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 94 619 1238 212 210 94 618 1236 213 211 2000 5 1 94 599 1198 210 215 94 598 1196 212 216 4000 1 -3 94 583 1166 208 219 94 582 1164 210 220 6000 -2 -7 94 569 1138 206 223 94 569 1138 207 224 8000 -6 -11 94 558 1116 203 227 94 558 1116 205 229 10,000 -10 -15 94 548 1096 201 231 94 548 1096 203 233 12,000 -14 -19 94 540 1080 199 235 94 540 1080 201 238 14,000 -17 -23 94 533 1066 196 240 94 533 1066 198 242 16,000 -21 -27 93 521 1042 193 243 93 521 1042 195 246 18,000 -25 -31 88 493 986 186 242 88 493 986 189 246 20,000 -29 -35 84 469 938 180 242 84 470 940 183 246 22,000 -33 -39 79 443 886 173 240 79 443 886 176 245 24,000 -37 -43 74 416 832 165 238 74 417 834 169 243 26,000 -41 -47 68 386 772 156 233 68 388 776 161 240 28,000 -46 -50 62 355 710 145 225 62 357 714 151 235 29,000 -48 -52 59 340 680 139 221 59 342 684 146 232 31,000 -52 -56 53 313 626 126 208 54 315 630 136 225 33,000 -56 -60 --- --- --- --- --- 49 291 582 125 215 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03625 NOTE During operations with ice vanes extended, torque will decrease approximately 10 percentage   points   (E.      G.,   64%   -   10   percentage   points   =   54%),   fuel   flow   will decrease   approximately   35   LBS/HR/ENG,   and   true   airspeed   will   be   reduced approximately 20 knots. Figure 7-69.  Normal Cruise Power at 1500 RPM - ISA -10 °C (Sheet 1 of 2)   IR 7-100  Change 2