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Engine
Failure After Takeoff
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Flying Handbook Menu > Emergency Procedures > Engine Failure After Takeoff
The altitude available is, in many ways, the
controlling factor in the successful accomplishment of an emergency
landing. If an actual engine failure should occur immediately
after takeoff and before a safe maneuvering altitude is attained,
it is usually inadvisable to attempt to turn back to the field
from where the takeoff was made. Instead, it is safer to immediately
establish the proper glide attitude, and select a field directly
ahead or slightly to either side of the takeoff path.
The decision to continue straight ahead is
often difficult to make unless the problems involved in attempting
to turn back are seriously considered. In the first place, the
takeoff was in all probability made into the wind. To get back
to the takeoff field, a downwind turn must be made. This increases
the groundspeed and rushes the pilot even more in the performance
of procedures and in planning the landing approach. Secondly,
the airplane will be losing considerable altitude during the
turn and might still be in a bank when the ground is contacted,
resulting in the airplane cartwheeling (which would be a catastrophe
for the occupants, as well as the airplane). After turning downwind,
the apparent increase in groundspeed could mislead the pilot
into attempting to prematurely slow down the airplane and cause
it to stall. On the other hand, continuing straight ahead or
making a slight turn allows the pilot more time to establish
a safe landing attitude, and the landing can be made as slowly
as possible, but more importantly, the airplane can be landed
while under control.
Concerning the subject of turning back to the
runway following an engine failure on takeoff, the pilot should
determine the minimum altitude an attempt of such a maneuver
should be made in a particular airplane. Experimentation at
a safe altitude should give the pilot an approximation of height
lost in a descending 180° turn at idle power. By adding
a safety factor of about 25 percent, the pilot should arrive
at a practical decision height. The ability to make a 180°
turn does not necessarily mean that the departure runway can
be reached in a power-off glide; this depends on the wind, the
distance traveled during the climb, the height reached, and
the glide distance of the airplane without power. The pilot
should also remember that a turn back to the departure runway
may in fact require more than a 180° change in direction.
Consider the following example of an airplane
which has taken off and climbed to an altitude of 300 feet AGL
when the engine fails. [figure16-5 on next page]. After a typical
4 second reaction time, the pilot elects to turn back to the
runway. Using a standard rate (3° change in direction per
second) turn, it will take 1 minute to turn 180°. At a glide
speed of 65 knots, the radius of the turn is 2,100 feet, so
at the completion of the turn, the airplane will be 4,200 feet
to one side of
the runway. The pilot must turn another 45° to head the
airplane toward the runway. By this time the total change in
direction is 225° equating to 75 seconds plus the 4 second
reaction time. If the airplane in a poweroff glide descends
at approximately 1,000 f.p.m., it In airplanes with piston engines,
prolonged practice of emergency descents should be avoided to
prevent excessive cooling of the engine cylinders.

figure16-5. Turning back to the runway
after engine failure.
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