TM 1-1510-225-10 7-93 MAXIMUM RANGE POWER 1700 RPM ISA 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 19 15 1650 74 804 212 213 1606 72 788 210 211 2,000 15 11 1561 70 750 204 211 1472 66 732 201 208 4,000 11 7 1472 66 704 198 210 1405 63 684 195 207 6,000 7 3 1360 61 650 189 208 1093 58 630 186 204 8,000 3 -1 1316 59 608 184 208 1227 55 586 180 204 10,000 -1 -5 1249 56 564 178 207 1137 51 542 174 203 12,000 -5 -9 1204 54 530 173 208 1115 50 506 169 203 14,000 -9 -13 1160 52 498 167 207 1048 47 472 163 202 16,000 -12 -17 1115 50 470 162 207 1004 45 444 157 202 18,000 -16 -21 1070 48 448 158 209 959 43 420 152 202 20,000 -20 -25 1048 47 428 153 210 937 42 396 147 202 22,000 -24 -29 1048 47 414 150 212 914 41 380 144 204 24,000 -28 -33 1070 48 408 149 218 914 41 370 142 208 26,000 -31 -37 1093 49 402 148 224 937 42 364 141 214 28,000 -35 -41 1115 50 400 147 230 959 43 362 141 221 29,000 -37 -42 1115 50 396 145 232 981 44 362 140 224 31,000 -41 -46 1093 49 390 142 235 1004 45 360 139 230 33,000 -45 -50 1115 50 392 140 240 1004 45 356 136 233 35,000 – – – – – – – – – – – – – – – – – – – – – 1004 45 356 134 238 Figure 7-85.  Maximum Range Power, 1700 RPM, ISA (Sheet 2 of 2)