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<td><font color="#056F8B"><strong>8. CRUISE OPERATING (2)</strong></font></td>
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<p><font face="Arial" style="font-size: 9pt; font-weight:700">Lockheed 1049G/C121G Super Constellation<br>
<em>Operations Manual</em> Synopsis</font></p>
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<td colspan="8"><font face="Arial" style="font-size: 11pt; font-weight:700"><strong>Long Range Cruise Operating Tables (2 of 2)</strong></font><br>
Four R3350-93A Engines, 115/145 grade fuel</td>
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<td colspan="8"><font face="Arial" style="font-size: 11pt; font-weight:700"><strong>120,000 Lbs. Gross Weight</strong></font></td>
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<td><strong>Altitude</strong></td>
<td><strong>BHP</strong></td>
<td><strong>RPM</strong></td>
<td><strong>BMEP</strong></td>
<td><strong>F.F.</strong></td>
<td><strong>TAS</strong></td>
<td><strong>Mixture</strong></td>
<td><strong>Blowers</strong></td>
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<td>5,000 Ft.</td>
<td>1433</td>
<td>1875</td>
<td>181</td>
<td>580</td>
<td>208</td>
<td>Lean</td>
<td>Low</td>
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<td>10,000 Ft.</td>
<td>1548</td>
<td>2150</td>
<td>170</td>
<td>630</td>
<td>225</td>
<td>Lean</td>
<td>Low</td>
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<td>15,000 Ft.</td>
<td>1676</td>
<td>2470</td>
<td>160</td>
<td>700</td>
<td>243</td>
<td>Lean</td>
<td>Low</td>
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<td>20,000 Ft.</td>
<td>1765</td>
<td>2425</td>
<td>172</td>
<td>733</td>
<td>258</td>
<td>Lean</td>
<td>High</td>
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<td colspan="8"><font face="Arial" style="font-size: 11pt; font-weight:700"><strong>130,000 Lbs. Gross Weight</strong></font></td>
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<td><strong>Altitude</strong></td>
<td><strong>BHP</strong></td>
<td><strong>RPM</strong></td>
<td><strong>BMEP</strong></td>
<td><strong>F.F.</strong></td>
<td><strong>TAS</strong></td>
<td><strong>Mixture</strong></td>
<td><strong>Blowers</strong></td>
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<td>5,000 Ft.</td>
<td>1570</td>
<td>2010</td>
<td>184</td>
<td>630</td>
<td>212</td>
<td>Lean</td>
<td>Low</td>
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<td>10,000 Ft.</td>
<td>1696</td>
<td>2240</td>
<td>176</td>
<td>685</td>
<td>230</td>
<td>Lean</td>
<td>Low</td>
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<td>15,000 Ft.</td>
<td>1784</td>
<td>2405</td>
<td>175</td>
<td>760</td>
<td>244</td>
<td>Lean</td>
<td>High</td>
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<td>20,000 Ft.</td>
<td>1938</td>
<td>2500</td>
<td>183</td>
<td>1250</td>
<td>264</td>
<td>Auto-rich</td>
<td>High</td>
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<td colspan="8"><font face="Arial" style="font-size: 11pt; font-weight:700"><strong>140,000 Lbs. Gross Weight</strong></font></td>
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<td><strong>Altitude</strong></td>
<td><strong>BHP</strong></td>
<td><strong>RPM</strong></td>
<td><strong>BMEP</strong></td>
<td><strong>F.F.</strong></td>
<td><strong>TAS</strong></td>
<td><strong>Mixture</strong></td>
<td><strong>Blowers</strong></td>
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<td>5,000 Ft.</td>
<td>1711</td>
<td>2195</td>
<td>184</td>
<td>695</td>
<td>218</td>
<td>Lean</td>
<td>Low</td>
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<td>10,000 Ft.</td>
<td>1848</td>
<td>2350</td>
<td>186</td>
<td>750</td>
<td>235</td>
<td>Lean</td>
<td>Low</td>
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<td>15,000 Ft.</td>
<td>1941</td>
<td>2500</td>
<td>184</td>
<td>1280</td>
<td>248</td>
<td>Auto-rich</td>
<td>High</td>
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<td>20,000 Ft.</td>
<td>2109</td>
<td>2600</td>
<td>192</td>
<td>1395</td>
<td>270</td>
<td>Auto-rich</td>
<td>High</td>
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<td colspan="8"><div align="left">
* <strong>F.F.:</strong> Fuel Flow in GPH<br>
* <strong>TAS:</strong> True Airspeed is IAS corrected for instrument error,
temperature, and pressure.<br>
* <strong>Ignition:</strong> Retard spark above 2500 RPM with low blowers,
and above 2400 RPM with high blowers. Except when the checklist directs
otherwise, use Normal Spark below these RPM settings.<br>
* <strong>Above table</strong> is calculated from <em>Operations Manual</em>
graphs (pages A6-38, figure A6-36 (sheet 1 of 5) to A6-42, figure A6-36 (sheet
5 of 5). Use these tables for other flight conditions.</div></td>
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