NAVWEPS 00-501-50 
AIRPLANE PERFORMANCE 
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