity of a wing tank is less than normal.
 (4)
 When the quantity of fuel in a tank is correct, release the manual plunger on the related refuel valve.

 (5)
 When all the fuel quantities are correct, stop the pump on the fuel tanker/pump unit.

 (6)
 Make an entry in the aircraft technical log, to check the fuel configuration before the subsequent flight.

 **ON A/C 301-399,
 Subtask 12-11-28-650-056-A
 A. Pressure Refuel without Electrical Power
 (1)
 Start the pump on the fuel tanker/pump unit.

 (2)
 Push and hold in the manual plunger(s) on the refuel valve(s) of the applicable fuel tank(s).

 (3)
 Use the MLIs to monitor the quantity of fuel in each tank (Ref. TASK 12-11-28-650-007).

 NOTE : Refer to the fuel tables for the maximum capacity of each fuel
____
 tank and for the total fuel capacity.

 (4)
 When the quantity of fuel in a tank is correct, release the manual plunger on the related refuel valve.

 (5)
 When all the fuel quantities are correct, stop the pump on the fuel tanker/pump unit.

 (6)
 Make an entry in the aircraft technical log, to check the fuel configuartion before the subsequent flight.

 1EFF : ALL 1 12-11-28Page 344 1 1 May 01/05R 1 1 1CES 1

 **ON A/C ALL
 5. Close-up
________
 Subtask 12-11-28-860-060

 A. Aircraft Configuration
 (1)
 Retract and lock the MMIs (Ref. TASK 12-11-28-650-007).

 (2)
 Disconnect the coupling of the fuel supply-hose from the aircraft refuel coupling.

 (3)
 Disconnect these bonding/ground cables:

 -between the aircraft and the fuel tanker/pump unit
 -if applicable, between the fuel tanker/pump unit and the ground
 -if applicable, between the aircraft and the ground. R **ON A/C 001-049, 052-099, 101-149, 151-199, 201-299, 301-399, 401-499,
 Subtask 12-11-28-410-054
 B. Close Access
 (1) To install the coupling cap and the access panel: CAUTION : MAKE SURE THAT THE HANDLE OF THE REFUEL COUPLING CAP POINTS
_______ AFT WHEN THE CAP IS CLOSED AND LOCKED.
 (a) Install the refuel coupling cap 41QM and close the access panel 622JB.
 (2) If you have refuelled the center tank, close the MLG door 744 (Ref. TASK 32-12-00-410-001).

R  **ON A/C 051-051, 
R  Subtask 12-11-28-410-054-A 
R  B. Close Access 
R  (1) To install the coupling cap and the access panel: 
R R  CAUTION : MAKE SURE THAT THE HANDLE OF THE REFUEL COUPLING CAP POINTS_______ AFT WHEN THE CAP IS CLOSED AND LOCKED. 
R R  (a) Install the applicable refuel coupling cap 101QM(41QM) and close the applicable access panel 522JB(622JB). 
R R  (2) If you have refuelled the center tank, close the MLG door 744 (Ref. TASK 32-12-00-410-001). 
R  **ON A/C ALL
 Subtask 12-11-28-942-056
 C. Removal of Equipment
 (1) Make sure that the work area is clean and clear of tool(s) and other items.
 (2) Remove the safety barriers.
 (3) Remove the warning notice(s).
 (4) Remove the access platform(s).
 (5) Remove the ground support and maintenance equipment, the special and standard tools and all other items.

 TASK 12-11-28-650-006

 Overwing (Gravity) Refuel
 WARNING : OBEY THE FUEL SAFETY PROCEDURES.

_______
 WARNING : STOP THE FUEL TANKER 200 ft. (60 m) FROM THE AIRCRAFT NOSE WHILE THE

_______ WEATHER RADAR OPERATES. DO NOT OPERATE THE FUEL TANKER/PUMP UNIT UNTIL YOU STOP THE OPERATION OF THE WEATHER RADAR.
 WARNING : MAKE SURE THE AREA AROUND THE AIRCRAFT IS SAFE BEFORE YOU START THE
_______ REFUEL/DEFUEL PROCEDURE. IN THE SAFETY AREA, DO NOT:
 -SMOKE

 -MAKE SPARKS OR FIRE

 -USE ANY EQUIPMENT WHICH IS NOT APPROVED FOR REFUEL/DEFUEL
 PROCEDURES.
 AIRCRAFT FUEL IS FLAMMABLE.

 WARNING : DO NOT GET YOUR CLOTHES SOAKED WITH FUEL.
_______
 WARNING : DO NOT SPILL FUEL ON THE ENGINES OR THE BRAKES. IF YOU SPILL FUEL ON

_______ ENGINES OR BRAKES THAT ARE HOT, IT CAN CAUSE FIRES.
 1.
 Reason for the Job

__________________
 Self Explanatory

 2.
 Job Set-up Information

　
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