TM 1-1520-238-10 7A-65 M01-281 110 30 100 50 60 40 80 90 70 30 100 50 60 40 80 90 70 160 30 100 20 120 110 90 60 40 50 70 80 170 140 150 180 170 180 160 140 150 120 130 90 60 50 40 30 100 80 70 110 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 20 PRESSURE ALTITUDE - 16,000 FEET 170 CRUISE 800 1000 1200 60 50 130 120 800 TOTAL FUEL FLOW – LB/HOUR 1200 80 600 130 600 FAT=+10C FAT=+20C 10 0 20 D F = 10.0 SQ FT D Q – % MAX RANGE MAX RANGE MAX OR R/C MAX END MAX OR R/C MAX END AIRSPEED INDICATED KNOTS AH–64A CRUISE T700–GE–701C 10 0 20 D F = 10.0 SQ FT D Q – % 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-17. Cruise Chart, 16,000 Feet, +10 C and +20 C (Sheet 4 of 4)