TM 1-1510-225-10 7-99 MAXIMUM RANGE POWER 1700 RPM ISA + 30 °C 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  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 49 45 1494 67 780 200 211 1427 64 766 198 209 2,000 45 41 1450 65 736 195 212 1383 62 724 194 211 4,000 41 37 1405 63 700 191 214 1360 61 688 190 213 6,000 37 33 1383 62 664 187 216 1338 60 652 187 216 8,000 34 29 1338 60 626 183 218 1293 58 614 183 218 10,000 30 25 1293 58 588 178 219 1249 56 574 178 218 12,000 26 21 1271 57 556 174 221 1227 55 544 174 220 14,000 22 17 1249 56 528 170 223 1182 53 516 169 222 16,000 18 13 1227 55 504 166 225 1160 52 490 166 224 18,000 14 9 1204 54 484 163 228 1137 51 466 161 226 20,000 10 5 1204 54 468 159 231 1093 49 444 156 226 22,000 6 1 1182 53 450 156 233 1070 48 424 152 228 24,000 3 -3 1137 51 428 150 232 1070 48 408 149 231 26,000 -1 -7 1115 50 410 144 232 1048 47 392 144 232 28,000 -5 -11 1160 52 418 146 244 1004 45 374 139 231 29,000 -7 -12 1160 52 414 144 244 1026 46 376 139 236 31,000 -11 -16 1160 52 410 140 247 1048 47 376 138 243 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7-88.  Maximum Range Power, 1700 RPM, ISA + 30 °C (Sheet 2 of 2)