TM 1-1510-218-10 7A-92 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   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 19 15 81 840 217 218 78 822 214 215 2,000 15 11 77 790 210 217 73 770 207 214 4,000 11 7 74 748 204 217 70 724 201 214 6,000 7 3 70 696 197 216 65 672 193 211 8,000 3 -1 67 656 191 216 63 632 188 212 10,000 -1 -5 65 614 186 216 60 588 182 212 12,000 -5 -9 63 582 181 216 58 554 177 212 14,000 -9 -13 62 554 177 219 57 526 172 213 16,000 -12 -17 61 532 173 221 55 500 167 214 18,000 -16 -21 60 514 169 223 54 482 163 216 20,000 -20 -25 59 500 165 226 53 464 160 218 22,000 -24 -29 59 488 162 229 53 452 157 221 24,000 -28 -33 60 482 161 235 54 444 155 227 26,000 -31 -37 59 464 155 235 55 438 154 232 28,000 -35 -41 59 462 153 240 54 428 150 234 29,000 -37 -42 60 466 152 243 54 428 148 236 31,000 -41 -46 – – – – – – – – – – – – 55 428 146 242 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7A-85.  Maximum Range Power, 1700 RPM, ISA (Sheet 1 of 2)