AEROPRAKT-32 Pilot Operating Handbook
A32-103-POH
24
C.G. position for the maximum take-off weight:
Item
Weight,
kg/lbs
×
CG arm,
m/inch
=
Moment,
kg×m/lbs×inch
Empty airplane
Crew (2×xx.x kg)
Baggage
Fuel (2×xx l)
Total:
X
CG
= Total moment / Total weight
=
Note
: X
CG
must be between 1.529 m and 1.780 m (19% and 37% MAC) as shown in
6.2 Installed equipment list
This subsection contains a table with the list of the installed optional equipment affecting
weight and balance of the aircraft. It is responsibility of the aircraft owner/operator that any
such equipment installed in the aircraft after the date of its manufacture is listed in the
table below.
No.
Equipment description and Part No.
Weight, kg CG arm, m
Summary of Contents for A32-103-POH
Page 29: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 29 Fig 3 Fuel system schematic...
Page 36: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 36 Fig 10 Engine pre start mixture control...
Page 38: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 38 Fig 12 Brake control system...
Page 50: ...AEROPRAKT 32 Pilot Operating Handbook A32 103 POH 50 Fig 22 Recovery system...
