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Learjet 35 - Page 201

Learjet 35
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Leerjet 35/36 Developed for Training Purposes 3-17
February 1998
Limitations
Center-of-Gravity Envelope
18,000 lb takeoff weight
Forward CG limit is F.S. 366.31 (5% MAC) for all weights up to
and including 10,000 lbs; tapers through F.S. 377.34 (18.83%
MAC) at 18,000 lbs to F.S. 377.69 (18.76% MAC) at 18,250 lbs.
Figure 35-2.18,000Lbs Center-of-Gravity Envelope Chart

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