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110k Engine
Attitude Limit:
Main Gear Struts Extended
Main Gear Struts Compressed
Body Contact Possible
V
V
REF 30 - 5
REF 30
115k Engine
(163) (181) (200) (218) (236) (254) (272) (290)
Gross Weight - 1000 lbs (kgs)
14
VREF 30 - 10
- 150 fpm at Touchdown
Sea Level Standard Day
Flaps 30
Forward CG Limit
October 31, 2006
777/787 Flight Crew Training Manual
Landing
Copyright © The Boeing Company. See title page for details.
6.16 FCT 777/787 Preliminary (TM)
777-300
Skid Contact Possible
12
14
8
10
2
4
6
0
Pitch Attitude - (Degrees)
Gross Weight - 1000 lbs (kgs)
280 320 360 400 440 480 520 560
(127) (145) (163) (181) (200) (218) (236) (254)
Attitude Limit:
Main Gear Struts Extended
Main Gear Struts Compressed
V
V
V
REF 30 - 10
REF 30 - 5
REF 30
- 150 fpm at Touchdown
Sea Level Standard Day
Flaps 30
Forward CG Limit
October 31, 2006
777/787 Flight Crew Training Manual
Landing
Copyright © The Boeing Company. See title page for details.
FCT 777/787 Preliminary (TM) 6.17
777-300ER
12
14
8
10
2
4
6
0
360 400 440 480 520 560 600 640
Gross Weight - 1000 lbs (kgs)
(163) (181) (200) (218) (236) (254) (272) (290)
Attitude Limit:
Main Gear Struts Extended
Main Gear Struts Compressed
Skid Contact Possible
Pitch Attitude - (Degrees)
V
V
REF 30 - 5
REF 30
VREF 30 - 10
- 150 fpm at Touchdown
Sea Level Standard Day
Flaps 30
Forward CG Limit
October 31, 2006
777/787 Flight Crew Training Manual
Landing
Copyright © The Boeing Company. See title page for details.
6.18 FCT 777/787 Preliminary (TM)
787-8
TBD
October 31, 2006
777/787 Flight Crew Training Manual
Landing
Copyright © The Boeing Company. See title page for details.
FCT 777/787 Preliminary (TM) 6.19
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
777-200, 777-200LR
14
12
8
6
10
4
2
0
0 20 40 60 80 100 120 140
Clearance - inches (cm)
Pitch Angle (Degrees)
Main Gear Struts Compressed
Tail Strike Proximity Sensor Contact
Main Gear Struts Extended
(0) (51) (102) (152) (203) (254) (305) (356)
October 31, 2006
777/787 Flight Crew Training Manual
Landing
Copyright © The Boeing Company. See title page for details.
6.20 FCT 777/787 Preliminary (TM)
777-300
14
12
8
6
10
4
2
0
Pitch Angle (Degrees)
Aft Body
Extended Tail Skid
Tail Strike Proximity Sensor Contact
Main Gear Struts Extended
Main Gear Struts Compressed
0 20 40 60 80 100 120 140
Clearance - inches (cm)
(0) (51) (102) (152) (203) (254) (305) (356)
October 31, 2006
777/787 Flight Crew Training Manual
Landing
Copyright © The Boeing Company. See title page for details.
FCT 777/787 Preliminary (TM) 6.21
777-300ER
Main Gear Struts Compressed
Main Gear Struts Extended
0 20 40 60 80 100 120 140
Clearance - inches (cm)
(0) (51) (102) (152) (203) (254) (305) (356)
14
12
8
6
10
4
2
0
Pitch Angle (Degrees)
Aft Body
Extended Tail Skid
Tail Strike Proximity Sensor Contact
October 31, 2006
777/787 Flight Crew Training Manual
Landing
Copyright © The Boeing Company. See title page for details.
6.22 FCT 777/787 Preliminary (TM)
787-8
TBD
October 31, 2006
777/787 Flight Crew Training Manual
Landing
Copyright © The Boeing Company. See title page for details.
FCT 777/787 Preliminary (TM) 6.23
Pitch and Roll Limit Conditions
The Ground Contact Angles - Normal Landing figure illustrates body roll
angle/pitch angles at which the airplane structure contacts the runway. Prolonged
flare increases the body pitch attitude 2° to 3°. When prolonged flare is coupled
with a misjudged height above the runway aft body contact is possible.
Fly the airplane onto the runway at the desired touchdown point and at the desired
airspeed. Do not hold it off and risk the possibility of a tailstrike.
Note: A smooth touchdown is not the criterion for a safe landing.
October 31, 2006
　
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本文鏈接地址：787機組訓練手冊Flight Crew Training Manual 787(98)