TM 1-1520-238-10 7A-53 M01-269 600 1000 800 1400 1200 1200 1000 800 600 1400 180 170 160 140 130 150 120 90 110 100 80 60 100 70 90 80 130 120 160 140 150 110 170 180 160 170 150 90 140 130 110 120 100 TOTAL FUEL FLOW – LB/HOUR 20 10 20 40 30 50 40 20 40 PRESSURE ALTITUDE - 12,000 FEET TOTAL FUEL FLOW – LB/HOUR 100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL 50 60 70 30 80 80 90 70 100 50 60 40 50 0 30 100 60 70 50 60 40 80 90 70 30 CRUISE 30 FAT=–30C FAT=–20C 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 – % MAX RANGE MAX RANGE MAX END OR MAX R/C MAX OR R/C MAX END AH–64A CRUISE T700–GE–701C DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988 ^VNE INDICATED TORQUE PER ENGINE ~ % INDICATED TORQUE PER ENGINE ~ % Figure 7A-15. Cruise Chart, 12,000 Feet, –30 C and –20 C (Sheet 2 of 5)