TM 1-1510-225-10 7-6 same  speed.    Use  the  tabular  data  table  at  the  top  of Figure  7-21,  Take-Off  Distance,  Flaps   UP   or   Figure 7-25, Take-Off Distance, Flaps APPROACH. The   takeoff   configuration   for   this   example   is Flaps UP.  The V1/V_r speed is 112 KIAS. Enter  the  speed,  112  KIAS,  in  the  appropriate block on the TOLD card. (11)    V2 / V_yse.  Use the tabular data table at the top of Figure 7-31, Climb – One Engine Inoperative. In accordance with the ATM, flaps are retracted just after liftoff at 105 KIAS for both a normal takeoff and in the event   of   an   engine   failure   after   V₁.      The   CLIMB SPEED   V₂   -   KNOTS,   Figure   7-31,   is   V_yse   and   is essentially  the  same  speed  as  V₂   for   a   takeoff   with flaps at 0%.  Consequently, V₂  flaps  0%  and  V_yse  are used as the V₂ speed for entry on the TOLD card.  V2 / V_yse for a 12,600 pound aircraft is 122 KIAS. Enter  the  speed  in  the  appropriate  block  on  the TOLD card. (11A) If     conducting     an     obstacle     clearance climb,    use    the    “Vx”    speed    from    the    TAKEOFF DISTANCE – FLAPS APPROACH chart. (12)    Climb    Gradient    Altitude.        This    is    the altitude to which the single engine climb gradient must be  continued  as  specified  in  the  applicable  DP.    The information  is  advisory  and  intended  as  a  reminder  to the crew of the altitude to which they must climb at V2 / V_yse in order to clear obstacles. For  this  example,  the  DP  specified  climbing  to 5000 feet MSL. Enter  the  altitude,  5000  feet,  in  the  appropriate block on the TOLD card. NOTE Items  13  through  17  are  initially  calculated at  takeoff  weight  as  a  contingency  for  a necessary return to the takeoff airport right after   departure.      The   items   must   be   re- calculated for the arrival at the destination. (13)    Runway   Length   Available.      This   is   the runway length available for landing. For this example, the runway length is 6000 feet and     there     is     no     displaced     threshold     or     other information  limiting  the  useful  landing  distance  of  the runway. Enter  the  length,  6000  feet,  in  the  appropriate block on the TOLD card. (14)    Landing  Weight.    For  the  takeoff  TOLD card,  landing  and  takeoff  weights  are  the  same.    For arrival  at  the  destination  the  TOLD  card  must  be  re- calculated  to  reflect  actual  aircraft  weight  and  airport conditions. For  this  example,  takeoff  and  landing  weight  is 12,600 pounds. Enter     the     weight,     12,600     pounds,     in     the appropriate block on the TOLD card. (15)    V_ref  Speed.  This speed is 1.3 times V_so at the   intended   landing   weight   if   the   landing   will   be accomplished  using  Flaps  DN.    If  the  landing  will  be accomplished  with  the  Flaps  at  APPROACH,  or  any setting greater than APPROACH but less than  DOWN, then  V_ref  is  1.3  times  V_s1  (the  stall  speed  for  FLAPS APPROACH).  Use Figure 7-13, Stall Speeds – Power Idle to determine applicable stall speeds. For  this  example,  the  landing  weight  (assuming an    emergency    return    to    the    departure    airport)    is 12,600  pounds  a  landing  with  the  Flaps    DOWN   is planned.      The   V_so   for   a   12,600-pound   aircraft   is 75 KIAS.  Therefore, V_ref is 1.3 times 75 = 97.5 and is rounded up to 98 KIAS. There  is  another  method  to  determine  V_ref   when the    landing    will    be    accomplished    with    the    Flaps DOWN.        Subtract    5    KIAS    from    the    APPROACH SPEED ~ KNOTS obtained from the tabular data table at  the  top  of  Figure  7-107,  Landing  Distance  Without Propeller Reversing, Flaps DOWN. For a 12,600-pound  aircraft,  the  given  APPROACH  SPEED is 103 KIAS – 5 KIAS = 98 KIAS. NOTE If  the  aircraft  will  be  landed  with  FLAPS less than full DOWN, the LANDING DISTANCE-   FLAPS   UP   (Figure   7-108   or 7-110)  must  be  used  to  obtain  the  landing distance for the TOLD card As  another  example,  if  the  landing  was  planned using  the  Flaps  at   APPROACH,  or  any  intermediate setting short of   DOWN,  then  the  V_ref  speed  would  be 1.3  times   V_s1  (the   FLAPS   APPROACH   stall   speed). FLAPS  APPROACH  stall  speed  for  a  12,600  pound aircraft  is  85  KIAS.    Therefore,  the  V_ref   speed  is  1.3 times 85 = 110.5 and is rounded up to 111 KIAS. For this example with Flaps DOWN enter the V_ref speed, 98 KIAS at the appropriate place on the TOLD