TM 1-1510-225-10 7-94 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 29 25 1717 77 824 211 215 1673 75 812 210 215 2,000 25 21 1673 75 786 207 218 1628 73 774 206 217 4,000 21 17 1650 74 750 203 220 1583 71 736 202 219 6,000 18 13 1606 72 710 198 221 1539 69 694 196 219 8,000 14 9 1561 70 670 193 222 1472 66 648 190 219 10,000 10 5 1494 67 630 188 223 1405 63 606 184 219 12,000 6 1 1472 66 598 183 225 1383 62 576 181 221 14,000 2 -3 1427 64 570 179 226 1338 60 546 176 222 16,000 -2 -7 1405 63 546 174 228 1293 58 520 171 223 18,000 -6 -11 1383 62 542 170 230 1271 57 496 167 225 20,000 -10 -15 1360 61 508 166 232 1249 56 478 162 226 22,000 -14 -19 1360 61 498 163 235 1249 56 468 159 229 24,000 -17 -23 1316 59 478 157 235 1249 56 458 157 233 26,000 -21 -27 1338 60 476 156 240 1227 55 440 152 234 28,000 -25 -31 1338 60 472 152 243 1204 54 434 148 237 29,000 -27 -32 1360 61 474 151 246 1227 55 434 147 240 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7-86.  Maximum Range Power, 1700 RPM, ISA + 10 °C (Sheet 1 of 2)