TM 1-1520-238-10 7A-43 M01-259 PRESSURE ALTITUDE - 8000 FEET 1000 600 1000 800 1200 600 800 1400 1200 110 80 90 100 120 140 150 160 130 180 170 60 100 70 90 80 130 120 160 140 150 110 170 140 130 110 90 100 180 160 170 150 TOTAL FUEL FLOW – LB/HOUR 10 60 40 70 30 50 20 0 80 70 30 100 50 30 TOTAL FUEL FLOW – LB/HOUR 50 100% RPM, 8 HELLFIRE CONFIGURATION, JP-4 FUEL 120 30 100 50 60 40 60 40 80 90 70 80 90 20 30 60 CRUISE 70 40 50 40 20 FAT=–20C FAT=–30C AIRSPEED INDICATED KNOTS AH–64A CRUISE T700–GE–701C 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 DATA BASIS: DERIVED FROM FLIGHT TEST AND ENGINE MODEL SPEC NO. E1290, 15 APRIL 1988 ^VNE INDICATED TORQUE PER ENGINE ~ % INDICATED TORQUE PER ENGINE ~ % MAX R/C OR MAX END MAX R/C OR MAX END Figure 7A-13. Cruise Chart, 8,000 Feet, –30 C and –20 C (Sheet 2 of 5)