TM 1-1510-218-10 7A-56 MAXIMUM CRUISE POWER 1700 RPM ISA + 30 C NOTES: IOAT, TORQUE, AND FUEL FLOW BASED ON 12,000 POUNDS. 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 TOTAL FUEL FLOW 13,000 LB 12,000 LB 11,000 LB 10,000 LB FEET C C % LB/HR IAS TAS IAS TAS IAS TAS IAS TAS SL 51 45 100 964 231 243 231 244 232 245 233 246 2000 47 41 100 936 228 248 229 249 230 250 231 251 4000 43 37 100 910 226 252 227 254 228 255 229 256 6000 39 33 100 882 223 257 224 259 225 260 226 261 8000 36 29 100 858 221 262 222 264 223 265 224 266 10,000 32 25 99 830 216 266 219 268 220 270 221 271 12,000 28 21 94 774 210 266 212 268 213 270 215 271 14,000 24 17 91 740 205 267 206 269 208 272 210 273 16,000 20 13 88 706 199 268 201 271 203 273 204 275 18,000 16 9 85 674 193 269 195 272 197 275 199 277 20,000 12 5 83 650 188 271 190 274 193 277 194 288 22,000 8 1 79 620 181 271 184 275 187 278 189 281 24,000 4 -3 74 580 173 267 176 272 179 276 182 280 26,000 0 -7 69 536 163 261 167 267 171 273 174 278 28,000 -4 -11 63 494 151 252 157 261 162 268 165 274 29,000 -7 -12 61 474 144 244 151 257 157 265 161 272 31,000 -11 -16 55 434 – – – – – – 138 243 146 257 151 266 33,000 -15 -20 51 402 – – – – – – – – – – – – 133 243 141 258 35,000 -19 -24 46 370 – – – – – – – – – – – – – – – – – – 128 243 Figure 7A-52.  Maximum Cruise Power, 1700 RPM, ISA + 30 C