TM 1-1510-218-10 7A-88 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 -1 -5 77 814 214 207 74 796 211 205 2,000 -5 -9 72 758 206 205 67 734 202 201 4,000 -9 -13 67 702 197 202 63 678 194 199 6,000 -13 -17 63 654 191 201 59 632 187 198 8,000 -17 -21 60 612 185 201 56 588 181 197 10,000 -21 -25 57 568 178 200 53 544 175 196 12,000 -25 -29 56 540 174 201 52 514 170 197 14,000 -29 -33 55 514 170 202 50 486 166 198 16,000 -33 -37 54 490 165 203 49 460 161 198 18,000 -37 -41 53 472 162 205 48 440 157 199 20,000 -41 -45 53 465 158 207 47 420 152 200 22,000 -45 -49 53 446 156 211 47 408 150 203 24,000 -49 -53 54 444 155 217 48 404 149 208 26,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 28,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 29,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7A-83.  Maximum Range Power, 1700 RPM, ISA – 20 C (Sheet 1 of 2)