TM 1-1510-218-10 7A-98 MAXIMUM RANGE POWER 1700 RPM ISA + 30 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 49 45 75 820 205 217 70 798 202 214 2,000 45 41 70 768 198 215 67 750 196 213 4,000 41 37 68 726 193 216 65 710 192 215 6,000 37 33 66 690 189 218 64 674 188 217 8,000 34 29 64 650 184 219 62 636 183 218 10,000 30 25 62 612 179 19 60 596 178 219 12,000 26 21 61 582 174 221 59 566 174 220 14,000 22 17 60 556 170 223 57 538 169 221 16,000 18 13 60 536 167 226 56 514 165 224 18,000 14 9 60 518 163 229 56 496 162 227 20,000 10 5 59 504 160 232 56 480 159 230 22,000 6 1 60 498 159 238 55 464 155 232 24,000 3 -3 62 498 158 245 55 452 151 235 26,000 -1 -7 61 486 153 246 57 456 152 244 28,000 -5 -11 – – – – – – – – – – – – 56 448 148 246 29,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7A-88.  Maximum Range Power, 1700 RPM, ISA + 30 C (Sheet 1 of 2)