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Flaps 20
Flaps 5
Flaps 1
Flaps Up
Weight = 345,000 Lbs
15° Bank
25° Bank
Max. Structural
Flaps Down
Load Factor,
40° Bank
156,485 Kgs
One Engine Inoperative
Sea Level
Standard Day
V2 (flaps 20)
October 31, 2004
767 Flight Crew Training Manual
General Information
Copyright © The Boeing Company. See title page for details.
1.8 FCT 767 (TM)
Maneuver Margins to Stick Shaker Landing
767-200
110 130 150 170 190 210 230 250
Maneuver Margin to Stick Shaker (G's)
3.4
3.0
2.6
2.2
1.8
1.4
1.0
Airspeed (KCAS)
Flaps 30
Flaps 20
Flaps 5
Flaps 1
Flaps Up
Weight = 270,000 Lbs
VREF30
15° Bank
25° Bank
Max. Structural
Flaps Down
Load Factor,
40° Bank
122,466 Kgs
All Engines Operating
Sea Level
Standard Day
October 31, 2004
767 Flight Crew Training Manual
General Information
Copyright © The Boeing Company. See title page for details.
FCT 767 (TM) 1.9
Maneuver Margins to Stick Shaker Takeoff
767-300
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)
Flaps 20
Flaps 5
Flaps 1
Flaps Up
Weight = 380,000 Lbs
15° Bank
25° Bank
Max. Structural
Flaps Down
Load Factor,
40° Bank
172,360 Kgs
One Engine Inoperative
Sea Level
Standard Day
V2 (flaps 20)
October 31, 2004
767 Flight Crew Training Manual
General Information
Copyright © The Boeing Company. See title page for details.
1.10 FCT 767 (TM)
Maneuver Margins to Stick Shaker Landing
767-300
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)
Flaps 30
Flaps 20
Flaps 5
Flaps 1
Flaps Up
Weight = 300,000 Lbs
VREF30
15° Bank
25° Bank
Max. Structural
Flaps Down
Load Factor,
40° Bank
136,074 Kgs
All Engines Operating
Sea Level
Standard Day
October 31, 2004
767 Flight Crew Training Manual
General Information
Copyright © The Boeing Company. See title page for details.
FCT 767 (TM) 1.11
Maneuver Margins to Stick Shaker Takeoff
767-400
2.0
2.6
2.2
1.8
1.4
140 160 180 200 220 240 260 280
40° Bank
25° Bank
15° Bank
Flaps Up
Flaps 20
Flaps 5
Fl aps 1
Maneuver Margin to Stick Shaker (G's)
Airspeed (KCAS)
Max. Structural
Flaps Down
Load Factor,
Weight = 450,000 Lbs
204,080 Kgs
One Engine Inoperative
Sea Level
Standard Day
1.0
2.4
V2 (flaps 20)
October 31, 2004
767 Flight Crew Training Manual
General Information
Copyright © The Boeing Company. See title page for details.
1.12 FCT 767 (TM)
Maneuver Margins to Stick Shaker Landing
767-400
120 140 160 180 200 220 240
Flaps Up
Flaps 20
Flaps 30
Flaps 5
Flaps 1
Weight = 350,000 Lbs
Max. Structural
Flaps Down
Load Factor,
158,730 Kgs
All Engines Operating
Sea Level
Standard Day
Maneuver Margin to Stick Shaker (G's)
Airspeed (KCAS)
260
VREF30
15° Bank
25° Bank
40° Bank
3.4
3.0
2.6
2.2
1.8
1.4
1.0
October 31, 2004
767 Flight Crew Training Manual
General Information
Copyright © The Boeing Company. See title page for details.
FCT 767 (TM) 1.13
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
　
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