EuroFOX - Pilot Operating Handbook and Flight Training Supplement
May 1. 2019
3-26
3.2.1 Airplane weight and balance statement
The CG position of empty aircraft is determined by weighting. The
procedure is described in the Maintenance manual. The whole procedure
must be repeated and new
Airplane weight and balance statement
must
be prepared whenever a modification or repair having impact to the weight
of the aircraft occurs.
Serial Number
56219
Registration:
4X-HSE
Aircraft Leveling:
Values Weighed:
Main wheels
right-hand
MRH =
L=
left-hand
MLH =
L
1
=
Nose wheel
MTS =
Resulting weight
Mres =
C.G. position
B = (M
pr
x L ) / M
vys
=
mm
X = L1
– B + 50 =
mm
_
X = (X x 100) / 1300 =
% B
SAT
Date:
Performed by:
3.2.2 Weight and balance determination for flight
WARNING
The aircraft must not be operated in violation of its
approved weight and balance limitations to assure safe
flying.
