TM 1-1510-225-10 7-101 MAXIMUM RANGE POWER 1700 RPM ISA + 37 °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 56 52 1516 68 788 200 214 1427 64 766 197 210 2,000 52 48 1427 64 738 194 213 1360 61 720 191 210 4,000 48 44 1383 62 696 189 214 1338 60 682 187 212 6,000 44 40 1338 60 654 184 215 1293 58 644 183 214 8,000 41 36 1293 58 618 179 216 1249 56 606 179 216 10,000 37 32 1249 56 580 175 217 1249 56 568 175 217 12,000 33 28 1227 55 548 171 219 1182 53 536 171 219 14,000 29 24 1204 54 520 166 220 1160 52 510 167 221 16,000 25 20 1182 53 496 162 222 1137 51 486 163 223 18,000 21 16 1160 52 476 159 225 1115 50 464 159 226 20,000 17 12 1160 52 462 156 229 1115 50 448 156 229 22,000 14 8 1160 52 446 152 231 1093 49 430 152 231 24,000 10 4 1115 50 426 147 232 1070 48 408 147 232 26,000 6 0 1160 52 424 147 239 1026 46 386 141 231 28,000 2 -4 1137 51 420 15 244 1048 47 380 139 239 29,000 0 -5 1160 52 418 143 246 1048 47 382 137 245 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7-89.  Maximum Range Power, 1700 RPM, ISA + 37 °C (Sheet 2 of 2)