TM 1-1510-223-10 NORMAL CRUISE POWER 1500 RPM ISA + 20°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 40 35 94 640 1280 215 224 94 640 1280 216 226 2000 36 31 94 619 1238 212 228 94 619 1238 214 230 4000 32 27 91 587 1174 207 229 91 587 1174 209 231 6000 28 23 87 555 1110 201 230 87 555 1110 204 232 8000 24 19 84 526 1052 196 231 84 526 1052 198 233 10,000 20 15 80 498 996 190 231 81 498 996 193 234 12,000 16 11 78 472 944 185 232 78 472 944 188 236 14,000 12 7 73 443 886 178 230 73 444 888 181 235 16,000 8 3 68 417 834 170 228 69 417 834 174 233 18,000 4 -1 65 391 782 163 227 65 392 784 168 233 20,000 0 -5 60 367 734 155 223 61 368 736 160 231 22,000 -4 -9 56 344 688 146 219 57 345 690 153 228 24,000 -8 -13 52 321 642 137 212 53 323 646 145 224 26,000 -13 -17 49 299 598 125 202 49 302 604 136 219 28,000 -16 -20 --- --- --- --- --- 46 282 564 127 212 29,000 -18 -22 --- --- --- --- --- 44 273 546 121 207 31,000 - -23 -26 --- --- --- --- --- 40 251 502 104 187 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559111 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 7-76.  Normal Cruise Power at 1500 RPM - ISA +20 °C (Sheet 1 of 2)  CA 7-114  Change 2