TM 55-1510-220-10
to the pilot's initial application of power. In selecting this
point, prime consideration shall be given to the required
accelerate-stop distance precomputed for the runway in
use. The nosewheel should be on the runway and rolling
straight before the touch-and-go procedures are initiated.
After the pilot applies power to within 5 percent of target,
the copilot's (instructor's) actions are the same as during a
normal takeoff. If touch-and-go landings are approved for
training purposes use the following procedure:
(1.)
Propeller levers - HIGH RPM.
(2.)
Flaps - As required.
(3.)
Trim - Set.
4.
Power stabilized - Check approximately 25%
minimum.
5.
Takeoff power - Set.
8-49. GO-AROUND.
When a go-around is commenced prior to the
LANDING check, use power as required to climb to, or
maintain, the desired altitude and airspeed. If the go-
around is started after the LANDING check has been
performed,
apply
maximum
allowable
power
and
simultaneously increase pitch attitude to stop the descent.
Retract the landing gear after insuring that the aircraft will
not touch the ground. Retract the flaps to APPROACH,
adjusting pitch attitude simultaneously to avoid an altitude
loss. Accelerate to best rate-of-climb airspeed (V
y
),
retracting flaps fully after attaining the (V
ref
) speed used
for the approach. Perform the following:
1.
Power - As required.
2.
Gear- UP.
3.
Flaps - UP.
4.
Landing lights - OFF.
5.
Climb power - Set.
(6.)
Yaw damp - As required.
(7.)
Brake de-ice - OFF.
8-50. AFTER LANDING.
Complete the following procedures after the aircraft
has cleared the runway:
(1.)
Condition levers - As required.
(2.)
Engine autoignition switch - OFF.
(3.)
Ice & rain switches - OFF.
(4.) Flaps- UP.
(5.)
Transponder - As required.
6.
Lights - As required.
(7.)
Mission control panel - Set.
8-51. ENGINE SHUTDOWN.
CAUTlON
To prevent sustained loads on rudder
shock links, the aircraft should be parked
with the nose gear centered.
1.
Brake de-ice - OFF.
2.
Parking brake - Set.
3.
Landing/taxi lights - OFF.
4.
Cabin temperature mode selector switch - OFF.
5.
Autofeather switch - OFF.
6.
Vent and aft vent blower switches - AUTO.
7.
INS - OFF.
8.
Mission equipment - OFF, as required.
9.
Inverter switches - OFF.
10.
Battery condition - Check as required.
11.
TGT - Check. TGT must be 660°C or below for
one minute prior to shutdown.
CAUTlON
Monitor
TGT
during
shutdown.
If
sustained
combustion
is
observed,
proceed immediately to ABORT START
procedure.
12.
Propeller levers - FEATHER.
13.
Condition levers - FUEL CUTOFF.
8-23
