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 -1 -5 86 594 1188 222 216 78 565 1130 214 209 2000 -5 -9 80 555 1110 214 214 73 529 1058 207 208- 4000 -9 -13 76 518 1036 206 213 69 494 988 201 207 6000 -13 -17 72 486 972 200 212 65 461 "922 194 206 8000 -17 -21 68 457 914 194 212 61 429 858 187 204 10,000 -21 -25 65 429 858 187 211 58 400 800 180 203 12,000 -25 -29 62 404 808 182 211 55 375 750 174 203 14,000 -29 -33 60 383 766 177 212 53 354 708 169 203 16,000 -32 -37 59 367 734 172 214 51 336 672 165 205 18,000 -36 -41 58 353 706 168 216 50 322 644 161 206 20,000 -40 -45 56 340 680 164 217 49 310 620 157 209 22,000 -44 -49 56 332 664 161 220 49 302 604 155 212 24,000 -48 -53 54 322 644 157 222 48 295 590 152 215 26,000 -52 -57 52 307 614 149 218 48 290 580 150 219 28,000 -56 -60 52 306 612 146 222 47 279 558 144 219 29,000 -58 -52 54 313 626 148 228 45 271 542 140 217 31,000 -62 -66 --- --- --- --- --- 45 270 540 137 220 33,000 -65 -70 --- --- --- --- --- 48 282 564 140 232 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT0587113 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-65.  Maximum Range Power at 1500 RPM - ISA -20°C (Sheet 1 of 2) 7A-100