TYPICAL PROPELLER  AIRCRAFT  ALTlTUOE PERFORMANCE  .  RATE OF,CL!MB_,  _-  .  tiAXlMUM LEVEL FLIGHT SPEED  HIGH BLOWER  CRITICAL ALTITUDE  FEE0 FOR MA% R c  LOW BLOWER  CRITICAL ALTITUDE  = y$y  VELOCITY, KNOTS  -e-*--  TROPOPAUSE  t-  \  MAXIMUM LEVEL  \  \  FLIGHT SPEED  -RATE  OF CLIMB  \  \  \  \  I  I  I  I  b  -8  VELOCITY, KNOTS  POWER OFF DESCENT PERFORMANCE  POWER  REQUIRED  HP  MINIMUM POWER REP ’ D  I  VELOCITY, KNOTS  Figure UP,  Climb ad Desceni Pedormome  lS7  NAVWEPS C&801-80  AIRPLANE PERFORMANCE 