TM 1-1510-225-10 7-90 MAXIMUM RANGE POWER 1700 RPM ISA – 10 °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  13,000 POUNDS 12,000 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 9 5 1784 80 830 216 213 1695 76 810 213 210 2,000 5 1 1739 76 782 209 212 1606 72 760 206 209 4,000 1 -3 1583 71 728 201 210 1494 67 704 198 207 6,000 -3 -7 1494 67 678 194 209 1405 63 656 191 205 8,000 -7 -11 1427 64 634 188 208 1338 60 610 184 204 10,000 -11 -15 1360 61 590 181 207 1271 57 566 178 203 12,000 -15 -19 1338 60 562 177 209 1227 55 536 173 204 14,000 -19 -23 1293 58 534 173 210 1182 53 506 168 205 16,000 -23 -27 1271 57 514 169 212 1160 52 482 164 206 18,000 -27 -31 1271 57 494 165 213 1137 51 460 159 207 20,000 -31 -35 1249 56 480 162 217 1115 50 442 156 209 22,000 -34 -39 1271 57 470 160 221 1115 50 430 153 212 24,000 -38 -43 1271 57 464 158 226 1137 51 426 152 218 26,000 -42 -47 1293 58 460 156 232 1160 52 422 151 224 28,000 -46 -51 1293 58 452 153 234 1182 53 420 150 230 29,000 -48 -52 1316 59 458 153 239 1182 53 420 149 232 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7-84.  Maximum Range Power, 1700 RPM, ISA – 10 °C (Sheet 1 of 2)