TM 55-1510-222-10
a.
Normal Landing. Refer to Chapter 7 for
performance data. When landing is assured:
1.
Autopilot and yaw damp Disengaged.
2.
GEAR DOWN annunciators Check.
3.
Flaps As required. After touchdown:
4.
Power levers Lift and retard to GROUND FINE.
5.
Brakes As required.
b.
Cross wind Landing. Refer to Chapter 7 for
recommended Vref speeds. Use the "crab-into-the-
wind" method to correct for drift during final approach.
The "crab" is changed to a slip (aileron into wind and top
rudder) to correct for drift during flare and touchdown.
After landing, position ailerons as required to correct for
cross wind effect. For cross wind exceeding the
published limits, a combination "slip and crab" method
at touchdown should be used.
c.
Soft Field Landing. Not applicable.
8-33. TOUCH-AND GO/STOP-AND GO LANDING.
When a touch and go landing is to be performed, the
following procedures shall be used:
1.
Propeller levers HIGH RPM.
2.
Flaps As required.
3.
Trim Set.
4.
Power stabilized Check 25% minimum.
5.
Takeoff power Set.
8-34. 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 ensuring that the aircraft will not touch
the ground. Retract the flamps to APPROACH,
adjusting pitch attitude simultaneously to avoid an
altitude loss. Accelerate to two engine rate-of-climb
airspeed retracting flaps fully after attaining Vref speed
used for the approach. Perform the following.
1.
Power Maximum allowable.
2.
Gear-UP.
3.
Flaps UP.
4.
Landing lights OFF.
5.
Climb power Set.
6.
Brake deice Off.
8-35. AFTER LANDING.
Complete the following procedures after the aircraft has
cleared the runway:
1.
Conditions levers HIGH IDLE.
2.
Propeller levers Retard to feather detent.
3.
Ice vane control switches ON.
4.
Engine auto ignition switches Off.
5.
Ice & rain switches -Off.
6.
Flaps UP.
7.
Radar/transponder As required.
8.
Lights As required.
9.
Mission control panel Set.
8-36. ENGINE SHUTDOWN.
NOTE
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 light OFF.
4.
Cabin air mode switch OFF.
5.
Autofeather switch OFF.
6.
Forward vent and afl. vent blower switches
AUTO.
7.
INS OFF.
Change 1 8-18
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