TM 1-1510-225-10 7-92 MAXIMUM RANGE POWER 1700 RPM ISA NOTES: DURING   OPERATION   WITH   ICE   VANES   EXTENDED,   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 19 15 1806 81 840 217 218 1739 78 822 214 215 2,000 15 11 1717 77 790 210 217 1628 73 770 207 214 4,000 11 7 1650 74 748 204 217 1561 70 724 201 214 6,000 7 3 1561 70 696 197 216 1450 65 672 193 211 8,000 3 -1 1494 67 656 191 216 1405 63 632 188 212 10,000 -1 -5 1450 65 614 186 216 1338 60 588 182 212 12,000 -5 -9 1405 63 582 181 216 1293 58 554 177 212 14,000 -9 -13 1383 62 554 177 219 1271 57 526 172 213 16,000 -12 -17 1360 61 532 173 221 1227 55 500 167 214 18,000 -16 -21 1338 60 514 169 223 1204 54 482 163 216 20,000 -20 -25 1316 59 500 165 226 1182 53 464 160 218 22,000 -24 -29 1316 59 488 162 229 1182 53 452 157 221 24,000 -28 -33 1338 60 482 161 235 1204 54 444 155 227 26,000 -31 -37 1316 59 464 155 235 1227 55 438 154 232 28,000 -35 -41 1316 59 462 153 240 1204 54 428 150 234 29,000 -37 -42 1338 60 466 152 243 1204 54 428 148 236 31,000 -41 -46 – – – – – – – – – – – – – – – 1227 55 428 146 242 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7-85.  Maximum Range Power, 1700 RPM, ISA (Sheet 1 of 2)