TM 1-1510-224-10 NORMAL CRUISE POWER 1500 RPM ISA -30°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 -11 -15 76 556 1112 212 203 71 537 1074 208 199 2000 -15 -19 72 521 1042 205 202 68 504 1008 202 199 4000 -19 -23 68 486 972 198 200 64 472 944 196 198 6000 -23 -27 64 455 910 192 200 61 441 -882 190 198 8000 -27 -31 61 425 850 185 198 57 410 820 183 196 10,000 -31 -35 58 399 798 179 198 54 383 766 176 195 12,000 -35 -39 57 379 758 175 199 51 358 716 170 194 14,000 -39 -43 56 363 726 171 202 49 337 674 165 195 16,000 -43 -47 55 350 700 168 204 47 318 636 160 195 18,000 -47 -51 54 338 676 165 207 46 302 604 155 195 20,000 -51 -55 53 327 654 161 208 45 290 580 151 197 22,000 -54 -59 53 322 644 159 213 45 287 574 150 202 24,000 -58 -63 54 318 636 157 217 46 284 568 150 207 26,000 -62 -67 53 313 626 155 221 47 283 566 149 213 28,000 -66 -70 51 299 598 147 217 47 280 560 147 218 29,000 -68 -72 52 302 604 147 221 46 273 546 144 217 31,000 -71 -76 55 315 630 150 233 45 266 532 138 217 33,000 -76 -80 --- --- --- --- --- 46 273 546 139 225 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0687115 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 10%,  fuel  flow  will  decrease  approximately  5%,  and  true  airspeed  will  be  reduced by approximately 10 knots. Figure 7A-64.  Maximum Range Power at 1500 RPM - ISA -30°C (Sheet 1 of 2) 7A-98