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 30 25 94 636 1272 219 225 94 635 1270 220 226 2000 26 21 94 616 1232 217 229 94 616 1232 218 231 4000 22 17 94 598 1196 215 234 94 598 1196 216 235 6000 18 13 94 582 1164 213 238 94 582 1164 214 240 8000 15 9 94 566 1132 210 242 94 566 1132 211 244 10,000 11 5 88 532 1064 203 242 88 533 1066 204 244 12,000 7 1 85 505 1010 198 243 85 505 1010 199 245 14,000 3 -3 81 479 958 193 244 81 479 958 194 247 16,000 -1 -7 77 452 904 187 245 77 453 906 189 248 18,000 -5 -11 73 426 852 181 245 73 427 854 183 248 20,000 -9 -15 69 402 804 174 244 69 402 804 177 248 22,000 -13 -19 65 378 756 167 243 65 379 758 170 247 24,000 -17 -23 60 355 710 160 242 61 355 710 164 247 26,000 -21 -27 56 331 662 153 239 56 332 664 157 245 28,000 -25 -30 52 309 618 145 236 52 310 620 150 243 29,000 -27 -32 50 298 596 141 234 50 299 598 146 242 31,000 -32 -36 46 277 554 133 229 46 278 556 139 239 33,000 -36 -40 42 256 512 123 222 43 258 516 131 235 35,000 -40 -44 38 235 470 111 210 39 237 474 122 229 BT0559110 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 7-74.  Normal Cruise Power at 1500 RPM - ISA +10 °C (Sheet 2 of 2)   CA Change 2  7-111