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VR
15 ft
V2
35 ft
V2
V1
VR
Available Runway (DRY)
Available Runway (WET)
Effect of using wet runway performance
Effect of using dry runway performance
Effect of blown tire
Effect of less than maximum
braking effort, engine-out
RTO, 3/4 brake pressure +
S/B + 1 Thrust Reverser
all engine RTO,
2 Thrust Reversers
(limit weight and V1) on a wet runway
engine-out RTO,
Brakes + S/B +
1 Thrust Reverser
(reduced V1 and GW)
engine-out RTO,
Brakes + S/B +
1 Thrust Reverser
Brakes + S/B +
October 31, 2004
767 Flight Crew Training Manual
Takeoff and Initial Climb
Copyright © The Boeing Company. See title page for details.
FCT 767 (TM) 3.23
Initial Climb - All Engines
After liftoff use the flight director as the primary pitch reference cross checking
indicated airspeed and other flight instruments. If the flight director is not used,
indicated airspeed and attitude become the primary pitch references.
After liftoff, the flight director commands pitch to maintain an airspeed of V2 +
15 to 25 knots until another pitch mode is engaged.
V2 + 15 is the optimum climb speed with takeoff flaps. It results in the maximum
altitude gain in the shortest distance from takeoff. Acceleration to higher speeds
reduces the altitude gain. If airspeed exceeds V2 + 15 during the initial climb, stop
the acceleration but do not attempt to reduce airspeed to V2 + 15. Any speed
between V2 + 15 and V2 + 25 knots results in approximately the same takeoff
profile. Crosscheck indicated airspeed for proper initial climb speed.
Retract the landing gear after a positive rate of climb is indicated on the altimeter.
Do not apply brakes after becoming airborne. Braking is automatically applied
when the landing gear lever is placed in the up position. After gear and flaps are
retracted, the PM should verify the gear and flaps indications are normal.
Minimum Fuel Operation - Takeoff
The minimum fuel recommended for takeoff is trip fuel plus reserves. On very
short flights this fuel quantity may not be enough to prevent forward fuel pump
low pressure lights from illuminating after takeoff.
If any main tank fuel pump indicates low pressure do not turn off fuel pump
switches. Avoid rapid acceleration of the airplane, reduce nose-up body attitude
and maintain minimum nose-up body angle required for a safe climb gradient.
Immediate Turn after Takeoff - All Engines
Obstacle clearance, noise abatement, or departure procedures may require an
immediate turn after takeoff. Initiate the turn at the appropriate altitude (normally
at least 400 feet AGL) and maintain V2 + 15 to V2 + 25 with takeoff flaps.
Note: A maximum bank angle of 30° is permitted at V2 + 15 knots with takeoff
flaps.
After completing the turn, and at or above flap retraction altitude, accelerate and
retract flaps while climbing.
Note: The possibility of an engine failure along the departure track must be
considered. Special engine out procedures, if available, are preferable to a
takeoff weight reduction to ensure all obstacles are cleared.
October 31, 2004
767 Flight Crew Training Manual
Takeoff and Initial Climb
Copyright © The Boeing Company. See title page for details.
3.24 FCT 767 (TM)
Roll Modes
After takeoff and climb is stabilized, select LNAV after passing 400 feet AGL. If
the departure procedure or route does not begin at the end of the runway, it may
be necessary to use the HDG SEL mode at 400 feet AGL to intercept the desired
track for LNAV capture. When the departure procedure is not a part of the active
flight plan, use HDG SEL or HDG HOLD mode. When an immediate turn after
takeoff is necessary, the desired heading may be preset before takeoff.
Note: On Pegasus and PIP FMC equipped airplanes, LNAV may be armed before
takeoff and engages automatically at 50 feet.
767-200, 767-300
Navaids and appropriate radials or tracks required for use during the departure
may be displayed on the navigation display using the FIX page feature. Use of the
STA and WPT switches on the EFIS control panel provides additional information
on the map display.
767-400
Navaids and appropriate radials or tracks required for use during the departure
may be displayed on the navigation display using the FIX page feature and/or
VOR/ADF switches on the EFIS control panel. Use of the STA and WPT switches
on the EFIS control panel provides additional information on the navigation
display.
Autopilot Engagement
The autopilot is FAA certified to allow engagement at or above 200 feet AGL after
　
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