File:FAA-8083-13 Fig 7-20.PNG

FAA-8083-13_Fig_7-20.PNG(733 × 295 pixels, file size: 29 KB, MIME type: image/png)

Summary

Description

Figure 7-20. Ground launch wind gradient.

Effect of wind gradient on airspeed during ground launch. Pilot must monitor airspeed indicator carefully. Goal is to fly fast enough to maintain safe margin above stall speed, but slower than

maximum permitted ground launch airspeed.
Source (2004) Airplane Flying Handbook, U.S. Government Printing Office, Washington D.C.: U.S. Federal Aviation Administration
Author FAA

Licensing

Public domain
This image or file is a work of a Federal Aviation Administration employee, taken or made as part of that person's official duties. As a work of the U.S. federal government, the image is in the public domain in the United States.

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Original upload log

The original description page was here. All following user names refer to en.wikipedia.
  • 2007-05-29 02:22 Dhaluza 733×295×8 (30122 bytes) Figure 7-20. Ground launch wind gradient. Effect of wind gradient on airspeed during ground launch. Pilot must monitor airspeed indicator carefully. Goal is to fly fast enough to maintain safe margin above stall speed, but slower than maximum permitted g

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Date/TimeThumbnailDimensionsUserComment
current17:48, 14 August 2007Thumbnail for version as of 17:48, 14 August 2007733 × 295 (29 KB)Seedermaster~commonswiki{{Information |Description=Figure 7-20. Ground launch wind gradient. Effect of wind gradient on airspeed during ground launch. Pilot must monitor airspeed indicator carefully. Goal is to fly fast enough to maintain safe margin above stall speed, but slow
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