Aeronautical Information Manual (AIM), page 520
AIM 12/10/15
2. Counter control is usually effective and wake location and thereby take avoidance precau-
induced roll minimal in cases where the wingspan tions.
and ailerons of the encountering aircraft extend
beyond the rotational flow field of the vortex. It is 1. An aircraft generates vortices from the
more difficult for aircraft with short wingspan moment it rotates on takeoff to touchdown, since
(relative to the generating aircraft) to counter the trailing vortices are a by-product of wing lift. Prior to
imposed roll induced by vortex flow. Pilots of short takeoff or touchdown pilots should note the rotation
span aircraft, even of the high performance type, must or touchdown point of the preceding aircraft. (See
be especially alert to vortex encounters. FIG 7-3-3.)
(See FIG 7-3-2.) 2. The vortex circulation is outward, upward
and around the wing tips when viewed from either
FIG 7-3-2 ahead or behind the aircraft. Tests with large aircraft
Wake Encounter Counter Control have shown that the vortices remain spaced a bit less
than a wingspan apart, drifting with the wind, at
altitudes greater than a wingspan from the ground. In
COUNTER
CONTROL
view of this, if persistent vortex turbulence is
encountered, a slight change of altitude and lateral
position (preferably upwind) will provide a flight
path clear of the turbulence.
3. Flight tests have shown that the vortices from
larger (transport category) aircraft sink at a rate of
several hundred feet per minute, slowing their
descent and diminishing in strength with time and
distance behind the generating aircraft. Atmospheric
turbulence hastens breakup. Pilots should fly at or
above the preceding aircraft's flight path, altering
course as necessary to avoid the area behind and
3. The wake of larger aircraft requires the below the generating aircraft. (See FIG 7-3-4.)
respect of all pilots. However, vertical separation of 1,000 feet may be
considered safe.
7-3-4. Vortex Behavior 4. When the vortices of larger aircraft sink close
to the ground (within 100 to 200 feet), they tend to
a. Trailing vortices have certain behavioral move laterally over the ground at a speed of 2 or
characteristics which can help a pilot visualize the 3 knots. (See FIG 7-3-5.)
FIG 7-3-3
Wake Ends/Wake Begins
Touchdown Rotation
Wake Ends Wake Begins
7-3-2 Wake Turbulence
Page 520 of the Aeronautical Information Manual (AIM.pdf)
AIM: Official Guide to Basic Flight Information and ATC Procedures