TM 1-1510-223-10 NORMAL CRUISE POWER 1500 RPM ISA + 30°C WEIGHT® 12,000 POUNDS 10,000 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 85 606 1212 208 220 85 606 1212 209 222 2000 46 41 82 576 1152 203 222 82 576 1152 205 224 4000 42 37 80 546 1092 199 224 80 547 1094 201 226 6000 38 33 77 518 1036 194 226 77 518 1036 196 228 8000 34 29 74 490 980 189 227 74 490 980 191 229 10,000 30 25 71 462 924 185 228 71 462 924 187 231 12,000 26 21 69 437 874 180 230 69 437 874 182 233 14,000 22 17 66 414 828 175 231 67 414 828 178 234 16,000 18 13 62 388 776 169 230 63 388 776 171 234 18,000 14 9 57 359 718 160 226 57 359 718 163 231 20,000 10 5 52 332 664 152 223 53 333 666 156 229 22,000 6 1 49 312 624 145 221 50 313 626 150 228 24,000 2 -3 46 292 584 138 219 46 292 584 143 226 26,000 -2 -7 43 274 548 131 216 44 275 550 138 225 28,000 -6 -10 41 260 520 125 213 41 261 522 132 225 29,000 -8 -12 40 252 504 121 211 40 253 506 129 224 31,000 -13 -16 37 234 468 110 202 37 236 472 122 220 33,000 -18 -20 32 211 422 84 163 34 217 434 112 213 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0559114 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 7-78.  Normal Cruise Power at 1500 RPM - ISA +30 °C (Sheet 2 of 2)  CA Change 2  7-119