TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA -30°C WEIGHT® 16,000 POUNDS 14,000 POUNDS PRESSURE ALTITUDE IOAT OAT 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 -11 -15 83 629 1258 231 220 83 628 1256 233 222 2000 -14 -19 83 610 1220 230 226 83 609 1218 232 227 4000 -18 -23 83 592 1184 230 232 83 592 1184 232 234 6000 -22 -27 83 576 1152 228 236 83 576 1152 230 238 8000 -25 -31 83 565 1130 227 242 83 564 1128 228 244 10,000 -29 -35 83 555 1110 225 247 83 555 1110 226 248 12,000 -33 -39 83 545 1090 222 251 83 544 1088 224 253 14,000 -37 -43 83 536 1072 220 257 83 535 1070 222 259 16,000 -40 -47 83 528 1056 218 262 83 528 1056 220 264 18,000 -44 -51 83 522 1044 216 268 83 521 1042 218 270 20,000 -48 -55 83 516 1032 214 273 83 515 1030 216 276 22,000 -51 -59 83 511 1022 212 279 83 511 1022 214 282 24,000 -55 -63 79 486 972 205 279 80 488 976 208 283 26,000 -59 -67 74 453 906 196 276 74 455 910 200 281 28,000 -64 -70 66 411 822 184 269 67 414 828 189 275 29,000 -66 -72 62 390 780 178 265 63 393 786 183 272 31,000 -70 -76 55 349 698 164 254 56 353 706 171 263 33,000 -75 -80 48 312 624 149 240 49 316 632 158 253 35,000 -79 -84 - - - - - - - - - - - - - - - 42 279 558 142 237 BT05210 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 7-40.  Maximum Cruise Power at 1700 RPM - ISA -30°C (Sheet 1 of 2) 7-58