TM 1-1510-218-10 9-3 b.  Engine     Malfunction     During     and     After Takeoff.    The  action  to  be  taken  in  the  event  of  an engine    malfunction    during    takeoff    depends    upon whether or not decision speed (V₁) has been attained. If an engine fails  immediately after V₁, the takeoff will be   continued   single-engine.      Accurate   performance planning  will  assure  safe  single-engine  performance capability. c.   Engine  Malfunction  Before  V₁  (Abort).   If an engine fails and the aircraft has not accelerated to recommended   decision   speed   (V₁),   retard   POWER levers  immediately  to  IDLE  and  stop  the  aircraft  with brakes  and  if  necessary  reverse  thrust.    Perform  the following: 1.   POWER levers – IDLE. 2.   Braking – As required. d.  Engine Malfunction after V₁. 1.   GEAR (positive climb) – UP. 2.   POWER – As required. 3.   FLAPS (105 KIAS) – UP. IF THE PROP DID NOT FEATHER, PERFORM STEP 4. 4.   PROP (dead engine) – FEATHER. ONCE THE PROP IS FEATHERED, PERFORM STEPS 5 THROUGH 8. 5.   TCAS – Set TA. 6.   LANDING/TAXI LIGHTS – OFF. 7.   BRAKE DEICE – OFF. 8.   Engine cleanup – Perform. NOTE Holding 3 to 5 bank (1/4 to 1/2 ball width) toward  the  operating  engine  will  assist  in maintaining directional control and improving aircraft performance. e.   Engine  Malfunction  During  Flight.    If  an engine  malfunctions  during  flight,  maintain  control  of the   aircraft   while   maintaining   heading   or   turn   as required.    Add  power  as  required  to  keep  airspeed from  decaying  excessively  and  to  maintain   altitude. Identify   the   failed   engine   by   feel   (if   holding   rudder pressure  to  keep  the  aircraft  from  yawing,  the  rudder being pressed indicates the good  engine)  and  engine instruments and confirm identification by retarding the power  lever  of  the  suspected  failed  engine.    Refer  to Chapter 7 for single-engine cruise information.  If one engine malfunctions during flight, perform the following procedure. 1.   Autopilot/yaw damp – Disengage. 2.   POWER – As required. 3.   Dead engine – Identify. 4.   PROP lever (dead engine) – FEATHER. 5.   GEAR – As required. 6.   FLAPS – As required. 7.   TCAS – Set TA. 8.   Power – Set for single-engine cruise. 9.   Engine cleanup – Perform. NOTE At  V₂/V_yse    speeds,  holding  3  to  5  bank (1/2    ball    width)    towards    the    operating engine will assist in maintaining directional control and improving aircraft performance. f.    Engine Malfunction During Final Approach.    If  an  engine  malfunctions  during  final approach, the propeller should not be feathered unless time, distance, and altitude permit or conditions require it.  If time, distance, and altitude are sufficient, perform the    Engine    Malfunction    During    Flight    Procedure. Otherwise    continue    approach    using    the    following procedure. 1.   POWER – As required. 2.   GEAR – DN. g.  Engine  Malfunction  (Second  Engine).    If the second engine fails, do not feather the propeller if an   engine   restart   not   using   the   starter   is   to   be attempted.  Engine restart without starter assist cannot be  accomplished  with  a  feathered  propeller  and  the propeller    will    not    unfeather    without    the    engine's operating.  140  KIAS  is recommended as the best  all around    glide    speed    (considering     engine    restart, distance  covered,  transition  to  landing  configuration, etc.),  although   it  does  not   necessarily   result   in   the O O