Image: FAA-8083-13 Fig 7-20
FAA-8083-13_Fig_7-20.PNG (733 × 295 pixels, file size: 29 KB, MIME type: image/png)
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.
Title: FAA-8083-13 Fig 7-20
Credit: (2004) Airplane Flying Handbook, U.S. Government Printing Office, Washington D.C.: U.S. Federal Aviation Administration
Author: FAA
Usage Terms: Public domain
License: Public domain
Attribution Required?: No
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