Aeropro A220 - 10 Appendix; Airplane Weight and Balance Statement

Aeropro CZ - A220 taildragger - Pilot Operating Handbook and Flight Training Supplement
March 21, 2020
47
Appendix 1. Airplane weight and balance statement - example
The CG position of empty aircraft is determined by weighing. 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
Registration:
Values weighed:
Main wheels
right-hand
Mrh =
L=
left-hand
Mlh =
L
1
=
Tail wheel
Most =
Resulting weight
Mres =
C.G. position
B = (M
ost
x (L- L
1
) – M
pr
x L
1
) / M
rst
= [ mm]
X = B + 50 = [ mm ]
_
X = (X x 100) / 1300 = [ %MAC ]
Date: Performed by:
Aircraft Leveling: