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Gear and Flaps Down Part 2 - NAR Associates

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1500<br />

1000<br />

E33A<br />

W = 3300 lbs<br />

Sea Level<br />

500<br />

Rate-of-climb (fpm)<br />

-500<br />

0<br />

-1000<br />

-1500<br />

0 50 100 150 200 250<br />

Velocity (mph)<br />

3f<br />

2f<br />

f<br />

Figure 4.<br />

Rate-of-climb versus velocity.<br />

configuration. Thus, precise speed control <strong>and</strong> attention to cleaning up the aircraft become more<br />

important. We’ll look at density altitude effects in Altitude Effects, <strong>Part</strong> 1.<br />

Copyright c○1996 David F. Rogers. All rights reserved. 6

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