TM 1-1510-223-10 NORMAL CRUISE POWER 1500 RPM ISA -10°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 9 5 94 618 1236 214 213 94 618 1236 215 214 2000 5 1 94 598 1196 213 218 94 597 1194 214 219 4000 2 -3 94 582 1164 211 222 94 582 1164 212 223 6000 -2 -7 94 569 1138 209 226 94 568 1136 210 227 8000 -6 -11 94 557 1114 207 230 94 557 1114 208 232 10,000 -10 -15 94 548 1096 205 235 94 547 1094 206 236 12,000 -13 -19 94 539 1078 202 239 94 539 1078 204 241 14,000 -17 -23 94 532 1064 200 244 94 532 1064 202 246 16,000 -21 -27 93 522 1044 197 248 94 522 1044 199 250 18,000 -25 -31 89 493 986 191 248 89 494 988 193 250 20,000 -29 -35 84 470 940 185 249 84 470 940 187 252 22,000 -33 -39 79 444 888 179 249 79 444 888 181 252 24,000 -37 -43 74 418 836 172 248 75 418 836 175 251 26,000 -41 -47 69 389 778 164 245 69 389 778 167 250 28,000 -45 -50 63 358 716 156 241 63 359 718 159 246 29,000 -48 -52 60 343 686 152 239 60 344 688 155 245 31,000 -51 -56 55 317 634 143 235 55 318 636 147 241 33,000 -56 -60 50 293 586 134 229 50 294 588 140 238 35,000 -60 -64 45 269 538 124 221 45 270 540 131 233 BT03626 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 7-69.  Normal Cruise Power at 1500 RPM - ISA -10 °C (Sheet 2 of 2)   IR Change 2  7-101