TM 1-1510-218-10 7A-95 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   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 29 25 73 800 209 214 71 788 208 212 2,000 25 21 71 760 205 215 68 744 202 213 4,000 21 17 68 714 199 215 64 694 196 212 6,000 18 13 65 670 193 215 61 650 190 212 8,000 14 9 62 626 187 215 58 604 183 211 10,000 10 5 58 582 180 214 54 558 176 209 12,000 6 1 57 552 177 216 53 526 173 211 14,000 2 -3 55 520 171 216 50 494 167 211 16,000 -2 -7 53 490 166 217 48 462 161 210 18,000 -6 -11 51 466 161 217 46 434 155 210 20,000 -10 -15 50 444 156 218 44 410 150 209 22,000 -14 -19 50 434 153 221 44 398 147 212 24,000 -17 -23 50 424 152 226 44 390 146 218 26,000 -21 -27 51 416 150 231 45 382 144 223 28,000 -25 -31 50 404 146 234 46 376 143 229 29,000 -27 -32 50 398 144 234 46 374 142 231 31,000 -31 -36 50 398 141 239 45 364 138 233 33,000 -35 -40 51 404 140 246 45 362 135 237 35,000 -39 -44 – – – – – – – – – – – – 46 368 134 244 Figure 7A-86.  Maximum Range Power, 1700 RPM, ISA + 10 C (Sheet 2 of 2)