TM 1-1510-218-10 7A-99 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   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 49 45 67 780 200 211 64 766 198 209 2,000 45 41 65 736 195 212 62 724 194 211 4,000 41 37 63 700 191 214 61 688 190 213 6,000 37 33 62 664 187 216 60 652 187 216 8,000 34 29 60 626 183 218 58 614 183 218 10,000 30 25 58 588 178 219 56 574 178 218 12,000 26 21 57 556 174 221 55 544 174 220 14,000 22 17 56 528 170 223 53 516 169 222 16,000 18 13 55 504 166 225 52 490 166 224 18,000 14 9 54 484 163 228 51 466 161 226 20,000 10 5 54 468 159 231 49 444 156 226 22,000 6 1 53 450 156 233 48 424 152 228 24,000 3 -3 51 428 150 232 48 408 149 231 26,000 -1 -7 50 410 144 232 47 392 144 232 28,000 -5 -11 52 418 146 244 45 374 139 231 29,000 -7 -12 52 414 144 244 46 376 139 236 31,000 -11 -16 52 410 140 247 47 376 138 243 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7A-88.  Maximum Range Power, 1700 RPM, ISA + 30 C (Sheet 2 of 2)