TM 1-1510-218-10 7A-94 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 29 25 77 824 211 215 75 812 210 215 2,000 25 21 75 786 207 218 73 774 206 217 4,000 21 17 74 750 203 220 71 736 202 219 6,000 18 13 72 710 198 221 69 694 196 219 8,000 14 9 70 670 193 222 66 648 190 219 10,000 10 5 67 630 188 223 63 606 184 219 12,000 6 1 66 598 183 225 62 576 181 221 14,000 2 -3 64 570 179 226 60 546 176 222 16,000 -2 -7 63 546 174 228 58 520 171 223 18,000 -6 -11 62 542 170 230 57 496 167 225 20,000 -10 -15 61 508 166 232 56 478 162 226 22,000 -14 -19 61 498 163 235 56 468 159 229 24,000 -17 -23 59 478 157 235 56 458 157 233 26,000 -21 -27 60 476 156 240 55 440 152 234 28,000 -25 -31 60 472 152 243 54 434 148 237 29,000 -27 -32 61 474 151 246 55 434 147 240 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7A-86.  Maximum Range Power, 1700 RPM, ISA + 10 C (Sheet 1 of 2)