TM 1-1520-238-10 7A-60 M01-276 600 80 100 40 140 600 160 150 170 130 180 170 50 20 60 80 90 30 70 30 110 TOTAL FUEL FLOW – LB/HOUR 70 70 90 TOTAL FUEL FLOW – LB/HOUR CRUISE 100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL PRESSURE ALTITUDE - 14,000 FEET 130 120 110 50 30 40 20 180 40 100 50 60 100 120 170 160 100 90 80 70 60 50 40 0 10 20 30 30 100 90 80 70 60 40 50 110 150 140 160 120 130 80 1200 1000 800 60 1400 1200 1000 800 90 150 140 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=+10C FAT=+20C MAX RANGE MAX RANGE MAX OR R/C MAX END 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 INDICATED TORQUE PER ENGINE ~ % INDICATED TORQUE PER ENGINE ~ % Figure 7A-16. Cruise Chart, 14,000 Feet, +10 C and +20 C (Sheet 4 of 5)