TM 1-1510-225-10 7-97 MAXIMUM RANGE POWER 1700 RPM ISA + 20 °C NOTES: DURING   OPERATION   WITH   ICE   VANES  E XTENDED,   TORQUE   WILL   DECREASE.      IN ORDER  TO  MAINTAIN  MAXIMUM  RANGE  CONFIGURATION, DO NOT RESET  POWER TO ORIGINAL SETTING.  FUEL FLOW WILL REMAIN ABOUT THE SAME, BUT TRUE AIRSPEED WILL BE REDUCED APPROXIMATELY 10 KNOTS. TO OBTAIN FUEL FLOW PER ENGINE, DIVIDE  THE TOTAL FUEL FLOW  VALUE FOR THE CORRESPONDING ALTITUDE BY TWO. WEIGHT  Ü  11,000 POUNDS 10,000 POUNDS PRESSURE ALT IOAT OAT TORQUE PER ENGINE FUEL FLOW TOTAL IAS TAS TORQUE PER ENGINE FUEL FLOW TOTAL IAS TAS FEET °C °C FT-LB % LB/HR KTS KTS FT-LB % LB/HR KTS KTS SL 39 35 1539 69 786 204 212 1494 67 776 203 211 2,000 35 31 1516 68 748 200 214 1450 65 736 199 213 4,000 31 27 1494 67 712 196 217 1427 64 700 196 216 6,000 28 23 1450 65 676 193 219 1383 62 658 190 216 8,000 24 19 1405 63 636 188 220 1316 59 614 184 216 10,000 20 15 1338 60 594 182 220 1249 56 572 178 216 12,000 16 11 1316 59 562 178 222 1227 55 538 174 217 14,000 12 7 1271 57 534 173 223 1182 53 510 170 218 16,000 8 3 1249 56 506 169 224 1137 51 482 165 219 18,000 4 -1 1204 54 482 164 226 1093 49 454 159 219 20,000 0 -5 1182 53 460 159 226 1048 47 428 154 219 22,000 -3 -9 1160 52 442 155 228 1026 46 410 150 220 24,000 -7 -13 1160 52 432 153 232 1026 46 398 147 224 26,000 -11 -17 1137 51 416 148 234 1048 47 390 146 230 28,000 -15 -21 1115 50 406 144 235 1026 46 382 142 233 29,000 -17 -22 1137 51 408 144 239 1026 46 376 140 233 31,000 -21 -26 1137 51 408 142 245 1026 46 372 138 237 33,000 -25 -30 – – – – – – – – – – – – – – – 1048 47 372 136 243 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7-87.  Maximum Range Power, 1700 RPM, ISA + 20 °C (Sheet 2 of 2)