TM 1-1510-223-10 MAXIMUM RANGE 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 9 5 91 617 1234 215 213 85 597 1194 211 209 2000 5 1 86 579 1158 208 213 80 558 1116 204 208 4000 1 -3 81 542 1084 201 212 74 518 1036 196 206 6000 -3 -7 76 508 1016 195 211 70 483 966 189 205 8000 -7 -11 72 577 954 188 210 66 451 902 182 204 10,000 -11 -15 69 448 896 182 210 62 421 842 176 203 12,000 -15 -19 66 423 846 177 210 59 395 790 170 203 14,000 -19 -23 64 401 802 172 211 57 372 744 165 203 16,000 -23 -27 62 382 764 168 213 55 353 706 161 204 18,000 -27 -31 59 362 724 162 212 53 336 672 156 205 20,000 -30 -35 58 349 698 157 212 52 324 648 152 207 22,000 -35 -39 55 330 660 149 210 51 315 630 150 211 24,000 -39 -43 52 315 630 142 207 50 303 606 146 212 26,000 -42 -47 52 311 622 139 210 47 286 572 138 208 28,000 -46 -50 54 319 638 139 217 45 274 548 131 206 29,000 -48 -52 55 323 646 140 222 45 275 550 131 209 31,000 -52 -56 --- --- --- --- --- 47 282 564 131 216 33,000 -56 -60 --- --- --- --- --- 49 288 576 131 224 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT055925 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 20 LBS/HR/ENG, and true airspeed will be reduced approximately 10 knots. Figure 7-93.  Maximum Range Power at 1500 RPM - ISA -10°C (Sheet 1 of 2)  CA Change 2  7-141