TM 1-1510-218-10 8A-19 8A-41.  LANDING. Performance data charts for landing computations assume the runway is paved, level, and dry.    Additional  runway  must  be  allowed  when  these conditions  are  not  met.    Do  not  consider  headwind during landing computations; however, if landing must be downwind,  include  the  tailwind  in  landing  distance computation.  Conduct all landings in accordance with the appropriate ATM.  Perform the following procedure as the aircraft nears the runway. 1.   AP & YD – Disengaged. 2.   GEAR DOWN lights – Check/confirm. 3.   PROP levers – HIGH RPM. 8A-42.  TOUCH AND GO LANDING. The   instructor   should   select   a   point   on   the runway   where   all   pre-takeoff   procedures   will   have been completed prior to the pilot’s initial application of power.      In   selecting   this   point,   prime   consideration shall be given to the required accelerate-stop distance pre-computed on a current Takeoff and Landing Data (TOLD)   card.      The   nose   wheel   should   be   on   the runway    and    rolling    straight    before    the    power    is advanced.  After the pilot applies power to within 5% of the takeoff power, the instructor’s actions are the same as    during    a    normal    takeoff.        Use    the    following procedure. 1.   PROP levers – HIGH RPM. 2.   FLAPS – As required. 3.   Trim – Set. 4.   Power stabilized – Check 27% minimum. 5.   Takeoff power – Set. 8A-43.  GO-AROUND/MISSED APPROACH. Accomplish   the   maneuver   in   accordance   with the appropriate ATM. 1.   Power – As required. 2.   GEAR – UP. 3.   FLAPS – APPROACH. 4.   FLAPS (105 KIAS) – UP. 5.   LANDING/TAXI LIGHTS – OFF. 6.   Climb power – Set. 7.   YAW DAMP – As required. 8.   BRAKE DEICE switch – Off. 8A-44.  AFTER LANDING. Complete   the   following    procedures   after   the landing  rollout  is  complete  and  normal  taxi  speed  is attained. 1.   CONDITION levers – As required. 2.   AUTO IGN – Off. 3.   ICE & RAIN switches – Off. 4.   FLAPS – UP. 5.   XPNDR – As required. 6.   Radar – As required. 7.   Lights – As required. a.   Strobe lights – Off. b.   RECOG – OFF. c.   LANDING/TAXI LIGHTS – As required. 8A-45.  ENGINE SHUTDOWN. NOTE To    prevent    sustained    loads    on    rudder shock  links,  the  aircraft  should  be  parked with the nose gear centered. 1.   BRAKE DEICE switch – Off. 2.   Parking brake – Set. 3.   LANDING/TAXI lights – OFF. 4.   EFIS POWER – OFF. 5.   INVERTERS – OFF. 6.   AUTOFEATHER switch – OFF. 7.   CABIN AIR/TEMP MODE switch – OFF. 8.   VENT  and  AFT  VENT  BLOWER  switch  – AUTO. 9.   BATT  condition  –  Check.    Battery  charge light    should    be    extinguished.        If    it    is illuminated, note loadmeter reading, turn the battery switch off momentarily, and turn the battery  switch  ON  and  wait  approximately 90 seconds.  Turn the battery switch off and note loadmeter reading.  Battery condition is unsatisfactory   if   the   battery   charge   light remains illuminated and charge current fails to decrease between checks. 10.  ITT/TGT – Check.  Must be 750 or below for 1 minute prior to shutdown.