TM 1-1510-218-10 7-48 RECOMMENDED CRUISE POWER 1700 RPM ISA + 30 °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 51 45 100 964 231 244 233 245 233 246 2,000 47 41 100 936 229 249 230 250 231 251 4,000 43 37 100 908 227 254 228 255 229 256 6,000 39 33 100 882 224 259 225 260 226 261 8,000 36 29 100 856 221 263 223 264 224 266 10,000 32 25 95 810 215 264 217 266 218 267 12,000 28 21 91 766 209 264 210 266 212 268 14,000 24 17 86 720 202 263 203 266 205 268 16,000 20 13 81 676 195 262 197 265 198 267 18,000 16 9 76 634 187 261 190 264 192 267 20,000 12 5 72 594 180 259 182 263 185 266 22,000 8 2 67 556 172 256 175 261 177 265 24,000 4 -2 63 518 163 252 167 258 170 262 26,000 -1 -6 58 484 154 246 158 254 162 260 28,000 -5 -10 54 450 142 236 149 249 154 256 29,000 -7 -12 52 424 135 229 144 244 150 254 31,000 -11 -16 47 400 --- --- 131 230 140 246 33,000 --- --- --- --- --- --- --- --- --- --- 35,000 --- --- --- --- --- --- --- --- --- --- Figure 7-44.  Recommended Cruise Power, 1700 RPM - ISA + 30 °C