TM 1-1510-223-10 LOITER POWER 1700 RPM ISA + 10°C WEIGHT® 12,000 POUNDS 10,000 POUNDS TORQUE FUEL TOTAL TORQUE FUEL TOTAL PRESSURE PER FLOW FUEL PER FLOW FUEL ALTITUDE IFAT FAT ENGINE PER FLOW IAS TAS ENGINE PER FLOW IAS TAS ENGINE ENGINE FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT   LBS/HR    LBS/HR KTS KTS 0 27 25 26 400 800 124 130 24 388 776 124 130 2000 23 21 27 383 766 124 134 24 371 742 124 134 4000 19 17 27 367 734 124 138 25 355 710 124 138 6000 15 13 28 351 702 124 142 25 339 678 124 142 8000 11 9 28 339 678 124 147 26 327 654 124 147 10,000 7 5 29 327 654 124 151 27 317 634 124 151 12,000 3 1 29 312 624 124 156 27 302 604 124 156 14,000 0 -3 30 299 598 124 161 28 288 576 124 161 16,000 -4 -7 30 286 572 124 166 28 276 552 124 166 18,000 -8 -11 31 275 550 124 172 28 265 530 124 172 20,000 -12 -15 32 266 532 124 178 29 255 510 124 178 22,000 -15 -19 32 260 520 124 184 30 248 496 124 184 24,000 -19 -23 33 254 508 124 190 30 242 474 124 190 26,000 -23 -27 34 252 504 124 197 31 237 474 124 197 28,000 -27 -30 35 252 504 124 204 32 235 470 124 204 29,000 -28 -32 35 253 506 124 208 32 235 470 124 208 31,000 -32 -36 36 254 508 124 215 33 236 472 124 215 33,000 -36 -40 37 257 514 124 223 34 238 476 124 223 35,000 -39 -44 --- --- --- --- --- 35 240 480 124 232 BT0559410 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately  7 percentage points (E.G., 67% - 7 percentage points = 60%), fuel flow will decrease approximately 20 LBS/HR/ENG, and true airspeed will be reduced approximately 20 knots. Figure 7-114.  Loiter Power at 1700 RPM - ISA +10°C (Sheet 2 of 2)  CA Change 2  7-183