TM 1-1510-218-10 7A-100 MAXIMUM RANGE POWER 1700 RPM ISA + 37 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 56 52 77 840 207 222 73 814 204 218 2,000 52 48 74 790 201 221 68 760 197 216 4,000 48 44 70 740 194 220 65 714 191 216 6,000 44 40 66 694 188 220 63 670 185 216 8,000 41 36 65 656 183 221 61 632 180 217 10,000 37 32 63 620 179 222 59 594 176 218 12,000 33 28 63 592 175 225 58 564 172 220 14,000 29 24 62 568 171 227 57 538 167 222 16,000 25 20 62 548 168 230 56 516 164 224 18,000 21 16 62 534 166 235 55 496 160 227 20,000 17 12 62 522 163 239 55 482 157 230 22,000 14 8 62 512 160 243 55 470 154 234 24,000 10 4 62 498 156 245 57 468 154 242 26,000 6 0 63 496 154 250 57 458 150 245 28,000 2 -4 – – – – – – – – – – – – 58 456 148 250 29,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7A-89.  Maximum Range Power, 1700 RPM, ISA + 37 C (Sheet 1 of 2)