TM 1-1510-225-10 7-95 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  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 29 25 1628 73 800 209 214 1583 71 788 208 212 2,000 25 21 1583 71 760 205 215 1516 68 744 202 213 4,000 21 17 1516 68 714 199 215 1427 64 694 196 212 6,000 18 13 1450 65 670 193 215 1360 61 650 190 212 8,000 14 9 1383 62 626 187 215 1293 58 604 183 211 10,000 10 5 1293 58 582 180 214 1204 54 558 176 209 12,000 6 1 1271 57 552 177 216 1182 53 526 173 211 14,000 2 -3 1227 55 520 171 216 1115 50 494 167 211 16,000 -2 -7 1182 53 490 166 217 1070 48 462 161 210 18,000 -6 -11 1137 51 466 161 217 1026 46 434 155 210 20,000 -10 -15 1115 50 444 156 218 981 44 410 150 209 22,000 -14 -19 1115 50 434 153 221 981 44 398 147 212 24,000 -17 -23 1115 50 424 152 226 981 44 390 146 218 26,000 -21 -27 1137 51 416 150 231 1004 45 382 144 223 28,000 -25 -31 1115 50 404 146 234 1026 46 376 143 229 29,000 -27 -32 1115 50 398 144 234 1026 46 374 142 231 31,000 -31 -36 1115 50 398 141 239 1004 45 364 138 233 33,000 -35 -40 1137 51 404 140 246 1004 45 362 135 237 35,000 -39 -44 – – – – – – – – – – – – – – – 1026 46 368 134 244 Figure 7-86.  Maximum Range Power, 1700 RPM, ISA + 10 °C (Sheet 2 of 2)