Copyright . The Boeing Company. See title page for details.
6.20 FCT 737 (TM) October 31, 2006
737 Flight Crew Training Manual
737-900 16 14
Pitch Attitude (Degrees)
8 6 4 2
0
Gross Weight - 1000 lbs (kgs)
737 Flight Crew Training Manual
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
737-300
Pitch Angle (Degrees)
16 14 12 10 8 6 4 2 0
0 10 20 30 40 50 60 70
(0) (25) (51) (76) (102) (127) (152) (178)
Clearance -inches (cm)
Copyright . The Boeing Company. See title page for details.
6.22 FCT 737 (TM) October 31, 2006
737 Flight Crew Training Manual
737-400
Pitch Angle (Degrees)
14 12 10 8 6 4 2 0
0 10 20 30 40 50 60 70
(0) (25) (51) (76) (102) (127) (152) (178)
Clearance - inches (cm)
737 Flight Crew Training Manual
737-500
Pitch Angle (Degrees)
16 14 12 10 8 6 4 2 0
0 10 20 30 40 50 60 70
(0) (25) (51) (76) (102) (127) (152) (178)
Clearance - inches (cm)
Copyright . The Boeing Company. See title page for details.
6.24 FCT 737 (TM) October 31, 2006
737 Flight Crew Training Manual
737-600
Pitch Angle (Degrees)
18 16 14 12 10 8 6 4 2 0
0 10 20 30 40 50 60 70
(0) (25) (51) (76) (102) (127) (152) (178)
Clearance - inches (cm)
737 Flight Crew Training Manual
Pitch Angle (Degrees)
737 Flight Crew Training Manual
737-800
Pitch Angle (Degrees)
14 12 10 8 6 4 2 0
0 10 20 30 40 50 60 70
(0) (25) (51) (76) (102) (127) (152) (178)
Clearance - inches (cm)
737 Flight Crew Training Manual
737-800SFP
Note: This figure shows runway clearance for the 737-400SFP airplane equippedwith a 2-position tail skid. For the 737-400SFP airplane equipped with a 1-position tail skid, see the basic 737-800 figure on the previous page.
Pitch Angle (Degrees)
14 12 10 8 6 4 2 0
0 10 20 30 40 50 60 70
(0) (25) (51) (76) (102) (127) (152) (178)
Clearance - inches (cm)
Copyright . The Boeing Company. See title page for details.
6.28 FCT 737 (TM) October 31, 2006
737 Flight Crew Training Manual
737-900 14
12
Pitch Angle (Degrees)
8 6 4 2
737 Flight Crew Training Manual
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.
Copyright . The Boeing Company. See title page for details.
6.30 FCT 737 (TM) October 31, 2006
737 Flight Crew Training Manual
Ground Contact Angles -Normal Landing
Conditions
.
Pitch about main gear centerline . Stabilizer full nose up
.
Slats fully extended . Elevator full down
.
Aileron full down . Struts compressed
.
Roll about outer tire centerline . Flaps 40
737-300 - 737-500
15
10
5
0
-5
0
Pitch Angle (Degrees)
737 Flight Crew Training Manual
737-600 - 737-900
Pitch Angle (Degrees)
15
10
5
0
-5 0 5 10 1520 Roll Angle (Degrees)
Copyright . The Boeing Company. See title page for details.
6.32 FCT 737 (TM) October 31, 2006
737 Flight Crew Training Manual
Landing Roll
Avoid touching down with thrust above idle since this may establish an airplane
nose up pitch tendency and increases landing roll. After main gear touchdown, initiate the landing roll procedure. If the speedbrakes do not extend automatically move the speedbrake lever to the UP position without delay. Fly the nose wheels smoothly onto the runway without delay. Control column movement forward of neutral should not be required. Do not attempt to hold the nose wheels off the runway. Holding the nose up after touchdown for aerodynamic braking is not an effective braking technique and may result in high nose gear sink rates upon brake application.
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