TM 1-1510-218-10 7A-97 MAXIMUM RANGE POWER 1700 RPM ISA + 20 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   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 % LB/HR KTS KTS % LB/HR KTS KTS SL 39 35 69 786 204 212 67 776 203 211 2,000 35 31 68 748 200 214 65 736 199 213 4,000 31 27 67 712 196 217 64 700 196 216 6,000 28 23 65 676 193 219 62 658 190 216 8,000 24 19 63 636 188 220 59 614 184 216 10,000 20 15 60 594 182 220 56 572 178 216 12,000 16 11 59 562 178 222 55 538 174 217 14,000 12 7 57 534 173 223 53 510 170 218 16,000 8 3 56 506 169 224 51 482 165 219 18,000 4 -1 54 482 164 226 49 454 159 219 20,000 0 -5 53 460 159 226 47 428 154 219 22,000 -3 -9 52 442 155 228 46 410 150 220 24,000 -7 -13 52 432 153 232 46 398 147 224 26,000 -11 -17 51 416 148 234 47 390 146 230 28,000 -15 -21 50 406 144 235 46 382 142 233 29,000 -17 -22 51 408 144 239 46 376 140 233 31,000 -21 -26 51 408 142 245 46 372 138 237 33,000 -25 -30 – – – – – – – – – – – – 47 372 136 243 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7A-87.  Maximum Range Power, 1700 RPM, ISA + 20 C (Sheet 2 of 2)