TM 1-1510-223-10 MAXIMUM RANGE POWER 1500 RPM ISA +30°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 49 45 71 553 1106 188 200 65 532 1064 183 195 2000 45 41 70 528 1056 185 203 64 508 1016 180 198 4000 41 37 68 499 998 181 204 63 481 962 177 200 6000 37 33 64 466 932 175 203 60 452 904 172 201 8000 33 29 60 434 868 168 203 57 423 846 167 201 10,000 29 25 57 404 808 162 202 55 396 792 162 202 12,000 25 21 54 377 754 156 201 52 370 740 157 202 14,000 21 17 51 352 704 151 200 49 345 690 152 202 16,000 17 13 47 328 656 144 198 45 319 638 145 199 18,000 13 9 45 313 626 138 198 41 296 592 137 195 20,000 9 5 45 304 608 136 201 38 276 552 130 193 22,000 5 1 45 297 594 134 205 37 262 524 126 193 24,000 2 -3 45 290 580 132 209 36 250 500 122 194 26,000 -2 -7 45 281 562 128 211 35 240 480 118 195 28,000 -7 -10 --- --- --- --- --- 35 234 468 115 199 29,000 -9 -12 --- --- --- --- --- 35 231 462 114 200 31,000 -13 -16 --- --- --- --- --- 34 218 436 109 199 33,000 --- -- --- --- --- --- --- --- --- --- --- --- 35,000 --- -- --- --- --- --- --- --- --- --- --- --- BT03596 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 7-100.  Maximum Range Power at 1500 RPM - ISA +30 °C (Sheet 2 of 2)  IR 7-156  Change 2