TM 1-1510-223-10 NORMAL CRUISE POWER 1500 RPM ISA 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 19 15 94 617 1234 211 213 94 616 1232 212 214 2000 15 11 94 603 1206 209 217 94 602 1204 210 218 4000 12 7 94 588 1176 206 221 94 588 1176 208 222 6000 8 3 94 574 1148 204 225 94 573 1146 206 227 8000 4 -1 94 561 1122 202 229 94 561 1122 203 231 10,000 0 -5 94 550 1100 199 233 94 550 1100 201 235 12,000 -4 -9 94 540 1080 197 238 94 540 1080 199 240 14,000 -7 -13 91 517 1034 191 238 91 518 1036 194 241 16,000 -11 -17 86 488 976 185 238 86 489 978 187 241 18,000 -15 -21 81 462 924 178 237 82 463 926 181 241 20,000 -19 -25 77 438 876 171 236 77 439 878 175 240 22,000 -24 -29 72 413 826 164 233 72 413 826 168 239 24,000 -28 -33 67 387 774 155 230 68 388 776 160 237 26,000 -32 -37 62 360 720 146 224 63 361 722 152 233 28,000 -36 -40 57 333 666 135 216 57 335 670 143 228 29,000 -38 -42 54 320 640 129 211 55 323 646 139 225 31,000 -42 -46 --- --- --- --- --- 50 298 596 128 217 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03627 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/HRIENG,   and   true   airspeed   will   be   reduced approximately 20 knots. Figure 7-71.  Normal Cruise Power at 1500 RPM - ISA (Sheet 1 of 2)   IR 7-104  Change 2