TM 1-1510-218-10 7A-89 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 -1 -5 70 776 208 202 67 760 206 200 2,000 -5 -9 64 716 199 199 61 698 197 196 4,000 -9 -13 59 660 191 196 56 642 189 194 6,000 -13 -17 56 612 185 195 52 592 182 192 8,000 -17 -21 52 568 178 194 49 546 175 191 10,000 -21 -25 49 522 171 192 45 500 168 188 12,000 -25 -29 47 490 167 193 43 466 163 188 14,000 -29 -33 46 460 162 193 41 434 157 187 16,000 -33 -37 44 432 156 192 38 402 151 186 18,000 -37 -41 42 408 152 193 37 374 145 185 20,000 -41 -45 41 384 147 192 35 348 139 183 22,000 -45 -49 41 370 143 195 34 332 136 185 24,000 -49 -53 42 366 142 200 36 328 136 191 26,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 28,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 29,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7A-83.  Maximum Range Power, 1700 RPM, ISA – 20 C (Sheet 2 of 2)