AEROPRAKT-32 Pilot Operating Handbook
A32-060-POH
23
C.G. position for the maximum take-off weight:
Item
Weight,
kg/lbs.
×
CG arm,
m/inch
=
Moment,
kg×m/lbs×inch
Empty airplane
724.2
×
62.4
=
45190
Crew (2× 79.5 kg)
350
×
65.5
=
22925
Baggage
45
×
91.3
=
4109
Fuel (2×57 l)
181.0
×
77.2
=
13973
Total:
1300.2
86197
X
CG
= Total moment / Total weight
=
66.3
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
Содержание A32
Страница 24: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 24 No Equipment description and Part No Weight kg CG arm m...
Страница 28: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 28 Fig 3 Fuel system schematic...
Страница 37: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 37 Fig 12 Brake control system...
Страница 42: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 42 Fig 15 Wiring diagram of A 32 electrical system main...
Страница 43: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 43 Fig 16 Block diagram of Garmin G3X system installation...
Страница 52: ...AEROPRAKT 32 Pilot Operating Handbook A32 060 POH 52 Fig 25 Recovery system...
