TM 1-1510-223-10 MAXIMUM CRUISE POWER 1700 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 -11 -15 83 612 1224 212 203 83 611 1222 214 204 2000 -15 -19 83 593 1186 212 208 83 592 1184 213 209 4000 -19 -23 83 575 1150 211 213 83 575 1150 212 215 6000 -23 -27 83 560 1120 209 217 83 559 1118 210 219 8000 -26 -31 83 547 1094 208 222 83 547 1094 209 224 10,000 -30 -35 83 539 1078 205 226 83 538 1076 207 228 12,000 -34 -39 83 531 1062 203 231 83 530 1060 205 233 14,000 -38 -43 83 524 1048 201 236 83 523 1046 203 238 16,000 -41 -47 83 518 1036 199 240 83 518 1036 201 243 18,000 -45 -51 83 514 1028 197 245 83 513 1026 199 248 20,000 -49 -55 83 510 1020 195 250 83 509 1018 197 253 22,000 -53 -59 83 506 1012 193 255 83 505 1010 195 258 24,000 -57 -63 79 479 958 186 255 79 480 960 189 259 26,000 -61 -67 72 442 884 177 251 73 444 888 180 255 28,000 -65 -70 64 400 800 165 243 65 401 802 169 249 29,000 -67 -72 61 379 758 159 239 61 381 762 164 246 31,000 -72 -76 54 341 682 146 228 55 344 688 153 238 33,000 -76 -80 47 305 610 131 213 48 309 618 141 228 35,000 -80 -84 --- --- --- --- --- 41 273 546 125 212 BT03277 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 7-42.  Maximum Cruise Power at 1700 RPM - ISA -300C (Sheet 1 of 2)   IR Change 2  7-53