![](https://www.pdfsearch.io/img/c0ac0df13caa665d70cb65025186694e.jpg) Date: 2016-03-23 15:15:49
| | TIME/DISTANCE/FUEL TO DESCEND Distance Based On Zero Wind Parameters: Descent Rate: 500 FPM Descent Speed: 90 KTS Power Setting: 2100 RPM Time: (Cruise Altitude – TPA)/500Add to Reading ListSource URL: aviation.ou.eduDownload Document from Source Website File Size: 174,91 KBShare Document on Facebook
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