TM 1-1520-238-10 7A-58 M01-274 140 130 150 170 160 180 130 140 110 600 1400 170 1000 160 800 800 1000 1200 1400 1200 600 150 50 70 110 160 120 80 90 150 20 20 30 100 50 60 40 80 90 180 170 30 20 60 0 30 10 70 CRUISE TOTAL FUEL FLOW – LB/HOUR 100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL PRESSURE ALTITUDE - 14,000 FEET 30 40 100 50 60 40 80 90 100 70 140 40 120 80 130 90 70 100 60 50 30 100 120 110 90 70 60 80 50 40 TOTAL FUEL FLOW – LB/HOUR FAT=–20C FAT=–30C 10 D F = 10.0 SQ FT D Q – % 0 20 MAX RANGE MAX RANGE MAX END OR MAX R/C MAX OR R/C MAX END AIRSPEED INDICATED KNOTS DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988 AH–64A CRUISE T700–GE–701C 10 0 20 D F = 10.0 SQ FT D Q – % ^VNE INDICATED TORQUE PER ENGINE ~ % INDICATED TORQUE PER ENGINE ~ % Figure 7A-16. Cruise Chart, 14,000 Feet, –30 C and –20 C (Sheet 2 of 5)