TM 55-1510-219-10
wind,
include
the
tailwind
in
landing
distance
computations. Plan the final approach to arrive at 50
feet over the landing area at APPROACH SPEED (Vref)
plus 1/2 wind gust speed. Perform the following
procedures as the aircraft nears the runway.
1.
Autopilot and yaw damp-Disengaged.
2.
Gear down lights-Check.
3.
Propeller levers-HIGH RPM.
8-42. 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 (Vy), retracting flaps fully after attaining the Vref
speed used for the approach. Perform the following
checks:
1.
Power-Maximum allowable.
2.
Gear- UP.
3.
Flaps-UP.
4.
Landing lights-OFF.
5.
Climb power-Set.
6.
Yaw damp-As required.
8-43. AFTER LANDING.
Complete the following procedures after the
aircraft has cleared the runway:
1.
Condition levers-As required.
2.
Engine auto ignition switch-OFF.
3.
Ice and rain switches-OFF.
4.
Flaps-UP.
5.
Avionics-As required.
6.
Lights-As required.
NOTE
Reverse should not be used as a
normal
practice
when
maneuvering
or
parking
the
aircraft.
7.
Mission control panel-Set (DL HV OFF).
8-44. ENGINE SHUTDOWN.
CAUTION
To prevent sustained loads on
rudder shock links, the aircraft
should be parked with the nose
gear centered.
1.
Brake deice-OFF.
2.
Parking brake-Set.
3.
Landing/taxi lights-OFF.
4.
Overhead floodlight-As required.
5.
Cabin temperature mode switch-OFF.
6.
Autofeather switch-OFF.
7.
Vent and aft vent blower switches-AUTO.
8.
INS-OFF.
9.
Mission equipment-OFF, as required.
10.
Inverter switches-OFF.
11.
Battery condition-Check as required.
12.
Avionics master switch-OFF.
13.
TGT-Check. TGT must be 660C or
below for one minute prior to shutdown.
14.
Propeller levers-FEATHER.
CAUTION
Monitor TGT during shutdown. If
sustained
combustion
is
observed, proceed immediately to
ABORT START procedure.
15.
Condition levers-FUEL CUTOFF.
WARNING
Do not turn exterior lights off until
propeller's rotation has stopped.
16.
Exterior lights -OFF.
17.
Master panel lights - OFF.
18.
Master switch - OFF
19.
Keylock switch - OFF.
20.
Oxygen system - As required.
8-19
