BOEING 737 Fuel Usage | Boeing 737 pilot training course,

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Fuel
Limitations
1. (ETOPS) Perform an operational check of the fuel crossfeed
valve during the last hour of cruise flight during each extended range
operation. Enter valve failure conditions resulting from the operational check in the airplane log.

2. Maximum tank fuel temperature: 49°C.

3. Inflight tank fuel temperature must be maintained at least 3°C above the
freezing point of the fuel being used or -45°C, whichever is higher.

4. Lateral fuel imbalance between wing tanks 1 and 2 must be scheduled to be
zero. Random fuel imbalance must not exceed 1000 lbs.

5. Fuel Crossfeed valve must be closed for takeoff and landing.

6. Center tank fuel pump switches
Ground Operations (Per A.D. 2001-08-24)
• Center tank fuel pump switches must not be positioned to ON unless
the center tank fuel quantity exceeds 1000 pounds (453 kilograms),
except when defueling or transferring fuel.
• Center tank fuel pump switches must be positioned to OFF when both
center tank fuel pump low-pressure lights illuminate.
• Center tank fuel pump switches must not be positioned to ON unless
personnel are available on the flight deck to monitor low-pressure
lights.
Note: Once the center tank fuel pump switches are turned on, they do
not need to be turned off once the fuel quantity depletes to less
than 1000 lbs.

7. Center tank fuel pump switches:
Per AD 2002-19-52, and AD 2002-24-51 with AMOC 140S-02-376:
“The center tank fuel pumps must be OFF for takeoff if center tank fuel is
less than 5,000 lbs. with the airplane readied for initial taxi.
Both center tank fuel pump switches must be selected OFF when center tank
fuel quantity reaches approximately 1,000 lbs. during climb and cruise or
3,000 lbs. during descent and landing. The fuel pumps must be positioned
OFF at the first indication of fuel pump low pressure.”
The center wing tank fuel quantity indication system must be operative to
dispatch with center wing tank fuel.
Note: The CONFIG indicator will annunciate when center tank fuel exceeds 1,600 lbs. and the center tank fuel pump switches are OFF. Do not
accomplish the CONFIG non-normal procedure prior to or during
takeoff with less than 5,000 lbs. of center tank fuel or during descent
and landing with less than 3,000 lbs. of center tank fuel.
Note: In a low fuel situation, both center tank pumps may be selected ON
and all center tank fuel may be used.
If the main tanks are not full, the zero fuel gross weight of the
airplane plus the weight of center tank fuel may exceed the maximum zero fuel gross weight by up to 5,000 lbs. for takeoff, climb, and cruise and up to 3,000 lbs. for descent and landing,
provided that the effects of balance (CG) have been considered.
If a center tank fuel pump fails with fuel in the center tank,
accomplish the FUEL PUMP LOW PRESSURE non-normal procedure. Prior to transferring or defueling conduct a lamp test of the
respective fuel pump low pressure lights. When transferring or
defueling from either the center or main wing tanks, the FUEL PUMP
LOW PRESSURE indication lights must be monitored and the fuel
pumps positioned to OFF at the first indication of fuel pump low
pressure. Fuel may be transferred from tank to tank or the aircraft
may be defuled with passengers on board, provided the fuel quantity
in the tank from which fuel is being taken is maintained at not less
than 2,000 pounds (900 kilograms). Deplane all passengers and
non-essential crew when defueling a tank or transferring fuel from a
tank that has a fuel quantity below 2,000 pounds (900 kilograms)
until the process has been completed and the respective fuel boost
pumps are turned off. The limitations contained in this AD supersede any conflicting basic aircraft flight manual limitations.”

Fuel Usage
Center Tank:

• If a center tank LOW PRESSURE light(s) illuminates during takeoff or
initial climb, the center tank pump(s) may remain on until the climb
attitude is reduced and the light(s) extinguishes or workload allows for
the pump(s) to be positioned OFF. When established in a level attitude
at cruise, if the center tank contains usable fuel and the center tank
switches are OFF, the center tank pump switches should be positioned
ON again.
• If the center tank contains more than 1000 lbs., the center tank switches must be turned ON. Verify the LOW PRESSURE lights extinguish and position both switches OFF when both LOW PRESSURE
lights illuminate.

• Use center tank fuel to depletion, followed by main wing tank fuel.
However, a maximum of 1000 lbs. may be retained in the center tank.
Auxiliary tank (if installed):
•  Auxiliary tank installed: Use auxiliary tank fuel and
center wing tank fuel equally until auxiliary tank fuel is depleted.

Tank Capacity – Usable

Wing tanks 1,499 U.S. Gals/10043 lbs. 1,288 U.S. Gals / 8630 lbs.

Center tank 2,313 U.S. Gals/15497 lbs. 4,299 U.S. Gals / 28803 lbs.

Auxiliary tank 390 U.S. Gals/2620 lbs. N/A

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CLICK 👉 CENTER TANK SCAVENGE JET PUMP

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CLICK 👉 FUEL MEASURING DRIPSTICK

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