(4) F72949 - Fuel measuring stick operating tool
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28-23-00
ALL ú ú 01 Page 202 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
C.
D.
E.
F.
A 737-300/400/500MAINTENANCE MANUAL
(5)
F70316-1 or F70316-140 - Auxiliary defueling external power control
unit (PCU), (used only for the procedure to defuel with the PCU).Standard Tools and Equipment
(1)
Truck - fuel, or equivalent servicing facility (must have a suction pump if you are scheduled to use suction defueling).
(2)
AIRPLANES WITH SUMP DRAIN VALVE P/N 80182; Tube - Center Wing Tank Sump Drain, 0.5 inch I.D. hose and clamp
(assembled locally).References
(1)
AMM 20-40-11/201, Static Grounding
(2)
AMM 28-10-00/201, Storage
(3)
AMM 28-11-11/401, Wing Fuel Tank Access Panels
(4)
AMM 28-22-61/401, Fuel Boost Pump Bypass ValveAccess
(1)
Location Zones 221 Center Section Fuel Tank 305 Left Fuel Tank 405 Right Fuel Tank
(2)
Access Panels 6540 Refueling Station Access Door 6535 Defueling Access Door
Defuel through the Pressure Fueling Receptacle With the Airplane Boost Pumps and the Defueling (Suction) Pump on the Fuel Truck
NOTE: It is necessary to operate the boost pumps.
____
S 862-014
(1)
Electrically ground the airplane and the fuel truck (AMM 20-40-11/201).
S 862-015
(2)
Connect the electrical power to the airplane (AMM 24-22-00/201).
NOTE: If you are not scheduled to defuel the No. 1 tank fully,
____ you can use the APU to supply electrical power. You must have a minimum quantity of fuel in the No. 1 tank to use the APU (AMM 49-11-00/201).
S 862-016
(3)
Make sure all circuit breakers for the fuel system on the P6 panel are closed.
(4)
Open the access door, 6540, for the refuel station (P15 panel).
(5)
Remove the cap on the fueling receptacle.
S 012-018
S 032-001
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