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 29 25 87 597 1194 202 207 84 587 1174 201 207 2000 25 21 83 563 1126 196 208 81 554 1108 196 208 4000 21 17 79 528 1056 190 207 78 521 1042 191 208 6000 17 13 75 495 990 184 207 74 489 978 185 208 8000 13 9 70 464 928 177 205 70 461 922 179 208 10,000 9 5 65 434 868 169 202 65 431 862 171 205 12,000 5 1 63 411 822 163 202 62 406 812 166 205 14,000 1 -3 60 386 772 157 201 59 382 764 160 205 16,000 -3 -7 57 366 732 151 200 56 358 716 154 203 18,000 -7 -11 55 348 696 145 199 53 338 676 148 202 20,000 -11 -15 55 341 682 142 202 49 316 632 140 199 22,000 -15 -19 57 345 690 142 209 47 301 602 134 197 24,000 -18 -23 58 346 692 141 214 47 296 592 131 200 26,000 -22 -27 --- --- --- --- --- 49 302 604 132 208 28,000 -26 -30 --- --- --- --- --- 51 304 608 131 214 29,000 -28 -32 --- --- --- --- --- 51 304 608 130 217 31,000-- --- --- --- --- --- --- --- --- --- --- --- --- 33,000-- --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03591 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 7-96.  Maximum Range Power at 1500 RPM - ISA +10 °C (Sheet 1 of 2)  IR Change 2  7-147