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