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 28 394 788 124 130 26 383 766 124 130 2000 23 21 28 377 754 124 134 26 366 732 124 134 4000 19 17 29 361 722 124 138 26 330 700 124 138 6000 15 13 29 346 692 124 142 27 335 670 124 142 8000 11 9 30 335 670 124 147 27 324 648 124 147 10,000 7 5 31 326 652 124 151 28 316 632 124 151 12,000 3 1 31 312 624 124 156 29 303 606 124 156 14,000 0 -3 32 300 600 124 161 29 290 580 124 161 16,000 -4 -7 32 288 576 124 166 30 278 556 124 166 18,000 -8 -11 33 278 556 124 172 30 268 536 124 172 20,000 -12 -15 33 270 540 124 178 31 259 518 124 178 22,000 -15 -19 34 265 530 124 184 32 253 506 124 184 24,000 -19 -23 35 260 520 124 190 32 248 496 124 190 26,000 -23 -27 36 260 520 124 197 33 244 488 124 197 28,000 -27 -30 37 261 522 124 204 34 244 488 124 204 29,000 -28 -32 37 262 524 124 208 34 245 490 124 208 31,000 -32 -36 39 264 528 124 215 35 246 492 124 215 33,000 -36 -40 --- --- --- --- --- 36 249 498 124 223 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03608 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 7-113.  Loiter Power at 1700 RPM - ISA +10°C (Sheet 2 of 2)  IR Change 2  7-181