TM 1-1520-238-10 7A-35 M01-251 180 110 150 130 140 100 160 170 120 1300 1100 90 120 180 150 130 140 100 170 160 110 900 700 1100 900 700 170 110 150 140 160 120 130 90 100 1300 100 60 40 80 10 20 30 50 60 70 30 70 80 60 50 40 20 30 90 40 80 50 TOTAL FUEL FLOW – LB/HOUR 30 70 80 90 70 30 50 60 40 80 90 70 0 100 20 60 50 40 TOTAL FUEL FLOW – LB/HOUR PRESSURE ALTITUDE - 4000 FEET 100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL CRUISE AIRSPEED INDICATED KNOTS 10 0 20 D F = 10.0 SQ FT D Q – % 10 0 20 D F = 10.0 SQ FT D Q – % FAT=+30C FAT=+40C DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988 AH–64A CRUISE T700–GE–701C MAX RANGE MAX RANGE MAX R/C OR MAX END MAX R/C OR MAX END INDICATED TORQUE PER ENGINE ~ % INDICATED TORQUE PER ENGINE ~ % Figure 7A-11. Cruise Chart, 4,000 Feet, +30 C and +40 C (Sheet 5 of 6)