TM 1-1510-218-10 7A-91 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 9 5 73 790 210 207 69 774 207 205 2,000 5 1 68 740 203 206 64 720 200 203 4,000 1 -3 62 682 194 203 59 660 190 199 6,000 -3 -7 59 632 187 201 55 612 184 198 8,000 -7 -11 55 586 181 200 52 566 177 197 10,000 -11 -15 52 542 174 199 49 520 171 196 12,000 -15 -19 51 510 169 200 47 488 166 196 14,000 -19 -23 49 480 164 200 44 456 160 195 16,000 -23 -27 47 454 159 200 42 428 155 195 18,000 -27 -31 45 428 154 200 40 400 149 194 20,000 -31 -35 44 408 150 201 39 378 145 194 22,000 -34 -39 44 394 147 204 38 360 141 196 24,000 -38 -43 45 388 146 209 39 352 140 200 26,000 -42 -47 46 384 145 215 40 346 138 206 28,000 -46 -51 47 382 144 221 41 344 137 211 29,000 -48 -52 48 384 144 224 41 344 137 214 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7A-84.  Maximum Range Power, 1700 RPM, ISA – 10 C (Sheet 2 of 2)