TM 1-1510-218-10 7A-101 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   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 56 52 68 788 200 214 64 766 197 210 2,000 52 48 64 738 194 213 61 720 191 210 4,000 48 44 62 696 189 214 60 682 187 212 6,000 44 40 60 654 184 215 58 644 183 214 8,000 41 36 58 618 179 216 56 606 179 216 10,000 37 32 56 580 175 217 56 568 175 217 12,000 33 28 55 548 171 219 53 536 171 219 14,000 29 24 54 520 166 220 52 510 167 221 16,000 25 20 53 496 162 222 51 486 163 223 18,000 21 16 52 476 159 225 50 464 159 226 20,000 17 12 52 462 156 229 50 448 156 229 22,000 14 8 52 446 152 231 49 430 152 231 24,000 10 4 50 426 147 232 48 408 147 232 26,000 6 0 52 424 147 239 46 386 141 231 28,000 2 -4 51 420 15 244 47 380 139 239 29,000 0 -5 52 418 143 246 47 382 137 245 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7A-89.  Maximum Range Power, 1700 RPM, ISA + 37 C (Sheet 2 of 2)