TM 1-1510-225-10
8A-25
surfaces of the wing. In the event of windshield icing,
reduce airspeed to 226 knots or below.
h. Descent. Use normal procedures in
Section II. Brake deicing should be considered if
moisture was encountered during previous ground
operations or in flight, in icing conditions with gear
extended.
i. Landing. Landing on an icy runway should
be attempted only when absolutely necessary and
should not be attempted unless the wind is within 10
of runway heading. Application of brakes without
skidding the tires on ice is difficult. In order not to
impair pilot visibility, reverse thrust should be used with
caution when landing on a runway covered with snow
or standing water. Use procedures in Section II for
normal landing.
j. Engine Shutdown. Use normal procedures
in Section II.
k. Before Leaving Aircraft. When the aircraft
is parked outside on ice or in a fluctuating freeze-thaw
temperature condition, the following procedures should
be followed in addition to the normal procedures in
Section II. After wheel chocks are in place, release the
brakes to prevent freezing. Fill fuel tanks to minimize
condensation, remove any accumulation of dirt and ice
from the landing gear shock struts, and install
protective covers to guard against possible collection
of snow and ice.
8A-57. DESERT OPERATION AND HOT WEATHER
OPERATION.
Dust, sand, and high temperatures encountered
during desert operation can sharply reduce the
operational life of the aircraft and its equipment. The
abrasive qualities of dust and sand upon turbine
blades and other moving parts of the aircraft and the
destructive effect of heat upon the aircraft instruments
will necessitate hours of maintenance if basic
preventive measures are not followed. In flight, the
hazards of dust and sand will be difficult to escape,
since dust clouds over a desert may be found at
altitudes up to 10,000 feet. During hot weather
operations, the principal difficulties encountered are
high turbine gas temperatures (ITT) during engine
starting, overheating of brakes, and longer takeoff and
landing rolls due to the higher density altitudes. In
areas where high humidity is encountered, electrical
equipment (such as communication equipment and
instruments) will be subject to malfunction by
corrosion,
fungi,
and
moisture
absorption
by
nonmetallic materials.
a. Preparation for Flight. Check the position of
the aircraft in relation to other aircraft. Propeller sand
blast can damage closely parked aircraft. Check that
the landing gear shock struts are free of dust and
sand. Check the instrument panel and general interior
for dust and sand accumulation. Open main entrance
door and cockpit vent storm windows to ventilate the
aircraft.
CAUTION
N1 speeds of 70% or higher may be
required to keep oil temperatures within
limits.
b. Engine Starting. Use normal procedures in
Section II. Engine starting under conditions of high
ambient temperatures may produce a higher than
normal ITT during the start. The ITT should be closely
monitored when the condition lever is moved to the
LOW IDLE position. If overtemperature tendencies
are encountered, the condition lever should be moved
to
IDLE CUTOFF position periodically during
acceleration of gas generator RPM (N1). Be prepared
to abort the start before temperature limitations are
exceeded.
c. Before Taxi and Engine Runup. Use
normal procedures in Section II. To minimize the
possibility
of
damage
to
the
engines
during
dusty/sandy conditions, activate ice vanes if the
temperature is below +15 °C.
d. Taxiing. Use normal procedures in Section
II. When practical, avoid taxiing over sandy terrain to
minimize propeller damage and engine deterioration
that results from impingement of sand and gravel.
During hot weather operation, use minimum braking
action to prevent brake overheating.
e. Takeoff. Use normal procedures in Section
II. Avoid taking off in the wake of another aircraft if the
runway surface is sandy or dusty.
f. During Flight. Use normal procedures in
Section II.
g. Descent. Use normal procedures in
Section II.
h. Landing. Use normal procedures in
Section II.
i. Engine Shutdown. Use normal procedures
in Section II.