TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA +10°C WEIGHT® 16,000 POUNDS 14,000 POUNDS PRESSURE ALTITUDE IFAT FAT TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT LBS/HR LBS/HR KTS KTS 0 30 25 83 634 1268 230 236 83 634 1268 231 237 2000 26 21 83 614 1228 228 240 83 614 1228 229 242 4000 23 17 83 596 1192 226 245 83 596 1192 227 246 6000 19 13 83 580 1160 224 250 83 580 1160 225 251 8000 15 9 83 567 1134 221 255 83 567 1134 223 257 10,000 11 5 83 558 1116 220 261 83 558 1116 221 262 12,000 8 1 81 537 1074 216 264 81 538 1076 217 266 14,000 4 -3 77 507 1014 210 265 77 507 1014 211 267 16,000 0 -7 73 477 954 203 265 73 478 956 205 268 18,000 -4 -11 69 449 898 197 265 69 450 900 199 268 20,000 -8 -15 65 425 850 190 265 65 425 850 192 269 22,000 -12 -19 61 400 800 183 265 62 401 802 186 269 24,000 -16 -23 58 376 752 176 264 58 376 752 179 268 26,000 -20 -27 54 352 704 169 262 54 353 706 172 267 28,000 -24 -30 50 330 660 161 260 50 331 662 165 266 29,000 -26 -32 48 319 638 157 258 48 320 640 162 265 31,000 -30 -36 44 297 594 149 254 45 298 596 154 262 33,000 -35 -40 41 274 548 139 247 41 276 552 146 258 35,000 -39 -44 36 251 502 127 237 37 253 506 136 252 BT058688 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 12%,  fuel  flow  will  decrease  approximately  8%,  and  true  airspeed  will  be  reduced by approximately 15 knots. Figure 7A-44.  Maximum Cruise Power at 1700 RPM - ISA +10°C (Sheet 2 of 2) 7A-67