TM 1-1520-238-10 7A-63 M01-279 90 30 100 50 60 40 80 90 70 30 100 50 60 40 80 90 70 140 30 80 130 20 90 70 600 40 50 60 120 110 160 170 140 150 160 120 170 130 100 70 40 20 30 80 60 50 110 0 10 20 30 100 TOTAL FUEL FLOW – LB/HOUR 1000 40 150 70 100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL 90 140 160 PRESSURE ALTITUDE - 16,000 FEET 170 CRUISE 800 1200 1000 110 60 50 130 120 800 TOTAL FUEL FLOW – LB/HOUR 1200 80 600 100 180 150 180 FAT=–20C FAT=–30C MAX RANGE MAX RANGE AH–64A CRUISE T700–GE–701C AIRSPEED INDICATED KNOTS MAX OR R/C MAX END MAX END OR MAX R/C DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988 ^VNE INDICATED TORQUE PER ENGINE ~ % INDICATED TORQUE PER ENGINE ~ % 10 D F = 10.0 SQ FT D Q – % 0 20 10 0 20 D F = 10.0 SQ FT D Q – % Figure 7A-17. Cruise Chart, 16,000 Feet, –30 C and –20 C (Sheet 2 of 4)