TM 1-1510-218-10 7A-96 MAXIMUM RANGE POWER 1700 RPM ISA + 20 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 39 35 73 810 205 213 71 798 204 212 2,000 35 31 72 722 201 215 69 758 200 214 4,000 31 27 70 734 197 217 69 726 197 217 6,000 28 23 69 698 193 219 67 688 193 219 8,000 24 19 67 660 188 220 65 650 188 221 10,000 20 15 65 622 183 222 63 610 183 222 12,000 16 11 63 588 179 223 61 578 179 223 14,000 12 7 62 562 174 224 60 550 175 225 16,000 8 3 61 538 170 226 59 526 171 227 18,000 4 -1 60 516 166 228 58 504 167 229 20,000 0 -5 60 502 163 231 58 488 163 232 22,000 -3 -9 59 490 159 234 57 472 159 234 24,000 -7 -13 60 484 157 239 55 452 154 234 26,000 -11 -17 61 484 156 245 55 444 151 238 28,000 -15 -21 61 480 152 247 56 446 149 244 29,000 -17 -22 – – – – – – – – – – – – 56 444 147 245 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7A-87.  Maximum Range Power, 1700 RPM, ISA + 20 C (Sheet 1 of 2)