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provide go-around guidance commands throughout the maneuver.
If a go-around is initiated after touchdown but prior to thrust reverser selection,
auto speedbrakes retract and autobrakes disarm as thrust levers are advanced. The
F/D go-around mode will not be available until go-around is selected after
becoming airborne.
Once reverse thrust is initiated following touchdown, a full stop landing must be
made. Factors dictating this are:
• five seconds are required for a reverser to transition to the forward thrust
position
• a possibility exists that a reverser may not stow in the forward thrust
position.
Normal Touchdown Attitude
The following figures illustrate the effect of airspeed on body attitude on
touchdown. It shows normal touchdown attitude for flaps 30. If flare control and
thrust are excessive near touchdown, the airplane tends to float in ground effect.
With proper airspeed control and thrust management, touchdown occurs at no less
than VREF - 5. The illustration shows that touchdown at a speed significantly
below VREF seriously reduces aft fuselage-runway clearance.
October 31, 2004
767 Flight Crew Training Manual
Landing
Copyright © The Boeing Company. See title page for details.
6.12 FCT 767 (TM)
Touchdown Body Attitudes
767-200
160 200 240 280 320 360 400 440
0
2
4
6
8
10
12
14
16
(72.6) (90.7) (108.9) (127.0) (145.1) (163.3)
Gross Weight - 1000 lbs (kgs)
(181.4) (199.6)
VREF 30 - 10
VREF 30
Body Contact Possible
VREF 30 - 5
Pitch Attitude (Degrees)
Sea Level Standard Day
2.5 fps R/S at Touchdown
Flaps 30
Attitude Limit:
Main Gear Struts Extended
Main Gear Struts Compressed
October 31, 2004
767 Flight Crew Training Manual
Landing
Copyright © The Boeing Company. See title page for details.
FCT 767 (TM) 6.13
767-300
Pitch Attitude (Degrees)
2
4
6
8
10
12
14
16
0
160 200 240 280 320 360 400 440
(72.6) (90.7) (108.9) (127.0) (145.1) (163.3)
Gross Weight - 1000 lbs (kgs)
(181.4) (199.6)
VREF 30 - 10
VREF 30
Skid Contact Possible
VREF 30 - 5
Sea Level Standard Day
2.5 fps R/S at Touchdown
Flaps 30
Attitude Limit:
Main Gear Struts Extended
Main Gear Struts Compressed
October 31, 2004
767 Flight Crew Training Manual
Landing
Copyright © The Boeing Company. See title page for details.
6.14 FCT 767 (TM)
767-400
200 240 280 320 360 400 440 480
Pitch Attitude (Degrees)
2
4
6
8
10
12
14
16
0
Gross Weight - 1000 lbs (kgs)
(90.7) (108.9) (127.0) (145.1) (163.3) (181.4) (199.6) (217.7)
Skid Contact Possible
VREF 30 - 10
VREF 30
VREF 30 - 5
Sea Level Standard Day
2.5 fps R/S at Touchdown
Flaps 30
Attitude Limit:
Main Gear Struts Extended
Main Gear Struts Compressed
October 31, 2004
767 Flight Crew Training Manual
Landing
Copyright © The Boeing Company. See title page for details.
FCT 767 (TM) 6.15
Body Clearance at Touchdown
The following figures show aft fuselage-runway clearance in relation to pitch
angle with all main gear tires on the runway.
Body Clearance above Ground
767-200
Pitch Angle (Degrees)
0
2
4
6
8
10
12
14
0 20 40 60 80 100 120 140
Clearance - inches (cm)
(0) (51) (102) (152) (203) (254) (305) (356)
Main Gear Struts Extended
Main Gear Struts Compressed
October 31, 2004
767 Flight Crew Training Manual
Landing
Copyright © The Boeing Company. See title page for details.
6.16 FCT 767 (TM)
767-300
10
12
14
0
2
4
6
8
0 20 40 60 80 100 120 140
Pitch Angle (Degrees)
Aft Body
Extended Tail Skid
(0) (51) (102) (152) (203) (254) (305) (356)
Clearance - inches (cm)
Main Gear Struts Extended
Main Gear Struts Compressed
October 31, 2004
767 Flight Crew Training Manual
Landing
Copyright © The Boeing Company. See title page for details.
FCT 767 (TM) 6.17
767-400
10
12
0
2
4
6
8
Pitch Angle (Degrees)
0 20 40 60 80 100 120 140
(0) (51) (102) (152) (203) (254) (305) (356)
Clearance - inches (cm)
Aft Body
Extended Tail Skid
Main Gear Struts Extended
Main Gear Struts Compressed
14
October 31, 2004
　
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