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Flaps Up
October 31, 2006
777/787 Flight Crew Training Manual
General Information
Copyright © The Boeing Company. See title page for details.
FCT 777/787 Preliminary (TM) 1.11
Maneuver Margins to Stick Shaker Takeoff
777-300
140 160 180 200 220 240 260 280
Maneuver Margin to Stick Shaker (G's)
3.4
3.0
2.6
2.2
1.8
1.4
1.0
Airspeed (KCAS)
Weight = 660,000 Lbs
25° Bank
Max. Structural
Flaps Down
Load Factor,
40° Bank
299,374 Kgs
One Engine Inoperative
Sea Level
Standard Day
15° Bank
Flaps 20
Flaps 5
Flaps 1
Flaps Up
V2 (flaps 20)
October 31, 2006
777/787 Flight Crew Training Manual
General Information
Copyright © The Boeing Company. See title page for details.
1.12 FCT 777/787 Preliminary (TM)
Maneuver Margins to Stick Shaker Landing
777-300
120 140 160 180 200 220 240 260
Maneuver Margin to Stick Shaker (G's)
3.4
3.0
2.6
2.2
1.8
1.4
1.0
Airspeed (KCAS)
Weight =524,000 Lbs
VREF30
25° Bank
Max. Structural
Flaps Down
Load Factor,
40° Bank
237,685 Kgs
All Engines Operating
Sea Level
Standard Day
15° Bank
Flaps Up
Flaps 30
Flaps 20
Flaps 5
Flaps 1
October 31, 2006
777/787 Flight Crew Training Manual
General Information
Copyright © The Boeing Company. See title page for details.
FCT 777/787 Preliminary (TM) 1.13
Maneuver Margins to Stick Shaker Takeoff
777-300ER
160 180 200 220 240 260 280 300
Maneuver Margin to Stick Shaker (G's)
3.4
3.0
2.6
2.2
1.8
1.4
1.0
Airspeed (KCAS)
Weight = 775,000 Lbs
25° Bank
Max. Structural
Flaps Down
Load Factor,
40° Bank
351,538 Kgs
One Engine Inoperative
Sea Level
Standard Day
Flaps Up
15° Bank
Flaps 5
Flaps 20
Flaps 1
V2 (flaps 20)
October 31, 2006
777/787 Flight Crew Training Manual
General Information
Copyright © The Boeing Company. See title page for details.
1.14 FCT 777/787 Preliminary (TM)
Maneuver Margins to Stick Shaker Landing
777-300ER
120 140 160 180 200 220 240 260
Maneuver Margin to Stick Shaker (G's)
3.4
3.0
2.6
2.2
1.8
1.4
1.0
Airspeed (KCAS)
Weight = 554,000 Lbs
VREF30
25° Bank
Max. Structural
Flaps Down
Load Factor,
40° Bank
251,293 Kgs
All Engines Operating
Sea Level
Standard Day
Flaps Up
15° Bank
Flaps 30
Flaps 20
Flaps 5
Flaps 1
October 31, 2006
777/787 Flight Crew Training Manual
General Information
Copyright © The Boeing Company. See title page for details.
FCT 777/787 Preliminary (TM) 1.15
Maneuver Margins to Stick Shaker Takeoff
787-8
TBD
October 31, 2006
777/787 Flight Crew Training Manual
General Information
Copyright © The Boeing Company. See title page for details.
1.16 FCT 777/787 Preliminary (TM)
Maneuver Margins to Stick Shaker Landing
787-8
TBD
October 31, 2006
777/787 Flight Crew Training Manual
General Information
Copyright © The Boeing Company. See title page for details.
FCT 777/787 Preliminary (TM) 1.17
Flap Operation
Acceleration Height - All Engines
The altitude selected for acceleration and flap retraction may be specified for each
airport. Safety, obstruction clearance, airplane performance or noise abatement
requirements are usually the determining factors. Some operators have adopted a
standard climb profile for all of their operations based on the airport which
requires the greatest height for level off to clear a close-in obstacle with an engine
failure.
The minimum altitude for flap retraction is 400 feet. Boeing recommends 1000
feet for the standard flap retraction altitude used in training.
Acceleration Height - Engine Out
Acceleration height for a takeoff with an engine failure after V1 is based on
accelerating to the recommended flaps up speed while retracting flaps and
selecting maximum continuous thrust limits within 5 minutes (10 minutes
optional) after initiating takeoff. Some combinations of high gross weight, takeoff
flap selection and airport elevation may require initiating flap retraction as low as
400 feet after takeoff with an engine failure.
At typical training weights, adequate performance exists to climb to 1000 feet
　
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