TM 1-1520-238-10 7A-27 M01-243 100 30 100 50 60 40 80 90 70 30 100 50 60 40 80 90 70 140 120 100 90 70 20 30 50 60 150 110 160 170 140 160 150 170 130 90 110 70 30 20 130 80 60 50 110 0 10 20 30 100 TOTAL FUEL FLOW – LB/HOUR 1300 PRESSURE ALTITUDE - 2000 FEET 40 150 70 100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL 90 140 160 700 170 CRUISE 1100 120 1300 60 50 130 120 1100 TOTAL FUEL FLOW – LB/HOUR 900 700 80 900 40 80 40 FAT=–10C FAT=0C DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988 AIRSPEED INDICATED KNOTS AH–64A CRUISE T700–GE–701C MAX RANGE MAX RANGE DATA BASIS: MAX R/C OR MAX END MAX R/C OR MAX END INDICATED TORQUE PER ENGINE ~ % INDICATED TORQUE PER ENGINE ~ % 10 0 20 D F = 10.0 SQ FT D Q – % 10 0 20 D F = 10.0 SQ FT D Q – % Figure 7A-10. Cruise Chart, 2,000 Feet, –10 C and 0 C (Sheet 3 of 6)