TM 1-1520-238-10 7A-48 50 60 70 80 90 M01-264 140 1400 1200 1000 800 1400 1200 1000 800 600 TOTAL FUEL FLOW – LB/HOUR TOTAL FUEL FLOW – LB/HOUR 150 100 30 70 90 80 110 100 50 10 120 100 40 110 90 170 180 0 50 40 20 80 40 20 70 70 20 30 170 130 600 150 140 170 180 160 120 80 70 40 110 100 60 120 90 130 30 60 30 50 60 80 40 60 50 100 30 90 160 CRUISE 140 130 150 160 100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL PRESSURE ALTITUDE - 10,000 FEET AH–64A CRUISE T700–GE–701C AIRSPEED INDICATED KNOTS 10 0 20 D F = 10.0 SQ FT D Q – % D F = 10.0 SQ FT D Q – % FAT=–30C FAT=–20C MAX RANGE MAX RANGE DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988 ^VNE INDICATED TORQUE PER ENGINE ~ % INDICATED TORQUE PER ENGINE ~ % MAX R/C OR MAX END MAX R/C OR MAX END 10 0 20 Figure 7A-14. Cruise Chart, 10,000 Feet, –30 C and –20 C (Sheet 2 of 5)