TM 1-1510-223-10 NORMAL CRUISE POWER 1500 RPM ISA -10°C WEIGHT® 16,000 POUNDS 14,000 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 9 5 94 631 1262 220 218 94 631 1262 221 219 2000 6 1 94 614 1228 218 222 94 613 1226 219 224 4000 2 -3 94 597 1194 216 226 94 597 1194 217 228 6000 -2 -7 94 583 1166 213 230 94 582 1164 215 232 8000 -6 -11 94 570 1140 211 235 94 570 1140 213 237 10,000 -10 -15 94 560 1120 209 239 94 559 1118 210 241 12,000 -13 -19 94 549 1098 206 244 94 549 1098 208 246 14,000 -17 -23 94 540 1080 204 248 94 540 1080 206 251 16,000 -21 -27 91 515 1030 198 249 91 516 1032 200 252 18,000 -25 -31 86 487 974 191 249 86 487 974 194 252 20,000 -29 -35 82 464 928 185 249 82 464 928 188 253 22,000 -33 -39 77 438 876 178 248 78 438 876 182 252 24,000 -37 -43 73 412 824 170 245 73 413 826 175 251 26,000 -41 -47 67 383 766 161 241 68 384 768 166 248 28,000 -45 -50 61 352 704 151 234 62 354 708 157 243 29,000 -48 -52 58 337 674 145 229 59 339 678 152 240 31,000 -52 -56 53 310 620 132 218 54 312 624 142 233 33,000 -57 -60 47 285 570 113 197 49 288 576 131 224 35,000 -60 -64 --- --- --- --- --- 44 264 528 117 210 BT055915 NOTE During operations with ice vanes extended, torque will decrease approximately 10 percentage   points   (E.G.,   64%   -   10   percentage   points   =   54%/0),   fuel   flow   will decrease   approximately   35   LBS/HRIENG,   and   true   airspeed   will   be   reduced approximately 20 knots. Figure 7-70.  Normal Cruise Power at 1500 RPM - ISA -10 °C (Sheet 1 of 2)   CA 7-102  Change 2