TM 1-1510-223-10 NORMAL CRUISE POWER 1500 RPM ISA +37°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 56 52 81 591 1182 193 207 81 591 1182 195 210 2000 52 48 79 559 1118 189 209 79 559 1118 191 211 4000 48 44 76 528 1056 184 210 76 528 1056 186 213 6000 44 40 73 498 996 179 210 73 498 996 181 214 8000 40 36 70 470 940 173 211 71 470 940 176 214 10,000 36 32 67 444 888 168 211 68 444 888 171 215 12,000 32 28 65 420 840 162 211 65 420 840 166 216 14,000 28 24 62 396 792 156 210 62 397 794 161 216 16,000 24 20 58 370 740 148 206 58 371 742 154 213 18,000 20 16 52 340 680 137 198 53 341 682 144 208 20,000 16 12 47 310 620 123 185 48 313 626 134 201 22,000 12 8 --- --- --- --- --- 44 292 584 124 194 24,000 --- --- --- --- --- --- --- --- --- --- --- --- 26,000 --- --- --- --- --- --- --- --- --- --- --- --- 28,000 --- --- --- --- --- --- --- --- --- --- --- --- 29,000 --- --- --- --- --- --- --- --- --- --- --- --- 31,000 --- --- --- --- --- --- --- --- --- --- --- --- 33,000 --- --- --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- --- --- BT03635 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 7-79.  Normal Cruise Power at 1500 RPM - ISA +37 °C (Sheet 1 of 2)  IR 7-120  Change 2