TM 1-1510-224-10 8-31.  BEFORE LANDING. 1. PROP SYN switch - As required. 2. PROP levers - As required. 3. Flaps (below 197 KIAS) -  APPROACH. 4. Gear (below 179 KIAS) - DN 5. LANDING LIGHTS switch - As required. (6) AUTOFEATHER switch - ARM. (7) ICE    VANE    CONTROL    switches    -    As required. (8) BRAKE deice - As required. (9) WOW OVERRIDE switch - OFF. (10) ANT  STOWED  annunciator  light  -  Check illuminated. 8-32.  LANDING. CAUTION The maximum demonstrated crosswind  component  is  20  knots  at 900.    Landing  the  aircraft  in  a  crab will impose side loads on the landing gear  and  should  be  recorded  on  DA Form 2408-13-1. a. Normal    Landing.          Refer     to     Chapter     7     for performance data.  When landing is assured: 1. Autopilot and yaw damper Disengage. 2. GEAR DOWN annunciators Check. 3. PROP levers HIGH RPM. b. Crosswind   Landing.      Refer   to   Chapter   7   for recommended  V_ref     speed.    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 crosswind effect. For crosswind 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/stop  and  go  landing  is  to be performed, the following procedures shall be used: (1) PROP 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,  retract  the flaps  to  APPROACH,  and  simultaneously  increase  pitch attitude  to  stop  the  descent.    Retract  the  landing  gear after  ensuring  that  the  aircraft  will  not  touch  the  ground. Accelerate to two engine climb airspeed, retracting flaps fully after attaining Vref 1. Power - Maximum allowable. 2. Gear - UP. 3. Flaps - UP. 4. LANDING LIGHTS switch - 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. PROP levers - Retard to  FEATHER detent (2) ICE VANE CONTROL switches - ON. (3) Engine AUTO IGNITION switches - Off. (4) ICE & RAIN switches - Off. 5. Flaps - UP. (6) Radar/transponder - As required. 7. Lights - As required. (8) Mission control panel - Set as follows: a. RADIO ALT switch - OFF. b. MISSION CONTROL ORIDE switch - OFF. c. ELINT/COMINT   switches   (2)   -   As required. d. ASE SILENT switch - OFF. 8-24