TM 1-1510-223-10 MAXIMUM RANGE POWER 1500 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 9 5 73 554 1108 199 197 52 480 960 175 174 2000 5 1 71 528 1056 195 200 57 478 956 180 185 4000 1 -3 68 496 992 190 200 56 454 908 177 187 6000 -3 -7 63 460 920 183 199 54 428 856 173 189 8000 -7 -11 59 428 856 176 197 52 401 802 169 189 10,000 -11 -15 56 397 794 170 196 50 375 750 164 189 12,000 -15 -19 53 370 740 164 195 47 349 698 158 189 14,000 -19 -23 50 346 692 158 195 45 325 650 153 189 16,000 -23 -27 48 325 650 153 195 42 302 604 147 188 18,000 -27 -31 45 306 612 148 195 39 281 562 142 187 20,000 -31 -35 44 291 582 144 196 37 265 530 137 187 22,000 -35 -39 43 282 564 141 199 37 254 508 134 189 24,000 -39 -43 43 275 550 139 203 36 244 488 131 191 26,000 -43 -47 43 268 536 137 207 35 235 470 128 194 28,000 -46 -50 42 259 518 134 209 35 228 456 126 198 29,000 -48 -52 41 252 504 130 208 35 225 450 124 199 31,000 -53 -56 38 238 476 122 203 35 221 442 123 204 33,000 -56 -60 39 239 478 120 208 34 215 430 120 206 35,000 -60 -64 40 246 492 121 216 32 202 404 112 202 BT055926 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 20 LBS/HR/ENG, and true airspeed will be reduced approximately 10 knots. Figure 7-93.  Maximum Range Power at 1500 RPM - ISA -10°C (Sheet 2 of 2)  CA 7-142  Change 2