TM 1-1510-223-10 NORMAL CRUISE POWER 1500 RPM ISA + 10°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 30 25 94 637 1274 216 222 94 636 1272 218 224 2000 26 21 94 617 1234 214 226 94 616 1232 216 228 4000 22 17 94 599 1198 212 230 94 599 1198 214 232 6000 18 13 94 583 1166 209 235 94 583 1166 211 237 8000 14 9 93 565 1130 206 238 94 566 1132 208 240 10,000 10 5 88 532 1064 199 237 88 532 1064 201 240 12,000 6 1 84 504 1008 193 238 84 505 1010 196 241 14,000 3 -3 81 478 956 187 238 81 478 956 190 242 16,000 -1 -7 77 451 902 181 238 77 452 904 184 242 18,000 -5 -11 72 425 860 174 236 73 426 852 178 241 20,000 -10 -15 68 400 800 167 234 68 401 802 171 240 22,000 -14 -19 64 376 752 159 231 64 377 754 164 238 24,000 -18 -23 59 352 704 150 227 60 354 708 156 236 26,000 -22 -27 55 329 658 140 220 56 330 660 148 232 28,000 -26 -30 51 306 612 128 210 51 308 616 139 226 29,000 -29 -32 48 294 588 120 201 49 297 594 134 222 31,000 -32 -36 --- --- --- --- --- 45 275 550 123 213 33,000 -37 -40 --- --- --- --- --- 41 253 506 105 192 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT055919 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 1 of 2)   CA 7-110  Change 2