TM 55-1550-222-10
d
Taxiing. Whenever possible, taxiing in deep
snow, light weight dry snow or slush should be avoided,
particularly in colder FAT conditions. If it is necessary
to taxi through snow or slush, do not set the parking
brake when stopped. If possible, do not park the aircraft
in snow or slush deep enough to reach the brake
assemblies. Chocks or sandbags should be used to
prevent the aircraft from rolling while parked. Before
attempting to taxi, activate the brake deice system,
insuring that the bleed air valves are OPEN and that the
condition levers are in HIGH IDLE. An outside observer
should visually check wheel rotation to ensure brake
assemblies have been deiced.
e.
Before Takeoff.
1.
If icing conditions are expected, activate all anti-
ice systems before takeoff, allowing sufficient time for
the equipment to become effective.
2.
If the possibility of ice accumulation on the
horizontal stabilizer or elevator exists, takeoff will not be
attempted.
f
Takeoff. Takeoff procedures for cold weather
operations are the same as for normal takeoff. Taking
off with temperature at or below freezing, with water,
slush or snow on the runway, can cause ice to
accumulate on the landing gear and can throw ice into
the wheel well areas. Such takeoffs shall be made with
brake deice on and with the ice vanes extended. Before
flight into icing conditions, the pilot and copilot
windshield anti-ice switches should be set at NORMAL
position.
g.
During Flight
1.
After takeoff from a runway covered with snow
or slush, it may be advisable to leave brake deice ON to
dislodge ice accumulated from the spray of slush or
water. Monitor BRAKE DEICE annunciator for
automatic termination of system operation and then turn
the switch OFF. During flight, trim tabs and controls
should also be exercised periodically to prevent
freezing. Ensure that anti-icing systems are activated
before entering icing conditions. Do not activate the
surface deice system until ice has accumulated at least
0.5 INCH. The propeller deice system operates
effectively as an anti-ice system and it may be operated
continuously in flight. If propeller imbalance due to ice
does occur, it may be relieved by increasing RPM
briefly, then returning to desired setting. Ice vanes must
be extended when operating in visible moisture or when
freedom from visible moisture cannot be assured, at +
5°C FAT or less. Ice vanes are designed as an anti-ice
system, not a deice system. After the engine air inlet
screens are blocked, lowering the ice vanes will not
rectify the condition.
2.
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. 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.
h.
Descent. Use normal procedures in Section II.
Brake icing 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 very difficult, due to the sensitive brakes. 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 the 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.
8-53. 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
8-23