787 Flight Crew Operations Manual
DO NOT USE FOR FLIGHT
Performance Dispatch
Text
787-8/
FAA
Category A Brakes
Copyright © The Boeing Company. See title page for details.
PD.13.6 D615Z003-TBC
Landing
Tables are provided for determining the maximum landing weight as
limited by field length or climb requirements for Flaps 30.
Maximum landing weight is the lowest of the field length limit weight,
climb limit weight or maximum certified landing weight.
Landing Field Limit Weight
Obtain wind corrected field length by entering upper table with field length
available and wind component along the runway. Now enter table with
wind corrected field length and pressure altitude to read field limit weight
for the expected runway condition.
Landing Climb Limit Weight
Enter table with airport OAT and pressure altitude to read landing climb
limit weight. Apply the noted adjustments as required.
Go-Around Climb Gradient
Enter the Reference Go-around Gradient table with airport OAT and
pressure altitude to determine the reference Go-Around Gradient. Then
adjust the reference gradient for airplane weight and speed using the tables
provided to determine the weight and speed adjusted Go-Around Gradient.
Note that data is for one engine inoperative.
Quick Turnaround Limit Weight
Enter table with airport pressure altitude and OAT to read maximum quick
turnaround weight. Apply the noted adjustments as required.
If the landing weight exceeds the maximum quick turnaround weight, wait
the specified time and then check that the wheel thermal plugs have not
melted before executing a subsequent takeoff.
February 15, 2010
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