TM 1-1510-225-10
8-27
indicator. Maintain original heading. Make no turns
unless absolutely necessary.
8-59. ICE AND RAIN (TYPICAL).
While in icing conditions, if there is an
unexplained 30% increase of torque
needed to maintain airspeed in level flight,
a cumulative total of 2 or more inches of
ice
accumulation
on
the
wing,
an
unexplained decrease of 15 KIAS, or an
unexplained deviation between pilot's and
copilot's airspeed indicators, the icing
environment should be exited as soon as
practicable. Ice accumulation on the pitot
tube assemblies could cause a complete
loss of airspeed indication.
The following conditions indicate a possible
accumulation of ice on the pilot tube assemblies and
unprotected aircraft surfaces. If any of the following
conditions are observed, the icing environment should
be exited as soon as practicable:
1. Total ice accumulation of 2 inches or more
on the wing surfaces. Determination of ice
thickness
can
be
accomplished
by
summing the estimated ice thickness on
the wing prior to each pneumatic boot
deice cycle (e.g., four cycles of minimum
recommended 1/2 inch accumulation).
2. A 30% increase in torque per engine
required to maintain desired airspeed in
level flight (not to exceed 85% torque)
when
operating
at
recommended
holding/loiter speed.
3. A decrease in indicated airspeed of
15 knots after entering the icing condition
(not slower than 1.4 times the power off
stall speed) if maintaining original power
setting in level flight. This can be
determined
by
comparing
pre-icing
condition entry speed to the indicated
speed after a surface deice cycle is
completed.
4. Any variations from normal indicated
airspeed between the pilot's and copilot's
airspeed indicators.
a. Typical Icing. Icing occurs because of
supercooled water vapor such as fog, clouds, or rain.
The most severe icing occurs on aircraft surfaces in
visible moisture or precipitation with a true outside air
temperature between 5 °C and +1 °C. However,
under some circumstances, dangerous icing conditions
may be encountered with temperatures below 10 °C.
The surface of the aircraft must be at a temperature of
freezing or below for ice to stick. If severe icing
conditions are encountered, ascend or descend to
altitudes where these conditions do not prevail. If flight
into icing conditions is unavoidable, proper use of
aircraft anti-icing and deicing systems may minimize
the problems encountered. Approximately 15 minutes
prior to flight into temperature conditions which could
produce frost or icing conditions, the pilot and copilot
windshield anti-ice switches should be set at NORMAL
or HIGH temperature position (after preheating) as
necessary to eliminate windshield ice. Stalling
airspeeds should be expected to increase when ice
has accumulated on the aircraft causing distortion of
the wing airfoil. For the same reason, stall warning
devices are not accurate and should not be relied
upon. Keep a comfortable margin of airspeed above
the normal stall airspeed with ice on the aircraft.
Maintain a minimum of 140 knots during sustained
icing conditions to prevent ice accumulation on
unprotected surfaces of the wing. In the event of
windshield icing, reduce airspeed to 226 knots or
below.
b. Rain. Rain presents no particular problems
other than slippery runways, restricted visibility, and
occasional incorrect airspeed indications.
c. Taxiing. Extreme care must be exercised
when taxiing on ice or slippery runways. Excessive
use of either brakes or power may result in an
uncontrollable skid.
d. Takeoff. Extreme care must be exercised
during takeoff from ice or slippery runways. Excessive
use of either brakes or power may result in an
uncontrollable skid.
e. Climb. Keep aircraft attitude as flat as
possible and climb with higher airspeed than usual, so
that the lower surfaces of the aircraft will not be iced by
flight at a high angle of attack.
f. Cruise Flight. Prevention of ice formation is
far more effective and satisfactory than attempts to
dislodge the ice after it has formed. If icing conditions
are inadvertently encountered, turn on the anti-icing
systems prior to the first sign of ice formation. Do not
operate deicer boots continuously. Allow at least 1/2
inch of ice on the wing deicer boots before activating
the deicer boots. Continued flight in severe icing
conditions should not be attempted. If ice forms on the
wing area aft of the deicer boots, climb or descend to
an altitude where conditions are less severe.
WARNING