TM 1-1510-218-10 7-46 RECOMMENDED CRUISE POWER 1700 RPM ISA + 10 °C NOTE: TO OBTAIN FUEL FLOW  PER  ENGINE,  DIVIDE  THE  TOTAL  FUEL  FLOW  VALUE  FOR  THE CORRESPONDING ALTITUDE BY TWO. AIRSPEED ~ KNOTS PRESSURE ALT IOAT OAT TORQUE PER ENGINE FUEL FLOW TOTAL @12,000 LB @11,000 LB @10,000 LB FEET ° C ° C % LB/HR IAS TAS IAS TAS IAS TAS SL 30 25 100 950 234 239 235 240 236 241 2,000 27 21 100 924 232 244 233 245 234 246 4,000 23 17 100 898 230 249 231 250 232 251 6,000 19 13 100 874 227 253 228 254 229 256 8,000 15 9 100 852 225 258 226 259 227 261 10,000 12 5 100 832 223 263 224 265 225 266 12,000 8 1 100 818 220 269 221 270 222 274 14,000 4 -2 100 804 217 273 219 275 220 276 16,000 1 -7 95 760 210 273 212 275 213 277 18,000 -4 -11 89 714 203 272 205 274 206 276 20,000 -8 -15 84 666 195 270 197 273 199 275 22,000 -42 -18 77 620 186 267 188 270 190 273 24,000 -16 -22 71 574 177 262 179 266 182 270 26,000 -20 -26 65 532 167 257 170 262 173 266 28,000 -24 -30 60 492 157 251 161 257 165 263 29,000 -26 -32 58 474 151 246 157 254 160 261 31,000 -31 -36 53 438 138 232 146 247 151 255 33,000 -36 -40 47 400 --- --- 132 231 141 217 35,000 -40 -44 44 370 --- --- --- --- 128 233 Figure 7-42.  Recommended Cruise Power, 1700 RPM - ISA + 10 °C