TM 1-1510-224-10 MAXIMUM CRUISE POWER 1700 RPM ISA +37°C WEIGHT® 16,000 POUNDS 14,000 POUNDS PRESSURE ALTITUDE IOAT OAT TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS TORQUE PER ENGINE FUEL FLOW PER ENGINE TOTAL FUEL FLOW IAS TAS FEET °C °C PERCENT LBS/HR LBS/HR KTS KTS PERCENT LBS/HR LBS/HR KTS KTS 0 57 52 73 607 1214 213 228 74 607 1214 215 230 2000 53 48 72 577 1154 209 231 72 577 1154 211 233 4000 49 44 70 548 1096 205 233 70 548 1096 207 235 6000 45 40 68 522 1044 200 235 68 522 1044 203 238 8000 41 36 66 495 990 195 236 66 495 990 198 239 10,000 37 32 63 468 936 189 237 64 468 936 192 240 12,000 33 28 60 436 872 182 235 60 437 874 186 240 14,000 29 24 56 407 814 175 233 57 408 816 179 239 16,000 25 20 53 378 756 166 230 53 379 758 171 236 18,000 21 16 48 349 698 156 223 49 351 702 162 232 20,000 17 12 44 323 646 145 216 45 324 648 153 227 22,000 12 8 41 302 604 134 207 42 304 608 144 222 24,000 9 4 - - - - - - - - - - - - - - - 38 283 566 134 215 26,000 5 0 - - - - - - - - - - - - - - - 36 266 532 125 208 28,000 0 -3 - - - - - - - - - - - - - - - 34 252 504 114 198 29,000 -2 -5 - - - - - - - - - - - - - - - 33 243 486 103 184 31,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 33,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - 35,000 - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - - BT05212 NOTE During  operations  with  ice  vanes  extended,  torque  will  decrease  approximately 12%,  fuel  flow  will  decrease  approximately  8%,  and  true  airspeed  will  be  reduced by approximately 15 knots. Figure 7-47.  Maximum Cruise Power at 1700 RPM - ISA +37°C (Sheet 1 of 2) 7-72