TM 1-1510-223-10 NORMAL CRUISE POWER 1500 RPM ISA +30°C WEIGHT® 16,000 POUNDS 14,000 POUNDS TORQUE FUEL TOTAL TORQUE FUEL TOTAL PRESSURE PER FLOW FUEL PER FLOW FUEL ALTITUDE IFAT FAT ENGINE PER FLOW IAS TAS ENGINE PER FLOW IAS TAS ENGINE ENGINE FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT   LBS/HR    LBS/HR KTS KTS 0 49 45 90 615 1230 202 215 90 615 1230 204 217 2000 45 41 87 584 1168 197 216 88 584 1168 200 218 4000 41 37 84 553 1106 192 217 85 553 1106 195 220 6000 38 33 81 524 1048 187 218 81 524 1048 190 220 8000 34 29 78 495 990 182 218 78 496 992 184 221 10,000 30 25 74 467 934 176 218 75 468 936 179 222 12,000 26 21 71 442 884 170 218 72 442 884 174 222 14,000 22 17 68 418 836 164 218 69 419 838 168 223 16,000 18 13 64 391 782 156 214 64 392 784 161 220 18,000 13 9 57 360 720 145 207 58 362 724 151 215 20,000 9 5 52 333 666 135 199 53 335 670 143 210 22,000 5 1 49 312 624 124 191 50 314 628 135 206 24,000 1 -3 --- --- --- --- --- 46 294 588 126 200 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03633 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately  10  percentage points   (E.      G.,   64%   10   percentage   points   =   54%),   fuel   flow   will   decrease   approximately   35 LBS/HR/ENG, and true airspeed will be reduced approximately 20 knots. Figure 7-77.  Normal Cruise Power at 1500 RPM - ISA +30 °C (Sheet 1 of 2)  IR 7-116  Change 2