737-600 - 737-900
VR Liftoff V2 to V2+ 20
12-14° 35 ft.
7 - 11°
0
5 10 to 12 Time Seconds
Retract the landing gear after a positive rate of climb is indicated on the altimeter. Retract flaps in accordance with the technique described in this chapter.
Copyright . The Boeing Company. See title page for details.
October 31, 2006 FCT 737 (TM) 3.33
Typical Takeoff Tail Clearance - One Engine Inoperative
The following diagram and table show the effect of flap position on liftoff pitch attitude and minimum tail clearance during takeoff with one engine inoperative. Additionally, the last column shows the pitch attitude for tail contact with wheels on the runway and landing gear struts extended. The tail strike pitch attitude remains the same as during takeoffs with all engines operating. For a discussion of tail strike procedures, see chapter 8 and the FCOM.
Note: Use of flaps 1 as a takeoff flap setting is restricted to airplanes delivered with this capability or to airplanes having flaps 1 installed as a takeoff flap setting.
Tail clearance height
Height Above Runway
Gear height
Min. tail clearance
737-300 - 737-500
Model Flaps Liftoff Attitude (degrees) Minimum Tail Clearance inches (cm) Tail Strike Pitch Attitude (degrees)
737-300 1 11.3 14 (36)
5 11.0 16 (41) 13.4
15 10.3 19 (48)
737-400 5 10.3 4 (10) 11.4
15 9.8 10 (25)
737-500 1 11.3 21 (53)
5 11.0 23 (58) 14.7
15 10.3 26 (66)
Copyright . The Boeing Company. See title page for details.
3.34 FCT 737 (TM) October 31, 2006
737 Flight Crew Training Manual
737-600 - 737-900
Model Flaps Liftoff Attitude (degrees) Minimum Tail Clearance inches (cm) Tail Strike Pitch Attitude (degrees)
737-600 1 11.0 24 (61)
5 11.0 24 (61)
10 10.8 25 (64) 16.2
15 10.5 26 (66)
25 10.2 28 (71)
737-700 1 11.0 18 (46)
5 11.0 18 (46)
10 10.8 19 (48) 14.7
15 10.6 21 (53)
25 10.2 23 (58)
737-800 1 8.9 10 (25)
5 8.9 10 (25)
10 8.7 10 (25) 11.0
15 8.5 13 (33)
25 8.3 15 (38)
737-800SFP 1 8.9 8 (20)
5 8.8 11 (28)
10 8.4 14 (36) 11.0
15 8.0 15 (38)
25 7.9 17 (43)
737-900 1 8.4 13 (33)
5 8.3 13 (33)
10 8.1 13 (33) 10.0
15 7.8 16 (41)
25 7.6 18 (46)
Copyright . The Boeing Company. See title page for details.
October 31, 2006 FCT 737 (TM) 3.35
737 Flight Crew Training Manual
Initial Climb - One Engine Inoperative
The initial climb attitude should be adjusted to maintain a minimum of V2 and a
positive climb. After liftoff the flight director provides proper pitch guidance.
Cross check indicated airspeed, vertical speed and other flight instruments. The
flight director commands a minimum of V2, or the existing speed up to a
maximum of V2 + 20.
If the flight director is not used, indicated airspeed and attitude become the
primary pitch references.
Retract the landing gear after a positive rate of climb is indicated on the altimeter.
The initial climb attitude should be adjusted to maintain a minimum of V2. If an
engine fails at an airspeed between V2 and V2 + 20, climb at the airspeed at which
the failure occurred. If engine failure occurs above V2 + 20, increase pitch to
reduce airspeed to V2 + 20 and maintain until flap retraction altitude.
The flight director roll mode commands wings level or HDG SEL (as installed)
after liftoff until LNAV engagement or another roll mode is selected. If ground
track is not consistent with desired flight path, use HDG SEL/LNAV to achieve
the desired track.
Indications of an engine fire, impending engine breakup or approaching or
exceeding engine limits, should be dealt with as soon as possible. Accomplish the
appropriate recall checklist items as soon as the airplane is under control, the gear
has been retracted and a safe altitude (typically 400 feet AGL or above) has been
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