TM 1-1510-218-10 7A-90 MAXIMUM RANGE POWER 1700 RPM ISA – 10 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   13,000 POUNDS 12,000 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 9 5 80 830 216 213 76 810 213 210 2,000 5 1 76 782 209 212 72 760 206 209 4,000 1 -3 71 728 201 210 67 704 198 207 6,000 -3 -7 67 678 194 209 63 656 191 205 8,000 -7 -11 64 634 188 208 60 610 184 204 10,000 -11 -15 61 590 181 207 57 566 178 203 12,000 -15 -19 60 562 177 209 55 536 173 204 14,000 -19 -23 58 534 173 210 53 506 168 205 16,000 -23 -27 57 514 169 212 52 482 164 206 18,000 -27 -31 57 494 165 213 51 460 159 207 20,000 -31 -35 56 480 162 217 50 442 156 209 22,000 -34 -39 57 470 160 221 50 430 153 212 24,000 -38 -43 57 464 158 226 51 426 152 218 26,000 -42 -47 58 460 156 232 52 422 151 224 28,000 -46 -51 58 452 153 234 53 420 150 230 29,000 -48 -52 59 458 153 239 53 420 149 232 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7A-84.  Maximum Range Power, 1700 RPM, ISA – 10 C (Sheet 1 of 2)