TM 55-1510-219-10
CAUTION
Do not pull out of the resulting
dive too abruptly as this could
cause excessive wing loads
and a possible secondary stall.
5.
Pull out of dive by exerting a smooth, steady
back pressure on the control wheel, avoiding
an accelerated stall and excessive aircraft
stresses.
8-51. DIVING.
Maximum diving airspeed (red line) is 245
KIAS or 0. 47 Mach. Flight characteristics are
conventional throughout a dive maneuver; however,
caution should be used if rough air is encountered
after maximum allowable dive speed has been
reached, since it is difficult to reduce speed in dive
configuration. Dive recovery should be very gentle
to avoid excessive aircraft stresses.
8-52. MANEUVERING FLIGHT.
The maximum speed (Va) at which abrupt
full control inputs can be applied without exceeding
the design load factor of the aircraft (Va 170 KIAS is
shown in Chapter 5). The data is based on 14,200
pounds. There are no unusual characteristics under
accelerated flight.
Section V. ADVERSE ENVIRONMENTAL CONDITIONS
8-53. INTRODUCTION.
The purpose of this part is to inform the pilot
of the special precautions and procedures to be
followed during the various weather conditions that
may be encountered in flight. This part is primarily
narrative, only those checklists that cover specific
procedures characteristic of weather operations are
included. The checklist in Section II provides for
adverse environmental operations.
8-54. COLD WEATHER OPERATIONS.
Operational difficulties maybe encountered
during extremely cold weather, unless proper steps
are taken prior to or immediately after flight. All
personnel should understand and be fully aware of
the necessary procedures and precautions involved.
a.
Preparation For Flight. Accumulations of
snow, ice, or frost on aircraft surfaces will adversely
affect takeoff distance, climb performance and stall
speeds to a dangerous degree. Such accumulations
must be removed before flight. In addition to the
normal exterior checks, following the removal of ice,
snow, or frost, inspect wing and empennage surfaces
to verify that these remain sufficiently cleared. Also,
move all control surfaces to confirm full freedom of
movement. Assure that tires are not frozen to wheel
chocks or to the ground. Use ground heaters, antiice
solution, or brake deice to free frozen tires. When
heat is applied to release tires, the temperature
should not exceed 71°C (160°F). Refer to Chapter 2
for anti-icing, deicing, and defrosting treatment.
b.
Engine Starting. When starting engines on
ramps covered with ice, propeller levers must be in
the FEATHER position to prevent the tires from
sliding. To prevent exceeding torque limits when
advancing CONDITION levers to HIGH IDLE during
the starting procedure, place the . power lever in
BETA and the propeller lever in HIGH RPM before
advancing the condition lever to HIGH IDLE.
c.
Warm-Up and Ground Test. Warm-up
procedures and ground test are the same as those
outlined in Section II.
d.
Taxiing. Whenever possible, taxiing in deep
snow, light weight dry show 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 insure brake assemblies have been
deiced. The condition levers may be returned to
LOW IDLE as soon as the brakes are free of ice.
e.
Before
Takeoff
If icing conditions are
expected, activate all anti-ice systems before
takeoff, allowing sufficient time for the equipment to
become effective.
f.
Takeoff. Takeoff procedures for cold
weather operations are the same as for normal
takeoff. Taking off with temperatures 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
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