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deviation from the reference weight at checkpoint as required by entering the off
reference fuel corrections table with the fuel required for the reference weight and
the actual weight at checkpoint. Read fuel and time required for the actual weight.
Holding
Single engine holding data is provided in the same format as the all engine holding
data and is based on the same assumptions.
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Introduction . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . .MAN.05
General . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.05.1
Non-Normal Maneuvers . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.05.1
Flight Patterns . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . . MAN.05.1
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MAN.05 Maneuvers-Introduction
Introduction General
Non-Normal Maneuvers and Flight Patterns are included for training and
review purposes.
Non-Normal Maneuvers
Flight crews are expected to do non-normal maneuvers from memory.
Flight Patterns
Flight patterns show procedures for some all-engine and
engine-inoperative situations.
Flight patterns do not include all procedural items but show
required/recommended:
• configuration changes
• thrust changes
• Mode Control Panel (MCP) changes
• pitch mode and roll mode changes
• checklist calls.
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D632W001-TBC MAN.1.1
MAN.1 Maneuvers-Non_Normal Maneuvers Approach to Stall Recovery
The following is immediately accomplished at the first indication of stall
buffet or stick shaker.
Note: *At high altitudes it may be necessary to decrease pitch attitude
below the horizon to achieve acceleration.
Rejected Takeoff
The captain has the sole responsibility for the decision to reject the takeoff.
The decision must be made in time to start the rejected takeoff maneuver
by V1. If the decision is to reject the takeoff, the captain must clearly
announce “REJECT,” immediately start the rejected takeoff maneuver, and
assume control of the airplane. If the first officer is making the takeoff, the
first officer must maintain control of the airplane until the captain makes a
positive input to the controls.
Prior to 80 knots, the takeoff should be rejected for any of the following:
• activation of the master caution system
• system failure(s)
• unusual noise or vibration
• tire failure
• abnormally slow acceleration
• unsafe takeoff configuration warning
• fire or fire warning
Pilot Flying Pilot Monitoring
• Advance the thrust levers to maximum
thrust.
• Smoothly adjust the pitch attitude* to
avoid ground contact or obstacles.
• Level the wings (do not change flaps or
landing gear configuration).
• Retract the speedbrakes.
• Verify maximum
thrust.
• Monitor altitude and
airspeed.
• Call out any trend
toward terrain contact.
• Verify all required
actions have been
completed and call out
any omissions.
When ground contact is no longer a factor:
• Adjust the pitch attitude to accelerate
while minimizing altitude loss.
• Return to a speed appropriate for the
configuration.
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