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 89 601 1202 206 204 80 571 1142 198 197 2000 5 1 84 562 1124 199 203 77 540 1080 194 198 4000 1 -3 79 526 1052 192 202 73 504 1008 187 197 6000 -3 -7 75 494 988 186 201 68 471 942 181 196 8000 -7 -11 71 465 930 180 201 65 441 882 175 196 10,000 -11 -15 68 438 876 174 201 61 413 826 169 195 12,000 -15 -19 66 415 830 169 202 59 389 778 164 195 14,000 -19 -23 64 396 792 165 203 57 368 736 159 196 16,000 -23 -27 62 380 760 161 205 54 350 700 154 196 18,000 -27 -31 60 365 730 156 205 53 334 668 150 197 20,000 -31 -35 59 353 706 152 206 52 323 646 146 199 22,000 -35 -39 56 336 672 145 204 52 317 634 144 203 24,000 -39 -43 53 320 640 138 201 51 307 614 141 205 26,000 -43 -47 --- --- --- --- --- 48 290 580 133 202 28,000 -47 -50 --- --- --- --- --- 46 278 556 126 199 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03587 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 7-92.  Maximum Range Power at 1500 RPM - ISA -10°C (Sheet 1 of 2)  IR Change 2  7-139