Leerjet 35/36 Developed for Training Purposes 3-15
February 1998
Limitations
Center-of-Gravity Envelope
17,000 lb takeoff weight
Forward CG limit is fuselage station (F.S.) 366.31 (5% MAC) for
all weights up to and including 10,000 lbs; tapers through F.S.
375.96 (16.66% MAC) at 17,000 lbs to F.S. 376.31 (17.09%
MAC) at 17,250 lbs. The aft CG limit is F.S. 387.00 (30% MAC)
for all weights.
Figure 35-1.17,000Lbs Center-of-Gravity Envelope Chart
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