TEST RUN DC9     (03/10/93) Feb 28 97 ch



<<<<<<<<<<<<<<<<<<<<<<<<<<<<<<< CASE INPUT DATA >>>>>>>>>>>>>>>>>>>>>>>>>>>>>

     Gravitational accel. (g)=       32.174(ft/s^2)
     Air density at takeoff  =        0.002(sl/ft^3
     Aircraft weight      (W)=    95000.000   (lbs)
     Aircraft wing area   (S)=     1000.000(ft/s^2)
     Max lift coeff   (CLmax)=        2.000(nondim)
     Ground lift coeff(CLgrd)=        0.300(nondim)
     Air lift coeff   (CLair)=        1.650(nondim)
     Ground drag coeff(CDgrd)=        0.080(nondim)
     Air drag coeff   (CDair)=        0.121(nondim)
     Roll frict coeff (MUgrd)=        0.025(nondim)
     Brake frict coeff(MUbrk)=        0.300(nondim)
     Angle of thrust (LAMBDA)=        0.000   (deg)
     Stall margin         (k)=        1.100(ft/s^2)
     Descision time    (TIME)=        3.000   (sec)
     Obstacle height  (OBSHT)=       35.000    (ft)
     EI pwr remaining (PLOSS)=        0.500 (fract)

THRUST =  31450.000 +    -17.263*V +      0.025*V^2



<<<<<<<<<<<<<<<<<<<<<<<<<<<<< NORMAL TAKEOFF DATA >>>>>>>>>>>>>>>>>>>>>>>>>
Time (s)      X-Dist (ft)      X-Vel (ft/s)   Y-Dist (ft)      Y-Vel (ft/s)
  0.000           0.000            0.000            0.000            0.000       
  1.000           4.914            9.818            0.000            0.000       
  2.000          19.615           19.574            0.000            0.000       
  3.000          44.040           29.265            0.000            0.000       
  4.000          78.123           38.889            0.000            0.000       
  5.000         121.794           48.441            0.000            0.000       
  6.000         174.980           57.918            0.000            0.000       
  7.000         237.604           67.318            0.000            0.000       
  8.000         309.588           76.636            0.000            0.000       
  9.000         390.849           85.871            0.000            0.000       
 10.000         481.301           95.020            0.000            0.000       
 11.000         580.858          104.079            0.000            0.000       
 12.000         689.429          113.047            0.000            0.000       
 13.000         806.921          121.921            0.000            0.000       
 14.000         933.239          130.699            0.000            0.000       
 15.000        1068.286          139.378            0.000            0.000       
 16.000        1211.962          147.958            0.000            0.000       
 17.000        1364.167          156.435            0.000            0.000       
 18.000        1524.798          164.808            0.000            0.000       
 19.000        1693.749          173.076            0.000            0.000       
 20.000        1870.915          181.237            0.000            0.000       
 21.000        2056.187          189.290            0.000            0.000       
 22.000        2249.458          197.233            0.000            0.000       
 23.000        2450.617          205.066            0.000            0.000       
 24.000        2659.553          212.787            0.000            0.000       
 24.936        2862.368          219.912            0.000            0.000       
 27.936        3555.614          242.080            0.000            0.000       
 28.000        3571.036          242.515            0.014            0.434       
 29.000        3816.720          248.600            4.282            8.473       
 30.000        4067.677          252.999           17.637           18.540       
 30.716        4249.870          254.707           35.000           26.859       

<<<<<<<<<<<<<<<<<<<<<<<<<< NORMAL TAKEOFF SUMMARY >>>>>>>>>>>>>>>>>>>>>>

     Rotation Velocity   (Vr)=      219.912  (ft/s)
     Liftoff Velocity   (Vlo)=      242.079  (ft/s)
     Velocity over obs.(Vobs)=      256.118  (ft/s)
     Rotation Distance   (Xr)=     2862.368    (ft)
     Liftoff Distance   (Xlo)=     3555.614    (ft)
     Distance to obst. (Xobs)=     4249.870    (ft)
     Rotation Time       (Tr)=       24.936     (s)
     Liftoff Time       (Tlo)=       27.936     (s)
     Time to obst.     (Tobs)=       30.716     (s)

     TOTAL TAKEOFF DIST (Xto)=     4249.870    (ft)
     TOTAL TAKEOFF TIME (Tto)=       30.716     (s)


<<<<<<<<<<<<<<<<<<<<<<<<<< OEI TAKEOFF SUMMARY >>>>>>>>>>>>>>>>>>>>>>

 Critical Velocity   (Vcrit) =      203.829  (ft/s)
 Decision Velocity      (V1) =      212.327  (ft/s)
 Velocity over obs.   (Vobs) =      256.118  (ft/s)
 Critical Distance   (Xcrit) =     2418.154    (ft)
 Decision Distance      (X1) =     3042.475    (ft)
 Balanced Field Length (BFL) =     5399.447    (ft)
 Critical Time       (Tcrit) =       22.841     (s)
 Decision Time          (T1) =       25.841     (s)
 OEI Takeoff Time     (TBFL) =       48.333     (s)