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Boeing 737-800 - Fuel System; Fuel Balance; Fuel Loading; Landing Gear

Boeing 737-800
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737 Flight Crew Operations Manual
Limitations -
Operating Limitations
Boeing Proprietary. Copyright © Boeing. May be subject to export restrictions under EAR. See title page for details.
L.10.8 D6-27370-866-EGP
YK981 - YQ456
# Avoid weather radar operation in a hangar, or within 50 feet (15.25 meters) of
fueling operations or a fuel spill.
Avoid weather radar operation when personnel are within the area normally
enclosed by the aircraft nose radome.
Note: The hangar recommendation does not apply to the weather radar test mode.
Runway Awareness and Advisory System (RAAS)
YK995 - YQ456
Do not use RAAS callouts or alerts for navigation.
Do not use RAAS callouts or alerts as a substitute for NOTAM or ATIS
information.
Fuel System
Maximum tank fuel temperature is 49°C.
Minimum tank fuel temperature prior to takeoff and inflight is - 43°C, or 3°C
above the fuel freezing point temperature, whichever is higher.
Note: The use of Fuel System Icing Inhibitor additives does not change the
minimum fuel tank temperature limit.
Intentional dry running of a center tank fuel pump (low pressure light illuminated)
is prohibited.
Fuel Balance
Lateral imbalance between main tanks 1 and 2 must be scheduled to be zero.
Random fuel imbalance must not exceed 453 kgs for taxi, takeoff, flight or
landing.
Fuel Loading
Main tanks 1 and 2 must be full if center tank contains more than 453 kgs.
Landing Gear
Operation with assumed temperature reduced takeoff thrust is not permitted with
anti-skid inoperative.
Non–AFM Operational Information
Note: The following items are not AFM limitations, but are provided for flight
crew information.
Do not apply brakes until after touchdown.
September 15, 2016

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