Center of Gravity
The following geometry applies to the PA-38-112 airplane when it is level. Refer to Leveling paragraph Chapter-8 of the Maintenance manual.
2.
The empty weight center of gravity (as weighed including optional equipment, full oil and operating fluids) can be determined by the followingformula:
C.G. Arm = N (A) + (R + L) (B) inches
T
Where: T = N + R + L
3.
Basic Empty Weight