Symphony SA-160 - Page 127

SA 160
AIRCRAFTA I R C R A F T
Symphony
AIRCRAFT
6-7
SECTION 6
WEIGHT AND BALANCE
Feb 25, 2005
(d) Basic Empty Weight Center of Gravity
(1) The basic empty weight We (as weighed including equipment
noted in the equipment list, required oil level and unusable
fuel) is given by:
We=N+L+R
where;
N = Nose wheel net weight (lbs)
R = Right main wheel net weight (lbs)
L = Left main wheel et weight (lbs)
(2) The center of gravity C of G corresponding to the basic
aircraft empty weight is given by;
CofG
We
where;
A = Distance from nose wheel from reference datum 44.2 In.
B = Distance from right and left main wheel from reference
datum 113.2 In.
(3) The empty weight moment Me corresponding to the basic
aircraft empty weight and C of G is given by;
Me= WexCofG
ThisdataisprovidedforeachSA160attimeofdelivey.
We
We =
We
We
N(A) + (R+L)(B)