FUEL  FLOW  I  APPLICABLE FOR A  PARTICULAR: WEIGHT  MAXIMUM  ALTITUDE  ENDURANCE  CONFIGURATION  LINE FROM ORIGIN  TANGENT TO CURVE  VELOCITY, KNOTS  100%  MAXIMUM  --  99% MAXIMUM RANGE  SPECIFIC  RANGE  APPLICABLE FOR A PARTICLAR  -CONFIGURATION  -ALTITUDE  -WEIGHT  VELOCITY, KNOTS  AREA REPRESENTS  Figure 2.23. Geneml Range Performance  159  NAVWEPS 00-501-50  AIRPLANE PERFORMANCE 