Standard Operating Procedures
L410 UVP-E20
Document No.:
SOP-L410-1
Page 2- 5
Rev: 1
Date: JAN 18
Prepared by: LA
Checked by: CLS
CENTRE OF GRAVITY (LANDING GEAR EXTENDED)
The centre of gravity limits must be always inside the envelope given by the curve
shown in Fig. 2
−
1. The position of the Mean Aerodynamic Chord is shown in Fig. 2
−
1. The dimensions are given in mm (inches).
The airplane will not tip over when being loaded if its centre of gravity is
maintained within the envelope during loading.
Summary of Contents for L410 UVP-E20
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