TM 1-1510-225-10 7-91 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 9 5 1628 73 790 210 207 1539 69 774 207 205 2,000 5 1 1516 68 740 203 206 1427 64 720 200 203 4,000 1 -3 1383 62 682 194 203 1316 59 660 190 199 6,000 -3 -7 1316 59 632 187 201 1227 55 612 184 198 8,000 -7 -11 1227 55 586 181 200 1160 52 566 177 197 10,000 -11 -15 1160 52 542 174 199 1093 49 520 171 196 12,000 -15 -19 1137 51 510 169 200 1048 47 488 166 196 14,000 -19 -23 1093 49 480 164 200 981 44 456 160 195 16,000 -23 -27 1048 47 454 159 200 937 42 428 155 195 18,000 -27 -31 1004 45 428 154 200 892 40 400 149 194 20,000 -31 -35 981 44 408 150 201 870 39 378 145 194 22,000 -34 -39 981 44 394 147 204 847 38 360 141 196 24,000 -38 -43 1004 45 388 146 209 870 39 352 140 200 26,000 -42 -47 1026 46 384 145 215 892 40 346 138 206 28,000 -46 -51 1048 47 382 144 221 914 41 344 137 211 29,000 -48 -52 1070 48 384 144 224 914 41 344 137 214 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7-84.  Maximum Range Power, 1700 RPM, ISA – 10 °C (Sheet 2 of 2)