TM 1-1510-223-10 NORMAL CRUISE POWER 1500 RPM ISA 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 19 -15 94 631 1262 218 220 94 631 1262 220 222 2000 16 11 94 617 1234 216 224 94 616 1232 218 226 4000 12 7 94 602 1204 214 228 94 601 1202 215 230 6000 8 3 94 586 1172 211 233 94 586 1172 213 235 8000 4 -1 94 573 1146 209 237 94 572 1144 211 239 10,000 1 -5 94 560 1120 207 242 94 560 1120 208 244 12,000 -3 -9 93 542 1084 203 245 93 542 1084 205 247 14,000 -7 -13 88 511 1022 196 244 89 512 1024 199 247 16,000 -11 -17 84 483 966 190 244 84 484 968 192 247 18,000 -15 -21 79 457 914 183 243 80 457 914 186 247 20,000 -19 -25 75 433 866 176 243 76 434 868 180 247 22,000 -23 -29 71 408 816 169 241 71 409 818 173 246 24,000 -27 -33 66 383 766 161 238 67 384 768 166 244 26,000 -31 -37 61 356 712 152 233 62 358 716 158 241 28,000 -36 -40 56 330 660 141 225 57 332 664 149 236 29,000 -38 -42 54 317 634 135 219 54 320 640 144 233 31,000 -43 -46 49 292 584 119 203 50 296 592 134 225 33,000 -46 -50 --- --- --- --- --- 45 273 546 121 214 35,000 -51 -54 --- --- --- --- --- 40 248 496 100 186 BT055917 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 7-72.  Normal Cruise Power at 1500 RPM - ISA (Sheet 1 of 2)   CA 7-106  Change 2