TM 1-1510-218-10 7A-110 ONE ENGINE INOPERATIVE MAXIMUM CRUISE POWER 1900 RPM ISA NOTES: DURING   OPERATION   WITH   ICE   VANE   EXTENDED,   TORQUE   WILL   DECREASE.      IF ORIGINAL  POWER  IS  NOT  OR  CANNOT  BE  RESET,  TRUE  AIRSPEED  WILL  DECREASE APPROXIMATELY 20 KNOTS AND FUEL FLOW  WILL DECREASE APPROXIMATELY 7%.  IF ORIGINAL  POWER IS RESET, TRUE AIRSPEED WILL BE UNCHANGED  AND FUEL  FLOW WILL INCREASE APPROXIMATELY 30 LB/HR/ENG. 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 18 15 100 525 184 185 186 187 188 189 190 191 2000 14 11 100 511 181 188 184 190 186 192 188 194 4000 11 7 100 497 179 190 181 193 184 196 186 198 6000 7 3 100 483 176 193 179 196 181 199 183 201 8000 3 -1 100 469 173 196 176 200 179 202 181 205 10,000 -1 -5 100 457 170 199 174 202 176 206 179 208 12,000 -5 -9 97 436 165 198 169 203 172 207 174 210 14,000 -9 -13 93 412 157 195 162 201 166 206 169 209 16,000 -13 -17 88 390 148 190 154 198 159 204 163 208 18,000 -17 -21 83 369 138 183 146 194 152 201 156 206 20,000 -21 -25 79 351 119 163 137 188 145 198 150 205 22,000 -26 -29 74 329 – – – – – – 123 175 136 193 143 202 24,000 -30 -33 69 305 – – – – – – – – – – – – 123 180 133 196 26,000 -33 -37 65 283 – – – – – – – – – – – – – – – – – – 121 185 28,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 29,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 31,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 33,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – 35,000 – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – – Figure 7A-98.  One Engine Inoperative Maximum Cruise Power, 1900 RPM, ISA